Electromagnetic actuator, vibration reduction apparatus, suspension system, and vehicle

Abstract

An electromagnetic actuator (1000), a vibration reduction apparatus (5000), a suspension system (10000), and a vehicle (20000). The electromagnetic actuator comprises a first assembly (220), a second assembly (210), and a measurement module (900); the second assembly is coupled to the first assembly to allow relative movement between the first assembly and the second assembly; and the measurement module is used for measuring relative displacement of the first assembly with the second assembly.

Description

Electromagnetic actuator, vibration damping device, suspension system and vehicle

[0001] CROSS-REFERENCE TO RELATED APPLICATIONS

[0002] This application is based on the Chinese patent application "Electromagnetic actuator, vibration damping device, suspension system and vehicle" with application number 202311868498.9 and application date December 29, 2023, and claims the priority of the above-mentioned Chinese patent application. The entire content of the above-mentioned Chinese patent application is hereby introduced into this application as a reference. Technical Field

[0003] The present application belongs to the field of vehicle technology, and specifically relates to an electromagnetic actuator, a vibration reduction device, a suspension system, and a vehicle. Background Art

[0004] An electromagnetic actuator is an electric motor that directly generates linear motion through electromagnetic force. It usually includes a stator assembly and a mover assembly. The stator assembly includes a winding coil wound on an iron core shaft. The winding coil is electrically connected to a power supply and can generate a magnetic field when energized to generate magnetic force with the mover assembly, thereby driving the mover assembly to move in a straight line.

[0005] However, existing electromagnetic actuators cannot effectively detect the position of the actuator assembly, which affects the working performance of the electromagnetic actuator. Summary of the Invention

[0006] To this end, the present application proposes an electromagnetic actuator, which can effectively detect the position of the mover assembly, solving the technical problem in the prior art that the electromagnetic actuator cannot effectively detect the position of the mover assembly, affecting the working performance of the electromagnetic actuator.

[0007] According to an embodiment of the present application, the electromagnetic actuator includes: a first component; a second component, the second component and the first component are coupled so that the first component and the second component can move relative to each other; and a detection module, the detection module being used to detect the relative displacement of the first component and the second component.

[0008] According to the electromagnetic actuator of the embodiment of the present application, a detection module is provided to detect the relative displacement of the first component and the second component, thereby accurately determining the relative position of the first component and the second component, facilitating the control of the movement of the first component and the second component, ensuring the stability of the relative movement of the first component and the second component, and thus ensuring the working performance of the electromagnetic actuator.

[0009] Optionally, the electromagnetic actuator also includes a housing, a accommodating cavity is formed in the housing, the first component and the second component are both arranged in the accommodating cavity, one of the first component and the second component is connected to the housing, and the first component and the second component are coupled so that one of the first component and the second component moves along the axis with the housing.

[0010] Optionally, the detection module includes a laser sensor, and the laser sensor is arranged at the top or bottom of the accommodating cavity.

[0011] Optionally, the housing is suitable for being fixed to the axle, and the electromagnetic actuator further includes a mounting bracket, which is mounted to the outside of the housing and is suitable for connecting the axle and the housing. The laser sensor is arranged in the mounting bracket, and the bottom wall of the accommodating cavity is provided with an avoidance hole for avoiding the optical path of the laser sensor.

[0012] Optionally, the electromagnetic actuator further includes a center rod, which connects the first component and the other of the second component; the detection module includes a first detection member and a second detection member coupled to the first detection member, and one of the housing and the center rod is provided with the first detection member and the other is provided with the second detection member.

[0013] Optionally, the housing is suitable for being fixed to a vehicle axle, and the center rod passes through a top wall of the housing to be connected to a vehicle body; the first detection member is provided on the housing, and the second detection member is provided on the center rod.

[0014] Optionally, the first detection component is arranged on the outside of the housing.

[0015] Optionally, a bearing is provided between the center rod and the housing, and a portion of the radial projection of the first detection member that overlaps with the housing partially overlaps with the radial projection of the bearing.

[0016] Optionally, a bearing is provided between the central rod and the housing, and the first detection member is spaced apart from the bearing.

[0017] Optionally, a mounting bracket is provided at the bottom of the casing, and an avoidance channel connected to the accommodating cavity is provided in the mounting bracket; at least a portion of the second detection member is located in the avoidance channel, and the first detection member can be moved into the avoidance channel to couple with the second detection member.

[0018] Optionally, the second detection member is formed in an arc shape.

[0019] According to an embodiment of the present application, the vibration reduction device includes the aforementioned electromagnetic actuator, which is suitable for being connected between the wheel and the vehicle body.

[0020] According to the vibration reduction device of the embodiment of the present application, the aforementioned electromagnetic actuator is adopted to ensure the working performance of the vibration reduction device.

[0021] The suspension system according to the embodiment of the present application includes the aforementioned vibration reduction device.

[0022] According to the suspension system of the embodiment of the present application, the aforementioned vibration reduction device is adopted to ensure the working performance of the suspension system.

[0023] A vehicle according to an embodiment of the present application includes the aforementioned suspension system.

[0024] According to the vehicle of the embodiment of the present application, the aforementioned suspension system is adopted to ensure the working performance of the vehicle and improve the comfort of the vehicle.

[0025] Additional aspects and advantages of the present application will become apparent from the following description or may be learned through practice of the present application. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] The above and / or additional aspects and advantages of the present application will become apparent and easily understood from the description of the embodiments in conjunction with the following drawings, in which:

[0027] FIG1 is a schematic diagram of an electromagnetic actuator according to some embodiments of the first aspect of the present application.

[0028] FIG2 is a cross-sectional view of an electromagnetic actuator according to some embodiments of the first aspect of the present application.

[0029] FIG3 is an exploded view of an electromagnetic actuator according to some embodiments of the first aspect of the present application.

[0030] FIG. 4 is an enlarged view of a portion of the structure of the electromagnetic actuator in FIG. 2 .

[0031] FIG5 is a schematic diagram of an electromagnetic actuator according to some embodiments of the second aspect of the present application.

[0032] FIG6 is an exploded view of an electromagnetic actuator according to some embodiments of the second aspect of the present application.

[0033] FIG7 is a cross-sectional view of an electromagnetic actuator according to some embodiments of the second aspect of the present application.

[0034] FIG8 is an exploded view of an electromagnetic actuator according to some other embodiments of the second aspect of the present application.

[0035] FIG9 is a schematic diagram of the first sub-housing of some embodiments of the second aspect of the present application.

[0036] FIG10 is a schematic diagram of the first sub-housing from another angle in some embodiments of the second aspect of the present application.

[0037] FIG11 is a schematic diagram of the second sub-shell of some embodiments of the second aspect of the present application.

[0038] FIG12 is a schematic diagram of the second sub-housing from another angle in some embodiments of the second aspect of the present application.

[0039] Figure 13 is a schematic diagram of the guide rod of some embodiments of the second aspect of the present application.

[0040] Figure 14 is a schematic diagram of the center rod and the second component of some embodiments of the second aspect of the present application.

[0041] Figure 15 is a front view of the bearing of some embodiments of the second aspect of the present application.

[0042] Figure 16 is a schematic diagram of bearings in some embodiments of the second aspect of the present application.

[0043] FIG17 is a cross-sectional view of an electromagnetic actuator according to some embodiments of the third aspect of the present application.

[0044] FIG18 is a partial enlarged view of area A in FIG17 .

[0045] FIG19 is a top view of an electromagnetic actuator according to some embodiments of the third aspect of the present application.

[0046] Figure 20 is a cross-sectional view of an electromagnetic actuator according to other embodiments of the third aspect of the present application.

[0047] Figure 21 is a schematic diagram of an electromagnetic actuator in some embodiments of the fourth aspect of the present application.

[0048] Figure 22 is a cross-sectional view of an electromagnetic actuator in some embodiments of the fourth aspect of the present application.

[0049] FIG23 is a schematic diagram of a partial structure of the electromagnetic actuator in FIG22 .

[0050] Figure 24 is a schematic diagram of the electromagnetic actuator of some embodiments of the fourth aspect of the present application with some structures omitted.

[0051] Figure 25 is a front view of the center rod of some embodiments of the fourth aspect of the present application.

[0052] Figure 26 is a schematic diagram of the outlet device and connecting wires of some embodiments of the fourth aspect of the present application.

[0053] Figure 27 is a cross-sectional view of an electromagnetic actuator of some embodiments of the fifth aspect of the present application.

[0054] Figure 28 is a schematic diagram of the center rod and the second part of some embodiments of the fifth aspect of the present application.

[0055] Figure 29 is a cross-sectional view of a partial structure of an electromagnetic actuator in some embodiments of the fifth aspect of the present application.

[0056] Figure 30 is a top view of the partial structure of the electromagnetic actuator of some embodiments of the fifth aspect of the present application.

[0057] Figure 31 is a schematic diagram of the second component of some embodiments of the fifth aspect of the present application.

[0058] Figure 32 is a cross-sectional view of the center rod and the second part of other embodiments of the fifth aspect of the present application.

[0059] Figure 33 is a schematic diagram of the second component of some other embodiments of the fifth aspect of the present application.

[0060] Figure 34 is a schematic diagram of the partial structure of the electromagnetic actuator of some further embodiments of the fifth aspect of the present application.

[0061] Figure 35 is a schematic diagram of the partial structure of the second component of some further embodiments of the fifth aspect of the present application.

[0062] Figure 36 is a cross-sectional view of an electromagnetic actuator of some embodiments of the sixth aspect of the present application.

[0063] Figure 37 is a cross-sectional view of the center rod of some embodiments of the sixth aspect of the present application.

[0064] Figure 38 is a top view of the partial structure of the electromagnetic actuator of some embodiments of the sixth aspect of the present application.

[0065] Figure 39 is a cross-sectional view of a partial structure of an electromagnetic actuator in some embodiments of the sixth aspect of the present application.

[0066] Figure 40 is a cross-sectional view of the center rod of other embodiments of the sixth aspect of the present application.

[0067] FIG41 is a schematic diagram of some embodiments of the first aspect of the stator core of the present application.

[0068] FIG42 is a schematic diagram of a structure in which part of the stator core in FIG41 is cut away.

[0069] FIG43 is a schematic diagram of some embodiments of the second aspect of the stator core of the present application.

[0070] FIG44 is a schematic diagram of a structure in which part of the stator core in FIG43 is cut away.

[0071] Figure 45 is a schematic diagram of some embodiments of the third aspect of the stator core of the present application.

[0072] FIG46 is a schematic diagram of a structure in which part of the stator core in FIG45 is cut away.

[0073] Figure 47 is a schematic diagram of some embodiments of the fourth aspect of the stator core of the present application.

[0074] FIG48 is a schematic diagram of a structure in which part of the stator core in FIG47 is cut away.

[0075] Figure 49 is a schematic diagram of some embodiments of the fifth aspect of the stator core of the present application.

[0076] Figure 50 is an exploded view of some embodiments of the fifth aspect of the stator core of the present application.

[0077] Figure 51 is an exploded view of some embodiments of the fifth aspect of the stator core of the present application.

[0078] Figure 52 is a schematic diagram of some embodiments of the sixth aspect of the stator core of the present application.

[0079] Figure 53 is an exploded view of some embodiments of the sixth aspect of the stator core of the present application.

[0080] Figure 54 is a schematic diagram of some embodiments of the seventh aspect of the stator core of the present application.

[0081] Figure 55 is a top view of the stator yoke in Figure 54.

[0082] Figure 56 is a cross-sectional view of Figure 55 along line AA.

[0083] Figure 57 is a schematic diagram of the stator teeth in Figure 54.

[0084] Figure 58 is a partial enlarged view of the stator teeth and stator yoke in Figure 54 when they are matched.

[0085] Figure 59 is a schematic diagram of an electromagnetic actuator in some embodiments of the seventh aspect of the present application.

[0086] Figure 60 is a schematic diagram of the second component in Figure 59.

[0087] Figure 61 is a cross-sectional view of the second component in Figure 60.

[0088] Figure 62 is a partially enlarged view of area B in Figure 61.

[0089] Figure 63 is a schematic diagram of the first type of iron core in some embodiments of the seventh aspect of the present application.

[0090] Figure 64 is a schematic diagram of the insulating skeleton of some embodiments of the seventh aspect of the present application.

[0091] Figure 65 is a schematic diagram of coils of some embodiments of the seventh aspect of the present application.

[0092] Figure 66 is a schematic diagram of the second type of iron core and coil in some embodiments of the seventh aspect of the present application.

[0093] Figure 67 is a schematic diagram of the third type of iron core in some embodiments of the present application.

[0094] Figure 68 is a cross-sectional view of the third type of core in some embodiments of the present application.

[0095] Figure 69 is a schematic diagram of the support core of some embodiments of the present application.

[0096] Figure 70 is a schematic diagram of a support frame according to some embodiments of the present application.

[0097] Figure 71 is a cross-sectional view of the third type of iron core and coil in some embodiments of the present application.

[0098] Figure 72 is a schematic diagram of an electromagnetic actuator in some embodiments of the eighth aspect of the present application.

[0099] Figure 73 is a cross-sectional view of an electromagnetic actuator of some embodiments of the eighth aspect of the present application.

[0100] Figure 74 is a cross-sectional view of the casing of some embodiments of the eighth aspect of the present application.

[0101] Figure 75 is a schematic diagram of the center rod of some embodiments of the eighth aspect of the present application.

[0102] Figure 76 is a schematic diagram of another angle of the center rod of some embodiments of the eighth aspect of the present application.

[0103] Figure 77 is an exploded view of the center rod of some embodiments of the eighth aspect of the present application.

[0104] Figure 78 is a schematic diagram of the first wiring assembly of some embodiments of the eighth aspect of the present application.

[0105] Figure 79 is a front view of the first wiring assembly of some embodiments of the eighth aspect of the present application.

[0106] Figure 80 is an exploded view of the first wiring assembly of some embodiments of the eighth aspect of the present application.

[0107] Figure 81 is a schematic diagram of the second wiring assembly of some embodiments of the eighth aspect of the present application.

[0108] Figure 82 is a front view of the second wiring assembly of some embodiments of the eighth aspect of the present application.

[0109] Figure 83 is an exploded view of the second wiring assembly of some embodiments of the eighth aspect of the present application.

[0110] Figure 84 is a schematic diagram of the third wiring assembly of some embodiments of the eighth aspect of the present application.

[0111] Figure 85 is a front view of the third wiring assembly of some embodiments of the eighth aspect of the present application.

[0112] Figure 86 is an exploded view of the third wiring assembly of some embodiments of the eighth aspect of the present application.

[0113] Figure 87 is a schematic diagram of the first core unit of some embodiments of the eighth aspect of the present application.

[0114] Figure 88 is a top view of the first core unit of some embodiments of the eighth aspect of the present application.

[0115] Figure 89 is an exploded view of the first core unit of some embodiments of the eighth aspect of the present application.

[0116] Figure 90 is an exploded view of the inner wire outlet device of some embodiments of the eighth aspect of the present application.

[0117] Figure 91 is a schematic diagram of coils of some embodiments of the eighth aspect of the present application.

[0118] Figure 92 is a top view of the coils of some embodiments of the eighth aspect of the present application.

[0119] Figure 93 is a schematic diagram of the second type of iron core in some embodiments of the eighth aspect of the present application.

[0120] Figure 94 is a cross-sectional view of the second type of iron core of some embodiments of the eighth aspect of the present application.

[0121] Figure 95 is a schematic diagram of the second type of iron core of some embodiments of the eighth aspect of the present application after the coil is omitted.

[0122] Figure 96 is a schematic diagram of the inner wiring device of some embodiments of the eighth aspect of the present application.

[0123] Figure 97 is an exploded view of the inner wiring device of some embodiments of the eighth aspect of the present application.

[0124] Figure 98 is a schematic diagram of the second core unit of some embodiments of the eighth aspect of the present application.

[0125] Figure 99 is a top view of the second core unit of some embodiments of the eighth aspect of the present application.

[0126] Figure 100 is a schematic diagram of the second core unit of some embodiments of the eighth aspect of the present application after the coil is omitted.

[0127] Figure 101 is a schematic diagram of the bottom wiring device of some embodiments of the eighth aspect of the present application.

[0128] Figure 102 is an exploded view of the bottom wiring device of some embodiments of the eighth aspect of the present application.

[0129] Figure 103 is a schematic diagram of the first outlet wire assembly of some embodiments of the eighth aspect of the present application.

[0130] Figure 104 is an exploded view of the first outlet wire assembly of some embodiments of the eighth aspect of the present application.

[0131] Figure 105 is a schematic diagram of the second output wire assembly of some embodiments of the eighth aspect of the present application.

[0132] Figure 106 is an exploded view of the second output wire assembly of some embodiments of the eighth aspect of the present application.

[0133] Figure 107 is a schematic diagram of the first phase lead connection of the electromagnetic actuator in some embodiments of the eighth aspect of the present application.

[0134] Figure 108 is a side view of Figure 107.

[0135] Figure 109 is a cross-sectional view of Figure 108 along line BB.

[0136] Figure 110 is a top view of Figure 107.

[0137] Figure 111 is a schematic diagram of the second phase lead connection of the electromagnetic actuator in some embodiments of the eighth aspect of the present application.

[0138] Figure 112 is a side view of Figure 111.

[0139] Figure 113 is a cross-sectional view of Figure 112 along line CC.

[0140] Figure 114 is a top view of Figure 111.

[0141] Figure 115 is a schematic diagram of the third phase lead connection of the electromagnetic actuator in some embodiments of the eighth aspect of the present application.

[0142] Figure 116 is a side view of Figure 115.

[0143] Figure 117 is a cross-sectional view of Figure 116 along line DD.

[0144] Figure 118 is a top view of Figure 115.

[0145] Figure 119 is a schematic diagram of an electromagnetic actuator in some embodiments of the ninth aspect of the present application.

[0146] Figure 120 is a schematic diagram of the partial structure of the electromagnetic actuator of some embodiments of the ninth aspect of the present application.

[0147] Figure 121 is a cross-sectional view of a partial structure of an electromagnetic actuator in some embodiments of the ninth aspect of the present application.

[0148] Figure 122 is an exploded view of the partial structure of the electromagnetic actuator of some embodiments of the ninth aspect of the present application.

[0149] Figure 123 is a top view of the insulating skeleton of some embodiments of the present application.

[0150] Figure 124 is a side view of the insulating skeleton of some embodiments of the present application.

[0151] Figure 125 is a schematic diagram of the insulating skeleton of some embodiments of the present application.

[0152] Figure 126 is a schematic diagram of the insulating skeleton from another angle in some embodiments of the present application.

[0153] Figure 127 is a schematic diagram of the insulation skeleton and the iron core assembly in some embodiments of the present application.

[0154] Figure 128 is a cross-sectional view of the partial structure of the electromagnetic actuator of some embodiments of the tenth aspect of the present application.

[0155] Figure 129 is an enlarged view of part of the structure in Figure 128.

[0156] Figure 130 is a partial cross-sectional view of part of the structure of the electromagnetic actuator of some embodiments of the tenth aspect of the present application.

[0157] Figure 131 is a schematic diagram of the partial structure of the electromagnetic actuator of some embodiments of the tenth aspect of the present application.

[0158] Figure 132 is a cross-sectional view of an electromagnetic actuator of some embodiments of the eleventh aspect of the present application.

[0159] Figure 133 is a partially enlarged view of area C in Figure 132.

[0160] Figure 134 is a partially enlarged view of area D in Figure 132.

[0161] Figure 135 is a cross-sectional view of an electromagnetic actuator of other embodiments of the eleventh aspect of the present application.

[0162] Figure 136 is a partially enlarged view of area E in Figure 135.

[0163] Figure 137 is a cross-sectional view of an electromagnetic actuator of some embodiments of the twelfth aspect of the present application.

[0164] Figure 138 is a schematic diagram of the partial structure of the electromagnetic actuator of some embodiments of the twelfth aspect of the present application.

[0165] Figure 139 is a partial cross-sectional view of the electromagnetic actuator in Figure 138.

[0166] Figure 140 is a cross-sectional view of the electromagnetic actuator in Figure 139 from another direction.

[0167] Figure 141 is a schematic diagram of an electromagnetic actuator in some embodiments of the thirteenth aspect of the present application.

[0168] Figure 142 is a cross-sectional view of an electromagnetic actuator in some embodiments of the thirteenth aspect of the present application.

[0169] Figure 143 is a schematic diagram of a laser sensor in some embodiments of the thirteenth aspect of the present application.

[0170] Figure 144 is a schematic diagram of some embodiments of the thirteenth aspect of the present application after the housing moves upward.

[0171] Figure 145 is a schematic diagram of some embodiments of the thirteenth aspect of the present application after the housing moves downward.

[0172] Figure 146 is a schematic diagram of the laser sensor and the second component of some embodiments of the thirteenth aspect of the present application.

[0173] Figure 147 is a bottom view of the electromagnetic actuator of some embodiments of the fourteenth aspect of the present application.

[0174] Figure 148 is a cross-sectional view of an electromagnetic actuator of some embodiments of the fourteenth aspect of the present application.

[0175] Figure 149 is a cross-sectional view of Figure 148 along line EE.

[0176] Figure 150 is a schematic diagram of the partial structure of the electromagnetic actuator of some embodiments of the fourteenth aspect of the present application.

[0177] Figure 151 is a cross-sectional view of an electromagnetic actuator of some embodiments of the fifteenth aspect of the present application.

[0178] Figure 152 is a schematic diagram of the partial structure of the electromagnetic actuator of some embodiments of the fifteenth aspect of the present application.

[0179] Figure 153 is one of the partial magnetic field distribution schematic diagrams of the electromagnetic actuator of some embodiments of the fifteenth aspect of the present application.

[0180] Figure 154 is the second schematic diagram of partial magnetic field distribution of the electromagnetic actuator of some embodiments of the fifteenth aspect of the present application.

[0181] Figure 155 is a linear relationship diagram between the magnetic field strength of the second detection component and the center rod stroke in some embodiments of the fifteenth aspect of the present application.

[0182] Figure 156 is a linear relationship diagram between the electrical signal of the first detection member and the center rod stroke in some embodiments of the fifteenth aspect of the present application.

[0183] Figure 157 is one of the structural schematic diagrams of the second detection component and the first detection component in some embodiments of the fifteenth aspect of the present application.

[0184] Figure 158 is the second structural schematic diagram of the second detection component and the first detection component in some embodiments of the fifteenth aspect of the present application.

[0185] Figure 159 is a cross-sectional view of an electromagnetic actuator of some embodiments of the sixteenth aspect of the present application.

[0186] Figure 160 is a partially enlarged view of area F in Figure 159.

[0187] Figure 161 is a schematic diagram of the first detection component of some embodiments of the sixteenth aspect of the present application.

[0188] Figure 162 is a schematic diagram of some embodiments of the sixteenth aspect of the present application after the housing moves upward.

[0189] Figure 163 is a schematic diagram of some embodiments of the sixteenth aspect of the present application after the housing moves downward.

[0190] Figure 164 is a bottom view of the electromagnetic actuator of some embodiments of the sixteenth aspect of the present application.

[0191] Figure 165 is a schematic diagram of the detection module of some embodiments of the seventeenth aspect of the present application.

[0192] Figure 166 is a schematic diagram of the detection module of some embodiments of the seventeenth aspect of the present application from another angle.

[0193] Figure 167 is a bottom view of the electromagnetic actuator of some embodiments of the seventeenth aspect of the present application.

[0194] Figure 168 is a schematic diagram of an electromagnetic actuator in some embodiments of the eighteenth aspect of the present application.

[0195] Figure 169 is a schematic diagram of the electromagnetic actuator of some embodiments of the eighteenth aspect of the present application with some structures omitted.

[0196] Figure 170 is an enlarged view of part of the structure in Figure 169.

[0197] Figure 171 is a cross-sectional view of an electromagnetic actuator of some embodiments of the eighteenth aspect of the present application.

[0198] Figure 172 is a top view of the electromagnetic actuator of some embodiments of the eighteenth aspect of the present application.

[0199] Figure 173 is an enlarged view of part of the structure in Figure 172.

[0200] Figure 174 is a schematic diagram of the suspension system of some embodiments of the present application.

[0201] Figure 175 is a cross-sectional view of a suspension system according to some embodiments of the present application.

[0202] Figure 176 is a schematic diagram of a vehicle according to some embodiments of the present application.

[0203] Reference numerals: 1000, electromagnetic actuator; 100, housing; 101, sub-housing; 1011, cylinder; 1013, slot; 1012, end cover; 400, guide rod; 430, Guide protrusion; 410, mounting boss; 411, through hole; 420, mounting plate; 421, fifth connecting hole; 1014, insertion portion; 110, first sub-housing; 115, first cavity; 111, first connecting portion; 1111, first connecting lug; 1112, first connecting hole; 112, third connecting portion; 1121, third connecting hole; 113, first avoidance groove; 114, third avoidance groove; 120, second sub-housing; 125, second cavity; 121, second connecting portion; 1211, second connecting lug; 1212, second connecting hole; 122, fourth connecting portion; 1221, fourth connecting hole; 123, second avoidance groove; 124, fourth avoidance groove 150, first fastener; 160, first avoidance through hole; 161, second avoidance through hole; 180, sixth connecting hole; 130, accommodating cavity; 131, avoidance hole; 193, anti-rotation hole; 194, wire groove; 195, second reinforcing rib; 191, mounting seat; 220, first component; 210, second component; 211, core assembly; 2014, stator core; 2141, stator tooth; 21411, first lamination; 21412, first center hole; 21416, first connecting structure; 21417, second anti-rotation protrusion; 2142, stator yoke; 21422, second lamination; 21421, second center hole; 21423, second Connecting structure; 21427, body; 21428, plug-in portion; 21425, anti-rotation groove; 2133, winding groove; 21415, positioning protrusion; 21424, inclined surface; 21426, first boss structure; 2012, first reinforcing rib; 2111, first type iron core; 21111, first annular groove; 21114, first iron core unit; 21115, second iron core unit; 21116, first internal mounting hole; 21117, third internal mounting hole; 2112, second type iron core; 21122, second internal mounting hole; 2119, placement groove; 350, second positioning portion; 2019, notch; 2013, cable trough; 2015, Wire outlet slot; 20111, groove; 2011, wiring space; 2016, support frame; 2017, support core; 2110, third type core; 212, winding assembly; 2121, connecting wire; 21211, first phase lead; 21212, second phase lead; 21213, third phase lead; 2018, first outlet; 214, second outlet; 2123, coil; 21231, lead wire; 21214, first phase winding; 21215, second phase winding; 21216, third phase winding; 2122, insulating paper; 213, insulating frame; 2131, lead channel; 2132, wire slot; 2138, second annular groove;2136, inner wall; 2134, second boss structure; 2135, insulating portion; 2137, assembly hole; 1016, bolt; 1017, positioning pin; 140, rotating shaft; 1015, elastic stopper; 300, center rod; 230, outlet device; 330, wire passage; 333, radial hole; 334, axial hole; 331, guide rod end outlet groove; 332, winding section outlet groove; 340, first positioning portion; 370, first anti-rotation portion; 320, cooling chamber; 3211, second water inlet; 3212, second water outlet; 32111, second cooling pipe; 32121, third cooling pipe; 321, first cooling chamber; 322, second cooling chamber; 3221 , sub-chamber; 810, cooling structure; 310, guide hole; 311, outlet; 831, first thread segment; 851, second thread segment; 312, sealing cover; 323, filling port; 2113, wiring assembly; 21131, long wiring assembly; 21132, middle wiring assembly; 21133, short wiring assembly; 2114, conductive member; 2115, insulating layer; 21151, first limiting feature; 2116, limiting member; 2117, first connector; 2118, second connector; 860, inner outlet device; 861, first assembly part; 862, first insulating member; 863, first conductor; 870, inner wiring device; 871, second assembly part; 872, second Insulator; 873, second conductor; 880, bottom terminal assembly; 881, third insulator; 882, third conductor; 8821, first phase connector; 8822, second phase connector; 8823, third phase connector; 216, outlet assembly; 2161, long outlet assembly; 2162, short outlet assembly; 2163, fourth insulator; 2164, fourth conductor; 2165, second retaining feature; 2166, retaining groove; 360, anti-rotation lever; 380, first retaining member; 390, second retaining member; 391, first portion; 392, second portion; 393, piston; 900, detection module; 910, laser sensor; 920, first sensor mounting bracket; 930 First detection component; 931, sensor connection end; 932, connecting rod; 933, sensor head; 940, second detection component; 950, assembly slot; 960, sensor mounting slot; 970, second sensor mounting bracket; 192, mounting bracket; 1921, avoidance channel; 170, bearing; 171, protrusion; 840, guide bearing; 850, limit nut; 500, upper support; 600, spring; 700, bushing; 800, buffer block; 830, assembly nut; 820, dust cover; 10000, suspension system; 2000, wheel; 3000, leaf spring; 4000, steering knuckle; 5000, vibration damping device; 6000, subframe; 20000, vehicle. DETAILED DESCRIPTION

[0204] The following describes in detail embodiments of the present application. Examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present application and are not to be construed as limiting the present application.

[0205] The electromagnetic actuator 1000 according to an embodiment of the present application will be described below with reference to the accompanying drawings.

[0206] As shown in FIG. 22 , an electromagnetic actuator 1000 according to an embodiment of the present application includes: a first component 220 , a second component 210 and a detection module 900 .

[0207] The second component 210 and the first component 220 are coupled so that the first component 220 and the second component 210 can move relative to each other.

[0208] The detection module 900 is used to detect the relative displacement between the first component 220 and the second component 210 .

[0209] As can be seen from the above structure, the electromagnetic actuator 1000 of the embodiment of the present application detects the relative displacement of the first component 220 and the second component 210 by setting a detection module 900, so that the position of the second component 210 can be accurately determined, the movement of the second component 210 can be controlled, and the position accuracy of the second component 210 after movement can be ensured, thereby improving the working performance of the electromagnetic actuator 1000.

[0210] At the same time, using the detection module 900 to detect the relative displacement of the first component 220 and the second component 210 can also reduce the difficulty of position detection of the second component 210 and ensure the accuracy of position detection of the second component 210.

[0211] It is understandable that, compared with the prior art, the electromagnetic actuator 1000 of the present application ensures the control accuracy of the moving position of the second component 210 by providing a detection module 900, thereby avoiding the technical problem of control accuracy defects.

[0212] In some embodiments, the detection module 900 can sense signals corresponding to different positions of the device under test and output position signals to the controller through wires to achieve the purpose of detecting the relative displacement of the first component 220 and the second component 210.

[0213] In some embodiments, as shown in FIG22 , the electromagnetic actuator 1000 further includes a housing 100, wherein a housing cavity 130 is formed in the housing 100, wherein a first component 220 and a second component 210 are both disposed in the housing cavity 130, wherein one of the first component 220 and the second component 210 is connected to the housing 100, and the first component 220 and the second component 210 are coupled so that one of the first component 220 and the second component 210 and the housing 100 move along an axis, thereby ensuring the working performance of the electromagnetic actuator 1000.

[0214] In some embodiments, the first component 220 is disposed in the housing 100 . Therefore, the above-mentioned detection module 900 detects the relative displacement between the first component 220 and the second component 210 . It can also be understood that the detection module 900 detects the relative displacement between the housing 100 and the second component 210 .

[0215] In some embodiments, as shown in conjunction with Figures 141-146 , the detection module 900 includes a laser sensor 910, which is disposed at the top or bottom of the accommodating cavity 130. This facilitates the use of the laser sensor 910 to detect the relative displacement between the housing 100 and the second component 210, thereby ensuring the accuracy of the relative displacement detection of the housing 100 and the second component 210 and reducing the difficulty of detecting the relative displacement between the housing 100 and the second component 210.

[0216] In some embodiments, as shown in conjunction with FIG141 and FIG142 , the housing 100 is adapted to be fixed to a vehicle axle, and the electromagnetic actuator 1000 further includes a mounting bracket 192, which is mounted to the exterior of the housing 100 and adapted to connect the vehicle axle to the housing 100. The laser sensor 910 is disposed within the mounting bracket 192, and the bottom wall of the accommodating cavity 130 is provided with a clearance hole 131 for avoiding the optical path of the laser sensor 910. By arranging the laser sensor 910 on the mounting bracket 192, the laser sensor 910 is disposed within the housing 100, thereby facilitating support of the laser sensor 910 by the housing 100 and improving the positional stability of the laser sensor 910. Furthermore, because the clearance hole 131 is provided on the bottom wall of the accommodating cavity 130 for avoiding the optical path of the laser sensor 910, the optical path generated by the laser sensor 910 disposed on the mounting bracket 192 can be projected into the accommodating cavity 130, thereby facilitating detection of relative displacement between the housing 100 and the second component 210 by the laser sensor 910.

[0217] In some embodiments, as shown in FIG143 , a first sensor mounting bracket 920 is provided at one end of the mounting bracket 192, and the laser sensor 910 is provided on the first sensor mounting bracket 920, so that the laser sensor 910 can be provided on the mounting bracket 192, making it easier to support the laser sensor 910 using the housing 100, thereby improving the positional stability of the laser sensor 910 and reducing the difficulty of fixing the laser sensor 910.

[0218] The laser sensor 910 and the first sensor mounting bracket 920 may be fixed by bolt connection.

[0219] In some embodiments, as shown in Figures 142-146, in the axial direction of the electromagnetic actuator 1000, the laser sensor 910 is facing the second component 210, so that the light path generated by the laser sensor 910 can be projected onto the second component 210, thereby facilitating the use of the laser sensor 910 to detect the relative displacement between the housing 100 and the second component 210.

[0220] In a specific example, the laser sensor 910 mainly determines the position by sensing the light reflected by the object and outputs the displacement signal of the electromagnetic actuator 1000. Its working principle is that before the electromagnetic actuator 1000 is started, the height of the laser sensor 910 is first calibrated and the position of the laser sensor 910 is measured. When the housing 100 moves upward relative to the second component 210 (as shown in Figure 144), the laser sensor 910 projects a visible light spot on the surface of the second component 210. The light reflected from the light spot is imaged on the photosensitive element in the laser sensor 910 through the light receiving system. When the laser sensor 910 is in contact with the second component 210, the laser sensor 910 is in contact with the photosensitive element in the laser sensor 910. 0 changes, the laser reflection angle will also change accordingly, causing the imaging position on the photosensitive element in the laser sensor 910 to change, thereby measuring the current position of the laser sensor 910 and the second component 210. When the housing 100 moves downward relative to the second component 210 (as shown in FIG145 ), the laser sensor 910 measures the current position of the laser sensor 910 and the second component 210 again according to the above method. By analyzing the changes in the position values ​​before and after the two times, the relative displacement of the housing 100 and the second component 210 can be obtained, thereby achieving the purpose of detecting the relative displacement of the housing 100 and the second component 210.

[0221] Through the above-mentioned configuration, this embodiment can be configured as an active measurement with a high measurement frequency, and the height parameters of the electromagnetic actuator 1000 can be obtained in real time. Neither low-frequency vibration nor even the stationary state of the vehicle 20000 affects the measurement parameters. In other words, even when the vehicle 20000 is stationary, it can still provide good information such as the posture of the vehicle 20000. Therefore, the laser sensor 910 of this embodiment can be used not only to measure the stroke of the electromagnetic actuator 1000, but also to obtain the movement speed of the electromagnetic actuator 1000 through the functional relationship between the difference in the stroke of the electromagnetic actuator 1000 and time. Taking Figures 144 and 145 as an example, the position of the housing 100 changes from Figure 144 to Figure 145 during one reflection reception cycle of the laser sensor 910. Based on this, the average speed of the electromagnetic actuator 1000 during one laser reflection reception cycle can be calculated. Because the measurement frequency of the laser sensor 910 is high, this speed can, to a certain extent, reflect the real-time speed of the electromagnetic actuator 1000.

[0222] In a specific example, the loads on different axles of vehicle 20000 can be preliminarily calculated by comparing the initial state of vehicle 20000. The basic principle is that the heights of the four wheels of vehicle 20000 are measured when vehicle 20000 starts or when vehicle 20000 is about to move. Since vehicle 20000 has no relative motion and road impact at this time, the distance change can be regarded as load compression damping. Based on this, the empty or fully loaded state of vehicle 20000 can be judged, thereby providing a more accurate reference basis for four-wheel control.

[0223] Similarly, the changes in the different speeds of the electromagnetic actuator 1000 within a laser reflection and reception cycle can reflect the real-time acceleration of the electromagnetic actuator 1000 to a certain extent. In theory, the number of sensors installed on the vehicle 20000 can be greatly reduced, achieving the purpose of economical design.

[0224] It should also be noted that, in this embodiment, the laser sensor 910 is arranged at the bottom of the electromagnetic actuator 1000, and the detection position is the bottom plane of the second component. Since the main movement of the housing 100 and the second component 210 is a linear movement up and down, in an actual motion scenario, the housing 100 and the second component 210 will also rotate relative to each other around the second component 210. Through the above arrangement, even if the housing 100 and the second component 210 are deflected, it can be ensured that the top of the mounting bracket 192, the laser sensor 910 and the bottom surface of the second component 210 remain parallel (as shown in FIG146), thereby avoiding the position data detected by the laser sensor 910 from being affected by the deflection of the housing 100 and the second component 210.

[0225] At the same time, since the laser sensor 910 is installed on the mounting bracket 192, the high temperature generated when the electromagnetic actuator 1000 moves can be avoided from interfering with the laser sensor 910, thereby ensuring the working performance of the laser sensor 910. At the same time, the laser sensor 910 is installed on the outside of the electromagnetic actuator 1000, which is more convenient for the replacement and installation of the laser sensor 910 and more conducive to after-sales replacement and maintenance.

[0226] In summary, this embodiment makes full use of the mounting bracket 192 and uses the laser sensor 910 with higher measurement accuracy to make up for the various shortcomings of traditional sensors. It surpasses traditional designs in many aspects such as layout space, measurement accuracy, measurement content, service life, and maintenance convenience.

[0227] In some embodiments, as shown in conjunction with Figures 150-163, the electromagnetic actuator 1000 further includes a central rod 300, which connects the first component 220 and the other of the second component 210. The detection module 900 includes a first detection member 930 and a second detection member 940, which is coupled to the first detection member 930. One of the housing 100 and the central rod 300 is provided with the first detection member 930, and the other is provided with the second detection member 940. This facilitates the use of the second detection member 940 and the first detection member 930 to cooperate in detecting the relative displacement between the housing 100 and the second component 210, thereby ensuring the accuracy of the position detection of the second component 210 and reducing the difficulty of the position detection of the second component 210.

[0228] In some embodiments, as shown in Figures 150-163 , the housing 100 is adapted to be fixed to a vehicle axle, and the center rod 300 passes through the top wall of the housing 100 to connect to the vehicle body; the first detection member 930 is provided on the housing 100, and the second detection member 940 is provided on the center rod 300. The housing 100 supports the first detection member 930, and the center rod 300 supports the second detection member 940, thereby improving the positional stability of the first detection member 930 and the second detection member 940, and facilitating the detection of relative displacement between the housing 100 and the second assembly 210 by the second detection member 940 in cooperation with the first detection member 930.

[0229] In some embodiments, as shown in Figures 147-150, an assembly groove 950 is provided on the center rod 300 (the specific structure of the assembly groove 950 can be seen in Figure 25), the second detection member 940 is fixed on the assembly groove 950 of the center rod 300, and a sensor mounting groove 960 is provided on the housing 100 facing the assembly groove 950. The first detection member 930 is arranged in the sensor mounting groove 960, forming a complete working environment for the position sensor, which is convenient for using the second detection member 940 and the first detection member 930 to detect the relative displacement of the housing 100 and the second component 210.

[0230] In some embodiments, as shown in Figures 151 to 154 , the first detection member 930 is disposed on the outside of the housing 100 , thereby reducing the difficulty of installing the first detection member 930 , and also facilitating replacement and repair of the first detection member 930 , thereby reducing the difficulty of maintaining the first detection member 930 .

[0231] At the same time, by arranging the first detection component 930 on the outside of the casing 100, the high temperature area of ​​the casing 100 can be effectively avoided, and the first detection component 930 can use natural wind to dissipate heat, which fully protects the first detection component 930 and avoids failure of the first detection component 930 to a certain extent.

[0232] In some embodiments, as shown in FIG152 , a bearing 170 is disposed between the center rod 300 and the housing 100, and the portion of the radial projection of the first detection member 930 that overlaps with the housing 100 partially overlaps with the radial projection of the bearing 170. In other words, the first detection member 930 and the bearing 170 partially overlap in the radial direction of the housing 100. This prevents the extension length of the bearing 170 from being excessively reduced due to the provision of the first detection member 930, provided that the extension length of the center rod 300 remains constant. In other words, by partially overlapping the first detection member 930 and the bearing 170, the extension length of the bearing 170 can be maintained, thereby ensuring the guiding effect of the bearing 170.

[0233] In some embodiments, the bearing 170 is provided with a sensor avoidance groove, and the first detection member 930 is disposed in the sensor avoidance groove. This allows the radial projection of the first detection member 930 to partially overlap with the housing 100 and the radial projection of the bearing 170. This also reduces the difficulty of securing the first detection member 930 and improves the positional stability of the first detection member 930, thereby ensuring the working performance of the first detection member 930 to a certain extent.

[0234] In some embodiments, a bearing 170 is disposed between the center rod 300 and the housing 100, and the first detection member 930 is spaced apart from the bearing 170. In other words, the portion where the radial projection of the first detection member 930 overlaps with the housing 100 is not limited to partially overlapping the radial projection of the bearing 170. Alternatively, the first detection member 930 and the bearing 170 may be spaced apart to ensure that the first detection member 930 and the bearing 170 are independent of each other and that their working performance is ensured.

[0235] The interval arrangement mentioned here can be understood as the first detection member 930 and the bearing 170 being spaced apart in the axial direction of the center rod 300 so that the first detection member 930 and the bearing 170 are independent of each other.

[0236] At the same time, a bearing 170 is provided between the center rod 300 and the housing 100 to limit the movement of the center rod 300. This allows the center rod 300 to move along the bearing 170, preventing the center rod 300 from easily deviating during the movement of the vehicle 20000, as shown in FIG158. The greater the deflection angle of the center rod 300, the greater the impact on the detection accuracy of the first detection member 930 and the second detection member 940, and even failure.

[0237] Therefore, by setting the bearing 170, the first detection member 930 has a good alignment with the second detection member 940 during the movement, and has a higher detection accuracy, thereby ensuring that during the normal operation of the detection module 900, the working surface of the first detection member 930 needs to remain parallel to the working surface of the second detection member 940 (as shown in Figure 157), so as to ensure that the second detection member 940 can obtain an accurate magnetic field signal, thereby ensuring the working performance of the detection module 900.

[0238] In some embodiments, as shown in FIG. 148 , the bearing 170 covers the top of the first detection member 930 , protecting the travel of the first detection member 930 and preventing the first detection member 930 from being squeezed when the housing 100 moves upward, thereby ensuring the performance of the first detection member 930 .

[0239] In some embodiments, as shown in Figure 150, the center rod 300 is provided with a first anti-rotation portion 370, and the housing 100 is provided with an anti-rotation hole 193. The anti-rotation column passes through the anti-rotation hole 193 and extends into the first anti-rotation portion 370 to limit the rotational freedom of the center rod 300 and prevent the center rod 300 and the housing 100 from rotating relative to each other, so that the second detection member 940 located on the center rod 300 can be precisely aligned with the first detection member 930 located on the housing 100, thereby ensuring the detection performance of the detection module 900.

[0240] In some embodiments, the first detection member 930 forms a magnetic field sensing element, and the second detection member 940 forms a magnetic field output element. As shown in FIG155, the second detection member 940 can obtain displacement within a certain range of travel by sensing the magnetic field of the second detection member 940, and the magnetic field signals at any two different positions within the travel are different, such as a linear relationship; as shown in FIG156, the second detection member 940 can sense the magnetic field signal emitted by the first detection member 930, and then convert it into an electrical signal, and the electrical signals at any two different positions within the travel are different, such as a linear relationship. There are many means of conversion here, such as the Hall principle. Finally, the sensed electrical signal (or converted into other signals, such as digital signals) is transmitted as an output signal to achieve the purpose of using the second detection member 940 and the first detection member 930 to cooperate in detecting the relative displacement of the housing 100 and the second component 210.

[0241] In summary, the first detection member 930 mainly detects the relative displacement of the housing 100 and the second component 210 by identifying the magnetic field signal of the second detection member 940. However, the magnetic field intensity emitted by the first component 220 and the second component 210 in the electromagnetic actuator 1000 is very high, which can easily interfere with the detection accuracy of the first detection member 930, resulting in a decrease in the accuracy of the detection module 900 or even failure.

[0242] In order to solve the above problem, the center rod 300 and the housing 100 can be supported by magnetic conductive materials. As shown in Figure 153, the magnetic field generated by the first component 220 and the second component 210 inside the electromagnetic actuator 1000 is distributed along the center rod 300 and the housing 100, and forms a closed magnetic field loop, so that the magnetic field strength at the position of the second detection component 940 is significantly increased, thereby avoiding the magnetic field generated by the first component 220 and the second component 210 inside the electromagnetic actuator 1000 from forming a divergent shape as shown in Figure 154.

[0243] At the same time, the distance between the detection module 900 and the first component 220 and the second component 210 can be increased to improve the magnetic field strength at the position of the second detection component 940, so that the magnetic field strength at the position of the second detection component 940 is significantly increased, thereby ensuring the detection accuracy of the detection module 900.

[0244] In some embodiments, as shown in Figures 159-164 , a mounting bracket 192 is provided at the bottom of the housing 100. A relief passage 1921 communicating with the accommodating chamber 130 is provided within the mounting bracket 192. At least a portion of the second detecting member 940 is located within the relief passage 1921, and the first detecting member 930 can be moved into the relief passage 1921 to couple with the second detecting member 940. This facilitates the use of the second detecting member 940 and the first detecting member 930 to detect relative displacement between the housing 100 and the second component 210, ensuring the accuracy of position detection of the second component 210 and reducing the difficulty of position detection of the second component 210.

[0245] At the same time, by locating at least a portion of the second detection member 940 in the avoidance channel 1921 , it is convenient to reduce the space reserved for the detection module 900 by the electromagnetic actuator 1000 , which is beneficial to the miniaturization design of the electromagnetic actuator 1000 .

[0246] In some embodiments, in combination with Figures 159, 160 and 161, the first detection member 930 includes a sensor connecting end 931, a connecting rod 932 and a sensing head 933. The first detection member 930 is fixed to the center rod 300 through the sensor connecting end 931, and the fixing method can be a bolt connection. The wiring harness of the first detection member 930 is arranged inside the connecting rod 932 and connected to the sensing head 933. The sensing head 933 can sense the magnetic field strength at different areas on the second detection member 940. By analyzing the different magnetic field strengths sensed by the sensing head 933, the relative displacement of the housing 100 and the second component 210 can be determined.

[0247] In some embodiments, at least a portion of the second detection member 940 is attached to the avoidance channel 1921. An adhesive may be used for attachment and fixation.

[0248] In some embodiments, the second detection component 940 is a magnetic scale, which is a device with its own magnetic field. The first detection component 930 is a Hall sensor, which outputs a displacement signal by sensing the changes in the magnetic field on the surface of the magnetic scale, thereby achieving the purpose of detecting the relative displacement between the housing 100 and the second component 210.

[0249] In some embodiments, since both the first component 220 and the second component 210 generate magnetic fields, and when the housing 100 moves upward, as shown in Figures 162 and 163, the second detection component 940 is closer to the first component 220 and the second component 210, the housing 100, the center rod 300, the connecting rod 932 and the mounting bracket 192 are all supported by non-magnetic materials, such as aluminum alloy materials. The use of the above materials can effectively shield the magnetic field generated by the first component 220 and the second component 210 around the first detection component 930 and the second detection component 940, thereby ensuring the detection accuracy of the detection module 900.

[0250] In some embodiments, the coercive force of the second detection member 940 is higher than the coercive force of the first component 220 to ensure that the second detection member 940 is not magnetized by the first component 220 , thereby ensuring the performance of the second detection member 940 .

[0251] In some embodiments, as shown in Figures 164 to 167 , the second detecting member 940 is formed in an arc shape to avoid induction failure between the second detecting member 940 and the first detecting member 930 when the first component 220 and the second component 210 rotate relative to each other, thereby ensuring that the first detecting member 930 can stably sense the magnetic field strength at different positions on the second detecting member 940, thereby ensuring the detection accuracy of the detection module 900.

[0252] The radius of the arc can be adaptively adjusted according to the radius of the housing 100 , and the angle of the arc can be determined according to the limit angle of relative rotation of the first component 220 and the second component 210 .

[0253] In some embodiments, an arc-shaped hole is opened on the mounting bracket 192 , and the first detecting member 930 is disposed in the arc-shaped hole, providing space for the first detecting member 930 to move up and down and rotate in a working state.

[0254] In some embodiments, as shown in Figures 165-167, the detection module 900 includes a second detection member 940, a first detection member 930 and a second sensor mounting bracket 970, wherein the second detection member 940 is a sensor magnetic scale, the first detection member 930 is a sensor reader, and the second sensor mounting bracket 970 is used to install and fix the sensor magnetic scale. The sensor magnetic scale provides a magnetic field, and the sensor reader is used to sense the magnetic field strength at different positions of the magnetic scale to detect the relative displacement of the housing 100 and the second component 210.

[0255] At the same time, the second sensor mounting bracket 970 can be provided to make the detection module 900 more securely fixed, thereby improving the position stability of the detection module 900.

[0256] Among them, the magnetic scale is composed of magnetic strips of different sizes and intervals and adopts a single code channel structure, so that the second detection component 940 is formed into a coded magnetic scale sensor, which is used to provide a non-periodic magnetic field, and enables the sensor reader to sense at the same time that the combined magnetic field of the non-coding area is unique within the entire stroke, thereby determining the absolute position of the first detection component 930 and ensuring the detection accuracy of the detection module 900.

[0257] In some embodiments, the second detection member 940 is made of a strong magnetic material such as neodymium iron boron, so that the second detection member 940 has a higher coercive force, can adapt to a more complex magnetic field environment, and effectively avoid the risk of demagnetization.

[0258] At the same time, by setting the second detection member 940 to adopt a single-channel structure, compared with the dual-channel structure, the width of the second sensor mounting bracket 970 and the size of the read head of the first detection member 930 can be effectively reduced, thereby effectively reducing the layout space of the first detection member 930 and providing more options for the layout position of the first detection member 930.

[0259] In some embodiments, as shown in Figures 168-173 , the outer wall of the housing 100 is provided with a wire groove 194 for guiding the wires of the detection module 900. By providing a wire electrically connected to the detection module 900, the signal detected by the detection module 900 can be transmitted to the controller via the wire. The controller then processes the signal and determines the position of the housing 100, thereby achieving the purpose of using the detection module 900 to detect the movement position of the housing 100.

[0260] At the same time, a wire groove 194 for guiding the wire is provided on the housing 100 to reduce the difficulty of routing the wire. The wire groove 194 can also be used to fix the wire to ensure the position stability of the wire and prevent the wire from bending as the housing 100 moves, thereby affecting the transmission of the signal. This improves the reliability of the electromagnetic actuator 1000, and can realize the use of the wire groove 194 to protect the wire, extend the service life of the wire, improve the safety of the wire, and improve the reliability of the wire.

[0261] It should be noted that the length of the wire groove 194 can be set according to the position of the external connector, and the depth of the wire groove 194 can be set according to the radial size of the wire and the structural strength of the housing 210, which is not limited here.

[0262] Optionally, the wire trough 194 is integrally formed with the housing 100. That is, the wire trough 194 is integrally formed on the housing 100 to reduce the difficulty of forming the wire trough 194.

[0263] In some embodiments, as shown in Figures 168, 169, and 170, the outer peripheral wall of the housing 100 is provided with a plurality of second reinforcing ribs 195, and a wire groove 194 is defined between at least two adjacent second reinforcing ribs 195, thereby reducing the difficulty of forming the wire groove 194.

[0264] At the same time, by providing a plurality of second reinforcing ribs 195 on the outer peripheral wall of the housing 100, the structural strength of the housing 100 can be improved, the service life of the housing 100 can be extended, and the wall thickness of the housing 100 can be reduced accordingly to achieve the purpose of lightweighting.

[0265] In some embodiments, as shown in Figures 168 and 169, the outer peripheral wall of the casing 100 is provided with a plurality of second reinforcing ribs 195, at least a portion of the second reinforcing ribs 195 extend along the radial direction of the casing 100, and at least a portion of the second reinforcing ribs 195 extend along the axial direction of the casing 100, so that the casing 100 is provided with a plurality of second reinforcing ribs 195 that are evenly arranged vertically and laterally. This uniformly distributed structural feature is beneficial to the processing technology design of the casing 100.

[0266] The second reinforcing ribs 195 extending along the radial direction of the housing 100 are mainly used to strengthen the bending rigidity of the housing 100 , and the second reinforcing ribs 195 extending along the axial direction of the housing 100 are mainly used to strengthen the compressive strength of the motor housing 5 .

[0267] At the same time, oblique reinforcement ribs may be provided on the outer peripheral wall of the housing 100 to avoid stress concentration.

[0268] In some embodiments, as shown in Figures 168 and 169, the lower end of the mounting seat 191 is designed with a triangular vertical reinforcement rib, which utilizes the principle of triangular structural stability to make the mounting seat 191 structure more stable, able to withstand greater spring force, and improve the compressive strength of the mounting seat 191.

[0269] In some embodiments, a second reinforcing rib 195 extending along the axial direction of the housing 100 is further arranged between two adjacent triangular vertical reinforcing ribs to improve the bending stiffness of the mounting base 191 .

[0270] In some embodiments, a wire avoidance structure is provided between the mounting base 191 and the housing 100 , so that the wires can pass through the mounting base 191 and be arranged in the wire groove 194 .

[0271] In some embodiments, the wire groove 194 is formed as a heat dissipation structure to dissipate heat from the electromagnetic actuator 1000 and ensure the performance of the electromagnetic actuator 1000 .

[0272] In some embodiments, the second reinforcing ribs 195 can be used to expand the heat dissipation area of ​​the housing 100, eliminating the need for an external heat dissipation cavity to assist in heat dissipation, reducing the complexity of the mechanism, increasing the degree of freedom of overall layout design, and achieving the purpose of lightweighting.

[0273] The depth and width of the second reinforcing rib 195 can be changed according to the diameter of the wire and the strength of the housing 100 .

[0274] In some embodiments, as shown in FIG. 1 , FIG. 2 , and FIG. 3 , the housing 100 includes a plurality of sub-housings 101 , which are connected to define an accommodating cavity 130 .

[0275] It should be noted that, in the description of this application, unless otherwise specified, "multiple" means two or more, that is, the housing 100 includes at least two sub-housings 101, and at least two sub-housings 101 are connected to define a accommodating cavity 130. This reduces the difficulty of assembling the housing 100 while also reducing the difficulty of molding the accommodating cavity 130, thereby improving maintainability.

[0276] As shown in Figures 1 to 4 , the first component 220 is disposed within the accommodating cavity 130, and the second component 210 is disposed within the accommodating cavity 130, with one of the first component 220 and the second component 210 being connected to the housing 100. That is, since both the first component 220 and the second component 210 are disposed within the accommodating cavity 130, the housing 100 can be used to support one of the first component 220 and the second component 210, thereby improving the positional stability of one of the first component 220 and the second component 210 and ensuring the working performance of the first component 220 and the second component 210 to a certain extent. Furthermore, the housing 100 can be used to protect the first component 220 and the second component 210, thereby extending the service life of the first component 220 and the second component 210 and reducing the cost of using the first component 220 and the second component 210.

[0277] It can be understood that one of the first component 220 and the second component 210 being connected to the housing 100 means that one of the first component 220 and the second component 210 is fixedly connected to the housing 100 .

[0278] At the same time, by configuring the housing 100 to include multiple sub-housings 101, the housing 100 is composed of multiple separate parts. In this way, when assembling the first component 220 and the second component 210, the first component 220 and the second component 210 can be first placed between the multiple sub-housings 101, and then the multiple sub-housings 101 can be connected to reduce the difficulty of assembling the first component 220 and the second component 210, improve the assembly effect, and to a certain extent avoid the first component 220 and the second component 210 from colliding with the housing 100 during the assembly process, thereby avoiding damage to the first component 220 and the second component 210, thereby extending the service life of the first component 220 and the second component 210 and ensuring the working performance of the first component 220 and the second component 210.

[0279] In addition, through the above arrangement, when the first component 220 and the second component 210 need to be maintained or repaired, the housing 100 can be directly opened to reduce the difficulty of maintaining the first component 220 and the second component 210 during use.

[0280] The first assembly 220 and the second assembly 210 are coupled so that the other of the first assembly 220 and the second assembly 210 and the housing 100 move along the axis, thereby driving the component of the first assembly 220 and the second assembly 210 connected to the housing 100 to move along the axis. The axis here can be understood as a straight line extending along the axial direction of the electromagnetic actuator 1000, that is, a straight line extending in the vertical direction in Figure 2.

[0281] That is to say, one of the first component 220 and the second component 210 is connected to the housing 100. When the first component 220 and the second component 210 are coupled, one of the first component 220 and the second component 210 moves along the axis together with the housing 100, thereby realizing the movement of the housing 100 and ensuring the working performance of the electromagnetic actuator 1000.

[0282] In some embodiments, one of the first component 220 and the second component 210 is a permanent magnet or an electromagnet, and the other is an electromagnetic coil. The electromagnetic coil cooperates with the permanent magnet to enable the first component 220 and the second component 210 to form a coupling, thereby improving the working performance of the electromagnetic actuator 1000. In other words, the first component 220 is the first excitation component, and the second component is the second excitation component.

[0283] It can be seen from the above structure that the electromagnetic actuator 1000 of the embodiment of the present application, by configuring the housing 100 to include multiple sub-housings 101, and the multiple sub-housings 101 are connected to define a accommodating cavity 130, can reduce the difficulty of assembling the housing 100 while also reducing the difficulty of assembling and maintaining the first component 220 and the second component 210, and at the same time avoid the first component 220 and the second component 210 from colliding with the housing 100 during the assembly process, thereby ensuring the working performance of the first component 220 and the second component 210.

[0284] It can be understood that compared with the prior art, the present application configures the casing 100 to include multiple sub-shells 101, thereby reducing the difficulty of assembling the first component 220 and the second component 210 arranged in the accommodating cavity 130, and the multiple sub-shells 101 are also conducive to reducing the difficulty of assembling the casing 100 itself, so that the first component 220 and the second component 210 can be effectively assembled in the casing 100, and to a certain extent avoid the first component 220 and the second component 210 from colliding with the casing 100 during the assembly process, thereby ensuring the working performance of the first component 220 and the second component 210.

[0285] In some embodiments, as shown in Figures 1 and 2 , multiple sub-housings 101 are arranged along an axis. That is, the multiple sub-housings 101 are arranged along the axial direction of the electromagnetic actuator 1000. This allows the housing 100 to be formed into multiple structures arranged along the axial direction of the electromagnetic actuator 1000, reducing the difficulty of molding the housing 100 and easing the difficulty of assembling the first component 220 and the second component 210 disposed within the housing 100, thereby improving the assembly efficiency of the electromagnetic actuator 1000.

[0286] In some embodiments, as shown in FIG2 , FIG3 and FIG4 , a plurality of sub-housings 101 include a cylinder 1011 with at least one open end and at least one end cap 1012 , and the end cap 1012 cooperates with the cylinder 1011 to form the housing 100 , thereby reducing the difficulty of molding the housing 100 .

[0287] By opening at least one end of the cylinder 1011 , the first component 220 and the second component 210 can be easily assembled into the cylinder 1011 .

[0288] At the same time, the inner surface accuracy of the cylinder 1011 and the surface accuracy of the first component 220 must be strictly controlled to ensure that the air gap between the first component 220 and the second component 210 is uniform, thereby ensuring the working performance of the electromagnetic actuator 1000.

[0289] In some embodiments, as shown in FIG2 , the lower end of the end cover 1012 is integrated with a mounting bracket 192 , which is suitable for connecting to the axle, thereby simplifying the connection method between the electromagnetic actuator 1000 and the axle, improving structural reliability, and reducing the assembly process and assembly time of the electromagnetic actuator 1000 .

[0290] The mounting bracket 192 mentioned here can be understood as the lower fork arm of the electromagnetic actuator 1000 .

[0291] In some embodiments, as shown in FIG. 2 , FIG. 3 and FIG. 4 , the end cover 1012 is provided at the opening of the cylinder 1011 to ensure the sealing of the accommodating cavity 130 .

[0292] In some embodiments, as shown in Figures 2, 3, and 4, the end cap 1012 is plugged into the cylinder 1011. This allows the end cap 1012 to be positioned at the opening of the cylinder 1011 while also providing a fixed connection between the end cap 1012 and the cylinder 1011, thereby ensuring the structural stability of the housing 100 and reducing the difficulty of molding the housing 100.

[0293] In some embodiments, as shown in FIG4 , one of the top wall of the end cap 1012 and the lower end of the barrel 1011 is provided with a slot 1013 and the other is provided with an inserting portion 1014 , which extends into the slot 1013 to achieve plug-in fit between the end cap 1012 and the barrel 1011 .

[0294] In some embodiments, as shown in FIG4 , the end cover 1012 is connected to the cylinder 1011 by bolts 1016. This achieves a fixed connection between the end cover 1012 and the cylinder 1011, ensures the connection strength between the end cover 1012 and the cylinder 1011, and simultaneously enables a detachable connection between the end cover 1012 and the cylinder 1011, thereby ensuring the structural stability and working performance of the housing 100.

[0295] In some embodiments, as shown in FIG. 4 , the end cap 1012 and the cylinder 1011 are positioned by positioning pins 1017 , thereby positioning the installation direction of the end cap 1012 , preventing mis-installation, and reducing the difficulty of connecting the end cap 1012 and the cylinder 1011 .

[0296] In some embodiments, an end cover connecting boss protruding radially outward is provided on the outer peripheral wall of the end cover 1012, and a corresponding cylinder connecting boss is provided on the cylinder 1011. Both the end cover connecting boss and the cylinder connecting boss are provided with connecting holes, and fasteners or bolts are passed through the connecting holes to achieve a fixed connection between the end cover 1012 and the cylinder 1011. The connection is achieved through the connecting boss, which can improve the cavity of the end cover 1012 and the cylinder 1011 while also improving the stability of the connection.

[0297] It should be noted that the specifications and quantity of the bolts 1016 and the positioning pins 1017 can be reasonably designed according to the actual mechanical strength requirements.

[0298] In some embodiments, as shown in Figures 2, 3, and 4, a guide rod 400 is provided on the end cover 1012. The guide rod 400 movably cooperates with the other of the first component 220 and the second component 210 to guide the movement direction of the housing 100 and one of the first component 220 and the second component 210. In other words, one of the first component 220 and the second component 210 is fixedly connected to the housing 100, and the other of the first component 220 and the second component 210 movably cooperates with the guide rod 400, thereby preventing the housing 100 from deflecting during movement, that is, ensuring that the housing 100 can move in a predetermined direction and ensuring the accuracy of the movement of the housing 100.

[0299] Through the above configuration, when the electromagnetic actuator 1000 is applied to the vehicle 20000 , the wheel 2000 can be moved in a predetermined direction, thereby ensuring the stability of the vehicle 20000 during driving.

[0300] In some embodiments, as shown in FIG. 2 , FIG. 3 and FIG. 4 , a guide bearing 840 is provided between the guide rod 400 and the other of the first component 220 and the second component 210 .

[0301] In some embodiments, the first component 220 is fixedly connected to the housing 100, and the guide rod 400 moves and cooperates with the second component 210 to guide the movement direction of the housing 100. The verticality and concentricity of the lower end of the second component 210 are determined by the guide rod 400 and the guide bearing 840.

[0302] In some embodiments, as shown in Figure 2, a bearing mounting slot is opened at the upper end of the cylinder 1011 for assembling the bearing 170. The bearing 170 serves to position the upper end of the second component 210. The verticality and concentricity of the upper end of the second component 210 are determined by the top surface of the cylinder 1011 and the bearing 170.

[0303] In summary, the electromagnetic actuator 1000 in this embodiment mainly consists of a bearing 170 , a cylinder 1011 , a first component 220 , a second component 210 , a guide bearing 840 , and an end cover 1012 . Among them, the first component 220 is attached to the inside of the cylinder 1011, and the bearing 170, the cylinder 1011, the end cover 1012 and the first component 220 constitute the mover part of the electromagnetic actuator 1000. The inside of the second component 210 is a coil winding. When three-phase electricity is passed through, a moving magnetic field will be formed. The magnetic field acts on the mover part. The second component 210 and the first component 220 generate an interaction force to make the casing 100 move up and down. Finally, the electromagnetic actuator 1000 realizes linear motion, and the linear motion of the casing 100 is controlled by adjusting the size and direction of the three-phase electricity to achieve the actual required motion state. In addition, this embodiment solves the problems of installation of the first component 220 and the second component 210, assembly of the mounting bracket 192, and movement and positioning of the casing 100 by reasonably designing the structure between the end cover 1012 and the cylinder 1011.

[0304] In a specific example, when assembling the electromagnetic actuator 1000, the first step is to install the first component 220 from the bottom of the cylinder 1011 into the inner surface of the cylinder 1011, the second step is to assemble the bearing 170 with the top surface of the cylinder 1011, and the third step is to put the guide bearing 840 into the mounting hole on the lower end surface of the second component 210. Then, the second component 210 is installed from the bottom of the cylinder 1011, and the upper end of the second component 210 is inserted into the bearing 170. Finally, the end cover 1 is installed. 012 is installed from the lower end of the cylinder 1011 upwards, the guide rod 400 is inserted into the guide bearing 840, the extension part 1014 is extended into the slot 1013, the end cover 1012 and the cylinder 1011 are connected by the bolt 1016 and the positioning pin 1017, and the housing 100 is pushed and pulled to check whether the housing 100 moves smoothly. If not, check whether the guide rod 400 is assembled in place and whether the machined dimensions of each part exceed the standard. Finally, power on the electromagnetic actuator 1000 to see if the movement is normal.

[0305] It is worth noting that the electromagnetic actuator 1000 of this embodiment adopts a split design structure for the cylinder 1011 and the end cover 1012, which facilitates the installation of the second component 210 and the first component 220; by integrating the end cover 1012, the guide rod 400 and the mounting bracket 192 into an integrated design, the connection method between the various parts of the electromagnetic actuator 1000 is simplified, the assembly process and assembly time are reduced, the structural reliability is improved, and the weight is reduced; by integrating the guide rod 400 in the end cover 1012 and designing an extension portion 1014 on the top surface of the end cover 1012 to cooperate with the inner surface of the cylinder 1011 for installation, it can be ensured that the center of the guide rod 400 and the cylinder 1011 coincide, thereby ensuring that the air gap between the second component 210 and the first component 220 is uniform; by adding a positioning pin 1017 between the end cover 1012 and the cylinder 1011, it is used to locate the installation direction of the end cover 1012 to prevent misinstallation.

[0306] In some embodiments, as shown in Figures 5, 6, and 8, multiple sub-housings 101 are arranged circumferentially, with the circumference being approximately perpendicular to the axis. That is, the multiple sub-housings 101 are not limited to being arranged along the axis of the electromagnetic actuator 1000, but can also be arranged circumferentially of the electromagnetic actuator 1000. This can also reduce the difficulty of assembling the housing 100, as well as the difficulty of assembling and maintaining the first and second assemblies 220, 210, thereby preventing the first and second assemblies 220, 210 from colliding with the housing 100 during assembly and ensuring the operating performance of the first and second assemblies 220, 210.

[0307] In some embodiments, as shown in Figures 9, 10, 11, and 12, the plurality of sub-housings 101 include a first sub-housing 110 and a second sub-housing 120. The first sub-housing 110 is formed with a first cavity 115, and the second sub-housing 120 is formed with a second cavity 125. The first sub-housing 110 and the second sub-housing 120 are disposed relative to each other so that the first cavity 115 and the second cavity 125 together form a receiving cavity 130. This reduces the difficulty of molding the receiving cavity 130 and facilitates the placement of the first component 220 and the second component 210 within the receiving cavity 130.

[0308] In some embodiments, as shown in Figures 6 and 8, the first sub-housing 110 and the second sub-housing 120 are rotatably connected. This means that the first sub-housing 110 and the second sub-housing 120 are not only connected but also rotatable relative to each other. In this way, during the assembly process of the first sub-housing 110 and the second sub-housing 120, the first sub-housing 110 and the second sub-housing 120 can be first rotatably connected. After the connection is in place, at least one of the first sub-housing 110 and the second sub-housing 120 can be rotated to form the housing 100, thereby reducing the difficulty of assembling the housing 100.

[0309] That is to say, the casing 100 of this embodiment is divided into two parts (a first sub-shell 110 and a second sub-shell 120) along its circumference, and the two parts are rotatably connected, so that the first sub-shell 110 and the second sub-shell 120 can rotate around the rotation connection point to open or close the casing 100, reducing the difficulty of opening and closing the casing 100.

[0310] Among them, when the first sub-shell 110 and the second sub-shell 120 are rotated to fully open the interior of the casing 100, on the one hand, it is convenient to assemble the first component 220 and the second component 210, and on the other hand, it is also convenient to maintain the first component 220 and the second component 210. At the same time, it can also avoid, to a certain extent, the first component 220 and the second component 210 from colliding with the casing 100 during the assembly process; when the first sub-shell 110 and the second sub-shell 120 are rotated to fully close the interior of the casing 100, the casing 100 can be used to support and protect the first component 220 and the second component 210.

[0311] It should be noted that when the casing 100 is formed into a cylindrical shell, the above-mentioned setting can realize the separation of the casing 100 into a first sub-shell 110 and a second sub-shell 120 in the radial direction of the casing 100, so as to reduce the difficulty of assembling the casing 100 and reduce the difficulty of matching the first component 220 and the second component 210 with the casing 100.

[0312] In some embodiments, as shown in Figures 9, 10, 11, and 12, the first sub-housing 110 is provided with a first connecting portion 111 protruding therefrom, and the second sub-housing 120 is provided with a second connecting portion 121 protruding therefrom, and the first connecting portion 111 and the second connecting portion 121 are rotatably connected. This means that the first sub-housing 110 is provided with a first connecting portion 111 and the first connecting portion 111 protrudes from the first sub-housing 110, and the second sub-housing 120 is provided with a second connecting portion 121 and the second connecting portion 121 protrudes from the second sub-housing 120. This facilitates the rotational connection between the first connecting portion 111 and the second connecting portion 121, thereby reducing the difficulty of connecting the first connecting portion 111 and the second connecting portion 121.

[0313] At the same time, after the first connecting portion 111 and the second connecting portion 121 are rotationally connected, the first sub-shell 110 and the second sub-shell 120 can be rotationally connected. In this way, during the assembly process of the second sub-shell 120 and the first sub-shell 110, the second sub-shell 120 and the first sub-shell 110 can be first rotationally connected. After the connection is in place, at least one of the second sub-shell 120 and the first sub-shell 110 can be rotated to form the housing 100, thereby reducing the difficulty of assembling the housing 100.

[0314] In some embodiments, as shown in FIG5 and FIG6 , the electromagnetic actuator 1000 further includes a rotating shaft 140. Both the first sub-housing 110 and the second sub-housing 120 are provided with shaft holes, and the rotating shaft 140 is disposed in the shaft holes to enable relative movement between the first sub-housing 110 and the second sub-housing 120. This achieves a rotational connection between the first sub-housing 110 and the second sub-housing 120 and reduces the difficulty of connecting the first sub-housing 110 and the second sub-housing 120.

[0315] In some embodiments, in combination with Figures 5-12, the first connecting portion 111 includes a plurality of first connecting lugs 1111, and the plurality of first connecting lugs 1111 are arranged at intervals. The second connecting portion 121 includes a plurality of second connecting lugs 1211, and the plurality of second connecting lugs 1211 are arranged at intervals. The plurality of first connecting lugs 1111 and the plurality of second connecting lugs 1211 are staggered. The first connecting lug 1111 is provided with a first connecting hole 1112, and the second connecting lug 1211 is provided with a second connecting hole 1212. The rotating shaft 140 is used to penetrate the plurality of first connecting holes 1112 and the plurality of second connecting holes 1212, so as to facilitate the use of the rotating shaft 140 to realize the rotational connection between the first connecting lug 1111 and the second connecting lug 1211, that is, to realize the rotational connection between the first sub-shell 110 and the second sub-shell 120.

[0316] 5 , so that the first connecting lugs 1111 and the second connecting lugs 1211 are not arranged opposite each other, so that the multiple first connecting lugs 1111 and the multiple second connecting lugs 1211 are staggered. In this way, after the first sub-shell 110 and the second sub-shell 120 are rotated and docked, the first connecting lugs 1111 and the second connecting lugs 1211 can be arranged opposite each other in the front-to-back direction of the casing 100. The front-to-back direction here intersects with the up-down direction and the left-to-right direction in FIG. 5 , so that the rotating shaft 140 can simultaneously pass through the multiple first connecting lugs 1111 and the multiple second connecting lugs 1211, so as to facilitate the use of the rotating shaft 140 to realize the connection between the multiple first connecting lugs 1111 and the multiple second connecting lugs 1211, that is, to realize the rotational connection of the first connecting portion 111 and the second connecting portion 121.

[0317] Among them, the left and right directions shown in Figure 5 can also be understood as the docking direction of the first sub-shell 110 and the second sub-shell 120. That is, during the docking process of the first sub-shell 110 and the second sub-shell 120, the multiple first connecting lugs 1111 and the multiple second connecting lugs 1211 are staggered, so that after the docking process of the first sub-shell 110 and the second sub-shell 120, the first connecting lugs 1111 and the second connecting lugs 1211 can be arranged opposite each other in the front-to-back direction of the casing 100. It can be understood that at this time, the axial holes on the first sub-shell 110 and the second sub-shell 120 are arranged opposite each other in the front-to-back direction.

[0318] In summary, the casing 100 of this embodiment is divided into two parts along its circumference, and the first sub-shell 110 and the second sub-shell 120 are connected by using the rotating shaft 140, the first connecting part 111 and the second connecting part 121, so that the first sub-shell 110 and the second sub-shell 120 can be rotated around the rotating shaft 140 to open or close the casing 100, so that the interior of the casing 100 can be completely opened, which is conducive to the positioning, installation, fixation, maintenance, etc. of the first component 220 and the second component 210 in the casing 100, and relative to the end opening of the casing 100, it can also prevent the first component 220 and the second component 210 from colliding with the casing 100 during the assembly process.

[0319] In some embodiments, as shown in FIG6 , an end portion of the first sub-housing 110 is rotatably connected to an end portion of the second sub-housing 120 in the axial direction of the housing 100. In other words, one axial end of the first sub-housing 110 is rotatably connected to one axial end of the second sub-housing 120, thereby achieving rotational coordination between the first sub-housing 110 and the second sub-housing 120 and reducing the difficulty of assembling the first sub-housing 110 and the second sub-housing 120.

[0320] In some embodiments, as shown in Figures 9, 10, 11 and 12, the first connecting portion 111 is provided at one axial end of the first sub-shell 110, and the second connecting portion 121 is provided at one axial end of the second sub-shell 120. In this way, after the first connecting portion 111 and the second connecting portion 121 are rotationally connected, the first sub-shell 110 and the second sub-shell 120 can be rotated together, and the end of the first sub-shell 110 and the end of the second sub-shell 120 can be rotationally connected.

[0321] Through the above arrangement, during the assembly of the casing 100, one end of the first sub-shell 110 and one end of the second sub-shell 120 can be first rotatably connected. After the connections are in place, the first component 220 and the second component 210 are assembled between the first sub-shell 110 and the second sub-shell 120 (as shown in Figure 6), and then the other end of the first sub-shell 110 and the other end of the second sub-shell 120 are driven to rotate toward each other to achieve the mating connection between the first sub-shell 110 and the second sub-shell 120.

[0322] In other embodiments, as shown in FIG8 , one side of the first sub-housing 110 and one side of the second sub-housing 120 are rotatably connected in the circumferential direction of the housing 100. In other words, the rotatable connection is not limited to the end of the first sub-housing 110 and the end of the second sub-housing 120. Alternatively, one side of the first sub-housing 110 and one side of the second sub-housing 120 may be rotatably connected in the circumferential direction of the housing 100. This also allows for rotatable coordination between the first sub-housing 110 and the second sub-housing 120, thereby reducing the difficulty of assembling the first sub-housing 110 and the second sub-housing 120.

[0323] In some embodiments, as shown in Figure 8, the first connecting portion 111 is provided on one side of the first sub-shell 110 in the circumferential direction, and the second connecting portion 121 is provided on one side of the second sub-shell 120 in the circumferential direction. In this way, after the first connecting portion 111 and the second connecting portion 121 are rotationally connected, the first sub-shell 110 and the second sub-shell 120 can be rotated together, and one side of the first sub-shell 110 and one side of the second sub-shell 120 can be rotationally connected.

[0324] Through the above-mentioned arrangement, as shown in Figure 8, during the assembly of the casing 100, one side of the first sub-shell 110 in the circumferential direction and one side of the second sub-shell 120 in the circumferential direction can be first rotationally connected. After the connection is in place, the first component 220 and the second component 210 are assembled between the first sub-shell 110 and the second sub-shell 120, and then the other side of the first sub-shell 110 in the circumferential direction and the other side of the second sub-shell 120 in the circumferential direction are driven to rotate toward each other to achieve the mating connection between the first sub-shell 110 and the second sub-shell 120.

[0325] In some embodiments, the first sub-housing 110 and the second sub-housing 120 are detachably coupled. That is, the first sub-housing 110 and the second sub-housing 120 are not only rotatably connected but also detachably coupled. This allows for a fixed connection between the first sub-housing 110 and the second sub-housing 120, thereby ensuring a stable relative position of the first sub-housing 110 and the second sub-housing 120, thereby ensuring the positional stability of the housing 100, facilitating the use of the housing 100 to support and protect the first component 220 and the second component 210, thereby extending the service life of the first component 220 and the second component 210 and improving the positional stability of the first component 220 and the second component 210.

[0326] At the same time, by setting the first sub-shell 110 and the second sub-shell 120 to be detachable, the difficulty of assembling and disassembling the first sub-shell 110 and the second sub-shell 120 is reduced, and the difficulty of assembling and disassembling the casing 100 is reduced, making it easier to maintain the first component 220 and the second component 210.

[0327] In some embodiments, as shown in Figure 6, one of the first sub-shell 110 and the second sub-shell 120 is provided with a third connecting portion 112, and the other is provided with a fourth connecting portion 122 facing the third connecting portion 112, and a first fastener 150 connects the third connecting portion 112 and the fourth connecting portion 122 to make the first sub-shell 110 and the second sub-shell 120 detachable. What this means is that when the first sub-shell 110 is provided with a third connecting portion 112, the second sub-shell 120 is provided with a fourth connecting portion 122; when the second sub-shell 120 is provided with a third connecting portion 112, the first sub-shell 110 is provided with a fourth connecting portion 122. In this way, when the first fastener 150 is connected to the third connecting portion 112 and the fourth connecting portion 122, the first sub-shell 110 and the second sub-shell 120 can be detachably matched. While achieving a fixed connection between the first sub-shell 110 and the second sub-shell 120, the relative positions of the first sub-shell 110 and the second sub-shell 120 can also be stabilized, thereby ensuring the positional stability of the casing 100 and reducing the difficulty of assembling the casing 100.

[0328] In some embodiments, in combination with Figures 9, 10 and 12, a third connection hole 1121 is provided on the third connection portion 112, and a fourth connection hole 1221 is provided on the fourth connection portion 122. The first fastener 150 connects the third connection hole 1121 and the fourth connection hole 1221, thereby achieving a fixed connection between the third connection portion 112 and the fourth connection portion 122.

[0329] Alternatively, the first fastener 150 may be a fastening bolt, a fastening screw, or a rivet.

[0330] Optionally, in combination with Figures 5, 6 and 8, the first sub-shell 110 is provided with a plurality of third connecting parts 112, and the plurality of third connecting parts 112 are respectively located on the side walls and end walls of the first sub-shell 110, and the second sub-shell 120 is provided with a plurality of fourth connecting parts 122 facing the third connecting parts 112. In this way, when the first fastener 150 connects the third connecting parts 112 and the fourth connecting parts 122, the side walls and end walls of the first sub-shell 110 and the second sub-shell 120 can be detachably matched to improve the connection strength of the first sub-shell 110 and the second sub-shell 120, thereby stabilizing the relative positions of the first sub-shell 110 and the second sub-shell 120.

[0331] In some embodiments, as shown in FIG. 7 , the housing 100 is provided with a first avoidance through hole 160 , which is connected to the accommodating cavity 130 . The first avoidance through hole 160 is suitable for avoiding the center rod 300 , and a cylindrical bearing 170 is provided in the first avoidance through hole 160 . Among them, by setting a first avoidance through hole 160 that avoids the center rod 300 and connects to the accommodating cavity 130, it can be ensured that the center rod 300 can extend into the accommodating cavity 130 through the first avoidance through hole 160; by setting a cylindrical bearing 170 in the first avoidance through hole 160, when the center rod 300 moves relative to the accommodating cavity 130, the bearing 170 can be used to guide the center rod 300 to ensure the position accuracy of the center rod 300 when it moves, and at the same time, it can also avoid the center rod 300 from contacting the hole wall of the first avoidance through hole 160 during the movement, thereby avoiding interference between the center rod 300 and the hole wall of the first avoidance through hole 160, so that the center rod 300 can accurately move relative to the accommodating cavity 130.

[0332] At the same time, by providing the bearing 170 , it is more conducive to ensuring that the air gap between the permanent magnet and the coil is maintained within a reasonable designed range, ensuring the stability of the system structure and improving the system's ability to resist side suction.

[0333] It should be noted that, since the first avoidance through hole 160 is formed on the housing 100, technical problems such as low smoothness of the hole wall of the first avoidance through hole 160 and poor position accuracy of the first avoidance through hole 160 may easily occur during the processing of the first avoidance through hole 160. At this time, if the center rod 300 is directly matched with the first avoidance through hole 160, the center rod 300 may easily interfere with the first avoidance through hole 160 during the movement. Therefore, in this embodiment, a cylindrical bearing 170 is provided in the first avoidance through hole 160. In this way, while the bearing 170 is used to guide the center rod 300, it can also avoid interference between the center rod 300 and the hole wall of the first avoidance through hole 160 during the movement, so as to ensure the position accuracy of the center rod 300 during the movement.

[0334] It should also be noted that the aforementioned movement of the central rod 300 relative to the accommodating cavity 130 may be movement or rotation.

[0335] Optionally, the bearing 170 is detachably disposed in the first avoidance through hole 160 , which facilitates separate processing of the bearing 170 to ensure the structural accuracy of the bearing 170 , thereby ensuring the guiding performance of the bearing 170 .

[0336] In some embodiments, as shown in Figures 15 and 16, a protrusion 171 is provided on the outer periphery of the bearing 170, and the protrusion 171 is fitted and connected in the first avoidance through hole 160 to achieve the fitting connection between the bearing 170 and the first avoidance through hole 160, thereby facilitating the use of the bearing 170 to guide the center rod 300, and making the structure of the bearing 170 simple and easy to install, and at the same time, there is no need to add an additional installation and fixing structure to fix the bearing 170.

[0337] In some embodiments, as shown in Figures 6 and 14, a second component 210 is provided on the center rod 300, so that when the center rod 300 is extended into the accommodating cavity 130, the second component 210 can be arranged in the accommodating cavity 130, so that the second component 210 can cooperate with the first component 220, thereby ensuring the working performance of the electromagnetic actuator 1000.

[0338] At the same time, by setting the second component 210 on the center rod 300 and setting the first component 220 on the casing 100, an electromagnetic solution can be formed in which the permanent magnet is placed outside and the coil component is placed inside. Under the constraints of limited space, a larger air gap diameter can be obtained, thereby providing greater active thrust.

[0339] It should be noted that, since the casing 100 of this embodiment is divided into a first sub-shell 110 and a second sub-shell 120 along its circumference, when the casing 100 is used on the electromagnetic actuator 1000, since the second component 210 needs to be divided into two halves when it is arranged on the first sub-shell 110 and the second sub-shell 120, magnetic flux lines cannot be generated. Therefore, when the casing 100 is used on the electromagnetic actuator 1000, the second component 210 is arranged on the center rod 300, and the first component 220 is arranged on the first sub-shell 110 and the second sub-shell 120 and divided into two parts; when the casing 100 is used on a rotating motor, since the directions of the second component 210 are different, the second component 210 can be arranged on the first sub-shell 110 and the second sub-shell 120 and divided into two parts, or it can be arranged on the center rod 300.

[0340] In some embodiments, as shown in Figures 6, 9, and 11, the first sub-housing 110 is provided with a first avoidance groove 113, and the second sub-housing 120 is provided with a second avoidance groove 123. The first avoidance groove 113 and the second avoidance groove 123 cooperate to define a first avoidance through-hole 160. This not only forms the first avoidance through-hole 160 in communication with the accommodating cavity 130 on the housing 100, but also reduces the difficulty of forming the first avoidance through-hole 160 and the difficulty of fitting the bearing 170 and the center rod 300 with the first avoidance through-hole 160, thereby improving the assembly efficiency of the housing 100.

[0341] At the same time, the above arrangement can also facilitate the assembly of the second component 210 on the central rod 300 into the accommodating cavity 130 .

[0342] In summary, it can be understood that after the housing 100 is divided into the first sub-housing 110 and the second sub-housing 120 along its circumferential direction, the center dividing plane of the housing 100 is a plane passing through the axis of the bearing 170 .

[0343] It should be noted that, for a cylindrical motor housing, the center dividing surface can divide the cylindrical motor housing into two symmetrical parts; for motor housings of other shapes (such as square, pentagonal, etc.), the center dividing surface can divide the housing 100 into two asymmetrical parts.

[0344] That is, when the housing 100 is formed into a cylindrical motor housing, the first sub-housing 110 and the second sub-housing 120 are generally structurally symmetrical; when the housing 100 is formed into a motor housing of other shapes, the first sub-housing 110 and the second sub-housing 120 are generally structurally asymmetrical.

[0345] In some embodiments, as shown in Figures 6 and 7, the housing 100 further includes a guide rod 400, and the other of the first component 220 and the second component 210 cooperates with the guide rod 400. This prevents the first component 220 and the other of the second component 210 from deviating during movement, that is, ensures that the first component 220 and the other of the second component 210 can move relative to each other in a predetermined direction, ensures the accuracy of the movement of the first component 220 and the other of the second component 210, and thus, to a certain extent, ensures that the relative axial distance between the housing 100 and the first component 220 and the other of the second component 210 remains unchanged during their relative movement.

[0346] In some embodiments, as shown in Figure 7, a guide hole 310 is provided at one end of the center rod 300 located in the accommodating cavity 130, and the guide rod 400 is movably matched with the guide hole 310 so that the guide rod 400 can be used to guide the moving direction of the center rod 300 to ensure the accuracy of the movement of the center rod 300.

[0347] In some embodiments, as shown in FIG7 , the guide rod 400 is disposed on the rotating shaft 140. This means that when the end of the first sub-housing 110 and the end of the second sub-housing 120 are rotatably connected, the guide rod 400 is disposed on the rotating shaft 140 to achieve a fixed connection between the end of the guide rod 400 and the housing 100, thereby reducing the difficulty of fitting the guide rod 400 and the housing 100, thereby facilitating the use of the housing 100 to support the guide rod 400 and improving the positional stability of the guide rod 400.

[0348] In some embodiments, as shown in FIG7 and FIG13 , the guide rod 400 is provided with a through hole 411 , and the rotating shaft 140 is passed through the through hole 411 , thereby achieving the arrangement of the guide rod 400 on the rotating shaft 140 .

[0349] In some embodiments, as shown in FIG. 13 , a mounting boss 410 is provided at the end of the guide rod 400 , a through hole 411 is provided on the mounting boss 410 , and the rotating shaft 140 passes through the through hole 411 to achieve a mating connection between the rotating shaft 140 and the guide rod 400 .

[0350] In summary, the first sub-shell 110, the second sub-shell 120 and the guide rod 400 of this embodiment are connected together by the rotating shaft 140, and the three can rotate relative to each other around the rotating shaft 140. When the housing 100 is specifically assembled, the rotating shaft 140 is first passed through the multiple first connecting lugs 1111, the multiple second connecting lugs 1211 and the end of the guide rod 400 in sequence to achieve the rotational cooperation of the first sub-shell 110, the second sub-shell 120 and the guide rod 400, and then the bearing 170 is sleeved on the center rod 300, and the center rod 300 is sleeved on the guide rod 400, and then the guide rod 400, the bearing 170 and the center rod 300 are rotated around the rotating shaft 140 so that they are close to one of the first sub-shell 110 or the second sub-shell 120. And ensure that the bearing 170 fits in the third avoidance groove 114 or the fourth avoidance groove 124, and then control the other of the first sub-shell 110 or the second sub-shell 120 to rotate around the rotating shaft 140, so that the first sub-shell 110 and the second sub-shell 120 fit together, and finally use the first fastener 150 to connect the first sub-shell 110 and the second sub-shell 120 to achieve a fixed connection between the first sub-shell 110 and the second sub-shell 120. During the above connection process, the second component 210 on the center rod 300 can be avoided from contacting the first component 220 on the first sub-shell 110 and the second sub-shell 120, thereby avoiding damage to the first component 220 and the second component 210, and extending the service life of the first component 220 and the second component 210.

[0351] In addition, the above-mentioned arrangement can also enable the guide rod 400 and the housing 100 to form a split and detachable design, which is more conducive to the installation and fixation of the first component 220 on the inner circumference of the housing 100 without losing the coaxiality of the guide rod 400 and the housing 100. At the same time, it is also convenient to process the guide rod 400 separately to ensure the smoothness of the surface of the guide rod 400, thereby ensuring the guiding performance of the guide rod 400.

[0352] In some embodiments, as shown in Figures 6, 7, and 8, at least a portion of the guide rod 400 extends out of the accommodating cavity 130, and a through hole 411 is provided on the portion of the guide rod 400 extending out of the accommodating cavity 130. In other words, the ends of the guide rod 400 extend out of the first sub-housing 110 and the second sub-housing 120, and the ends of the guide rod 400 are connected to the first sub-housing 110 and the second sub-housing 120. This achieves a fixed connection between the guide rod 400 and the housing 100, thereby facilitating the use of the housing 100 to support the guide rod 400, improving the positional stability of the guide rod 400, thereby ensuring the working performance of the guide rod 400, and facilitating the use of the guide rod 400 to guide the movement direction of the center rod 300.

[0353] At the same time, by extending the end of the guide rod 400 out of the first sub-shell 110 and the second sub-shell 120, the guide rod 400 and the shell 100 can be connected outside the shell 100, so as to reduce the difficulty of connecting the guide rod 400 and the shell 100, that is, to reduce the difficulty of matching the guide rod 400.

[0354] In some embodiments, as shown in Figure 7, the housing 100 is provided with a second avoidance through hole 161, which is connected to the accommodating cavity 130. The second avoidance through hole 161 is used to avoid the guide rod 400, so that the end of the guide rod 400 can extend out of the first sub-shell 110 and the second sub-shell 120 and be connected to the first sub-shell 110 and the second sub-shell 120, so as to reduce the difficulty of connecting the guide rod 400 and the housing 100.

[0355] Optionally, as shown in Figures 6, 8, 10, and 12, the first sub-housing 110 is provided with a third avoidance groove 114, and the second sub-housing 120 is provided with a fourth avoidance groove 124. The third avoidance groove 114 and the fourth avoidance groove 124 cooperate to define a second avoidance through-hole 161. This not only forms the second avoidance through-hole 161 in communication with the accommodating cavity 130 on the housing 100, but also reduces the difficulty in forming the second avoidance through-hole 161 and the difficulty in fitting the guide rod 400 to the second avoidance through-hole 161, thereby improving the assembly efficiency of the housing 100.

[0356] Optionally, as shown in Figures 7 and 13, a guide protrusion 430 is provided on the guide rod 400, and the guide protrusion 430 is fitted and connected in the second avoidance through hole 161 to achieve the fitting connection between the guide rod 400 and the second avoidance through hole 161, and to position the guide rod 400 to ensure the position stability of the guide rod 400.

[0357] In other embodiments, as shown in FIG8 , one side of the first sub-housing 110 and one side of the second sub-housing 120 are rotatably connected in the circumferential direction of the housing 100, and the end of the guide rod 400 extends to one side of the axial end of the first sub-housing 110 and the second sub-housing 120 and is connected to the first sub-housing 110 and the second sub-housing 120. This means that when one side of the first sub-housing 110 and one side of the second sub-housing 120 are rotatably connected, the end of the guide rod 400 is connected to the axial end of the first sub-housing 110 and the second sub-housing 120. In this way, while the first sub-housing 110 and the second sub-housing 120 are rotatably connected, the guide rod 400 can also be effectively matched with the center rod 300, so that the guide rod 400 can be used to guide the movement direction of the center rod 300.

[0358] In some embodiments, as shown in Figure 8, in the circumferential direction of the casing 100, one side of the first sub-shell 110 and one side of the second sub-shell 120 are rotatably connected, and a mounting plate 420 is set at the end of the guide rod 400, and a fifth connecting hole 421 is provided on the mounting plate 420. The first sub-shell 110 and the second sub-shell 120 are both provided with a sixth connecting hole 180 facing the fifth connecting hole 421. The second fastener connects the fifth connecting hole 421 and the sixth connecting hole 180 to fix the guide rod 400 to the first sub-shell 110 and the second sub-shell 120, so that the casing 100 is used to support the guide rod 400, thereby improving the position stability of the guide rod 400 and ensuring the working performance of the guide rod 400.

[0359] Alternatively, the second fastener may be a fastening bolt, a fastening screw, or a rivet.

[0360] In summary, the first sub-shell 110 and the second sub-shell 120 of this embodiment are connected together by the rotating shaft 140, and the two can rotate relative to each other around the rotating shaft 140. When the housing 100 is specifically assembled, the rotating shaft 140 is first passed through the multiple first connecting lugs 1111 and the multiple second connecting lugs 1211 in sequence to achieve the rotational fit of the first sub-shell 110 and the second sub-shell 120. Then, the center rod 300 is set in one of the first sub-shell 110 and the second sub-shell 120, and the bearing 170 is sleeved on the center rod 300 and the center rod 300 is sleeved on the guide rod 400. Then, the other of the first sub-shell 110 and the second sub-shell 120 is rotated around the rotating shaft 140 so that it is close to the first sub-shell 110 or the second sub-shell 120. One of the second sub-shells 120, and ensure that the bearing 170 fits in the third avoidance groove 114 and the fourth avoidance groove 124, so that the first sub-shell 110 and the second sub-shell 120 fit together, and finally use the first fastener 150 to connect the first sub-shell 110 and the second sub-shell 120, and use the second fastener to connect the guide rod 400 to achieve a fixed connection between the first sub-shell 110 and the second sub-shell 120. In the above connection process, the second component 210 on the center rod 300 can also be completely avoided from contacting the first component 220 on the first sub-shell 110 and the second sub-shell 120, thereby avoiding damage to the first component 220 and the second component 210, and extending the service life of the first component 220 and the second component 210.

[0361] In some embodiments, the electromagnetic actuator 1000 of this embodiment is formed as a cylindrical linear motor. The cylindrical linear motor has a relatively closed structure, good sealing and no unilateral magnetic pull, so as to ensure the working performance of the electromagnetic actuator 1000.

[0362] It should be noted that when the electromagnetic actuator 1000 is formed as a cylindrical linear motor, the first sub-shell 110 and the second sub-shell 120 of the housing 100 are both formed as semi-cylindrical, so that the first sub-shell 110 and the second sub-shell 120 can cooperate to form a complete cylindrical motor housing.

[0363] In some embodiments, as shown in FIG. 7 , a spring 600 is provided on the electromagnetic actuator 1000 . The spring 600 is used to provide partial damping force and withstand partial vibration impact to improve the working performance of the electromagnetic actuator 1000 , thereby ensuring the comfort of the vehicle 20000 .

[0364] Optionally, as shown in FIG7 , the electromagnetic actuator 1000 is further provided with an upper support 500 and a mounting seat 191. The upper support 500 is connected to the side of the center rod 300 away from the accommodating cavity 130, and the mounting seat 191 is connected to the outer peripheral wall of the housing 100. A receiving space for a spring 600 is formed between the upper support 500 and the mounting seat 191. The spring 600 is placed in the receiving space so that the upper support 500 and the mounting seat 191 cooperate to fix the spring 600. In this way, when the electromagnetic actuator 1000 is applied to the suspension system 10000 of the vehicle 20000, when the vehicle 20000 is excited by the road surface and the center rod 300 and the housing 100 move relative to each other, the spring 600 can be used to buffer and absorb vibrations. At the same time, the spring 600 can also provide a certain damping effect, thereby enhancing the vibration reduction effect of the electromagnetic actuator 1000 and thus improving the comfort of the vehicle 20000.

[0365] In some embodiments, as shown in Figure 7, the spring 600 is arranged between the upper support 500 and the mounting seat 191, and the upper end of the spring 600 is abutted against the upper support 500, and the lower end of the spring 600 is abutted against the mounting seat 191. In this way, during the relative movement of the center rod 300 and the housing 100, the spring 600 can be compressed or stretched, so that the spring 600 can provide part of the damping force and withstand part of the vibration impact, thereby improving the comfort of the vehicle 20000.

[0366] In some embodiments, as shown in Figure 7, a bushing 700 is provided on the side of the center rod 300 away from the accommodating cavity 130, the bushing 700 is connected to the upper support 500, and buffer blocks 800 are provided on the opposite sides of the upper support 500 and the mounting seat 191, and the spring 600 is arranged between the two buffer blocks 800.

[0367] In some embodiments, as shown in Figures 17, 18, 19, and 20, the first assembly 220 is connected to the housing 100, and an elastic stopper 1015 is provided between the housing 100 and the second assembly 210. The elastic stopper 1015 abuts against the housing 100 and the second assembly 210, respectively. This ensures that the electromagnetic actuator 1000 can buffer the vibration of the second assembly 210 during operation, extending the service life of the second assembly 210 and reducing the noise generated by the electromagnetic actuator 1000 during operation.

[0368] In some embodiments, the elastic stopper 1015 is formed as a spring 600 and / or a buffer pad. This means that the elastic stopper 1015 is formed as a spring 600; or, the elastic stopper 1015 is formed as a buffer pad; or, the elastic stopper 1015 is formed as a spring 600 and a buffer pad, so that the elastic stopper 1015 can buffer the vibration of the second component 210, extend the service life of the second component 210, and reduce the noise generated by the electromagnetic actuator 1000 during operation.

[0369] It should be noted that the specific implementation forms of the elastic limiter 1015 of this embodiment include but are not limited to rubber pads, polyurethane pads, spiral springs, leaf springs, coil springs and other elastic parts. This embodiment has no restrictions on the number and layering of the elastic limiter 1015. For example, the use of multi-layer buffer pads or circumferentially arranged multiple springs are all within the scope of embodiments that can be implemented in this embodiment.

[0370] In some embodiments, as shown in Figure 20, the elastic limiter 1015 is a coil spring, which is arranged between the housing 100 and the second component 210. In actual use, in order to buffer the movement of the second component 210, it is necessary to ensure that the coil spring is in a compressed state after assembly. Therefore, the compression amount of the coil spring can be ensured by pressing the end cover 1012.

[0371] In some embodiments, as shown in Figures 17, 10 and 20, the second component 210 is located inside the housing 100 and distributed along the inner radial circumference of the housing 100, and the elastic limiter 1015 is located at the lower part of the second component 210 and the upper side of the end cover 1012.

[0372] Among them, the second component 210 is composed of a multi-layer magnet component, and a layer of magnets forms a complete circular ring. All layers of magnets are pasted to the inner wall of the casing 100. An elastic limiter 1015 is set at the bottom of the bottom layer of magnets. The lower end of the elastic limiter 1015 is connected to the top of the stopper of the end cover 1012. Because the elastic limiter 1015 has a certain elasticity, it ensures that during the operation of the electromagnetic actuator 1000, the elastic limiter 1015 can buffer the vibration of the magnet.

[0373] It should be noted that the size of the elastic limiter 1015 is not fixed and can be adjusted according to the size of the electromagnetic actuator 1000, which has the advantage of high adaptability.

[0374] At the same time, the elastic limiting member 1015 of this embodiment can integrate the function of the sealing module to seal the gap between the end cover 1012 and the housing 100.

[0375] In a specific example, during the assembly process, glue is first applied to the outer surface of the second component 210, and then the second component 210 is assembled into the interior of the housing 100 in layers along the axial direction of the electromagnetic actuator 1000. After the assembly of the bottom-layer second component 210 is completed, the elastic limiter 1015 is assembled, and finally the end cover 1012 is assembled. When the elastic limiter 1015 is a coil spring, the pre-compression of the coil spring can be completed.

[0376] It should also be noted that the preload of the coil spring in this embodiment should not be too large to avoid excessive pressure on the magnet. During implementation, the preload can be controlled by the height of the protruding portion 1014 on the end cover 1012 .

[0377] In some embodiments, two adjacent sub-housings 101 of the plurality of sub-housings 101 are rotatably connected. This means that regardless of whether the plurality of sub-housings 101 are arranged relative to each other in the circumferential direction of the housing 100 or in the axial direction of the housing 100, the two adjacent sub-housings 101 are rotatably connected, thereby reducing the difficulty of assembling the housing 100 and the first component 220 and the second component 210, and to a certain extent preventing the first component 220 and the second component 210 from colliding with the housing 100 during assembly.

[0378] In some embodiments, the multiple sub-housings 101 are detachably connected. This allows for fixed connection of the multiple sub-housings 101, ensuring a stable relative position of the multiple sub-housings 101, thereby ensuring the positional stability of the housing 100, facilitating the use of the housing 100 to support and protect the first component 220 and the second component 210, thereby extending the service life of the first component 220 and the second component 210 and improving the positional stability of the first component 220 and the second component 210.

[0379] At the same time, by arranging the multiple sub-shells 101 to be detachably matched, the difficulty of assembling and disassembling the multiple sub-shells 101 can be reduced, thereby reducing the difficulty of assembling and disassembling the housing 100 and facilitating the maintenance of the first component 220 and the second component 210.

[0380] In some embodiments, as shown in Figures 20-26 , an electromagnetic actuator 1000 includes a central rod 300, with a portion of the central rod 300 extending out of the housing 100. This facilitates a secure connection between the central rod 300 and external components, reduces the difficulty of connecting the central rod 300 and external components, and thereby ensures the operating performance of the electromagnetic actuator.

[0381] In some embodiments, as shown in conjunction with FIG21 and FIG22 , the second assembly 210 includes: a core assembly 211 and a winding assembly 212. The core assembly 211 is disposed on a center rod 300, and the winding assembly 212 is disposed on the core assembly 211. This allows the core assembly 211 and the winding assembly 212 to be supported by the center rod 300, thereby improving the positional stability of the core assembly 211 and the winding assembly 212. At the same time, the core assembly 211 and the winding assembly 212 can cooperate with the first assembly 220 to ensure the working performance of the electromagnetic actuator 1000.

[0382] In summary, the second component 210 is arranged on the center rod 300, and the first component 220 is arranged on the housing 100. The first component 210 and the second component 220 are coupled to enable the center rod 300 and the housing 100 to produce relative movement, thereby ensuring the working performance of the electromagnetic actuator 1000.

[0383] In some embodiments, as shown in conjunction with Figures 22 and 23, the center rod 300 is provided with a wire passage 330, through which the connecting wires 2121 of the winding assembly 212 pass and extend out of the housing 100. This allows the connecting wires 2121 of the winding assembly 212 to be led from the interior of the housing 100 to the exterior of the housing 100, making it easier to lead the connecting wires 2121 of the winding assembly 212 out, thereby reducing the difficulty of electrical connection of the winding assembly 212. Furthermore, the center rod 300 can be used to protect the connecting wires 2121, thereby extending the service life of the connecting wires 2121 and improving the safety of the connecting wires 2121.

[0384] In some embodiments, a quick-change connector is provided at the end of the electromagnetic actuator 1000 to enable quick plugging and unplugging of the connecting wire 2121 and the electrical control component.

[0385] In some embodiments, as shown in Figures 22, 23 and 26, a wire outlet device 230 is provided in the center rod 300, and a wire passing channel 330 is provided in the wire outlet device 230, thereby realizing the setting of the wire passing channel 330 in the center rod 300 and reducing the difficulty of forming the wire passing channel 330.

[0386] It should be noted that the overall structure of the electromagnetic actuator 1000 of this embodiment is based on the traditional hydraulic damping shock absorber, in which the intermediate damper is replaced by a linear motor. According to the structural composition of the electromagnetic actuator 1000, it mainly includes a first component 220 (moving subassembly), a second component 210 (stator assembly) and an upper support 500, in which the first component 220 and the second component 210 constitute a linear motor, and the connecting line 2121 of the second component 210 is led to the outside of the casing 100 through the center rod 300.

[0387] In a specific example, the second component 210 is part of the stator component, which is located on the inner side of the entire electromagnetic actuator 1000 and includes a connecting wire 2121, a wire outlet device 230, a detection module 900, a center rod 300, a first limiter 380, an iron core assembly 211, a winding assembly 212, a guide bearing 840, a limiter nut 850, a bearing 170 and an assembly nut 830. Among them, the connecting wire 2121, the limiter nut 850, the guide bearing 840, the first limiter 380, the wire outlet device 230, the bearing 170 and the assembly nut 830 are all assembled on the center rod 300 and together constitute a central component, which integrates multiple functions such as limiting, positioning, anti-rotation, heat dissipation, guiding, and wire outlet. The iron core assembly 211 and the winding assembly 212 constitute the second component 210.

[0388] In some embodiments, the core assembly 211 and the winding assembly 212 are both annular. The second component 210 is composed of several core assemblies 211 and winding assemblies 212, which are stacked with one layer of winding assembly 212 on top of another layer of core assembly 211 and are sleeved on the center rod 300, eventually becoming a cylindrical shape. It is fixed to the center rod 300 by a limiting nut 850. This design facilitates the manufacturing of the core assembly 211 and the winding of the winding assembly 212. The detection module 900 is fixed on the assembly groove 950 of the center rod 300 to accurately locate the relative position between the mover assembly and the stator assembly, thereby achieving accurate control. The connecting wire 2121 is fixed to the center rod 300 through the wire outlet device 230.

[0389] In some embodiments, as shown in FIG24 , a first reinforcing rib 2012 is provided on the outer peripheral wall of the core assembly 211. A wiring channel is provided within the first reinforcing rib 2012. The wiring channel is used to guide the connecting wires 2121 of different phases of the winding assembly 212 to the wire passage 330 of the center rod 300. Here, the wiring channel is provided on the inner side of the first reinforcing rib 2012. The wiring channel facilitates leading out the connecting wires 2121 of the winding assembly 212, thereby reducing the difficulty of electrical connection of the winding assembly 212.

[0390] At the same time, the difficulty of forming the wiring channel can be reduced by providing the first reinforcing rib 2012 . The wiring channel can also limit the position of the connecting line 2121 , thereby improving the position stability of the connecting line 2121 .

[0391] In some embodiments, the first reinforcing rib 2012 protrudes toward the outer periphery of the core assembly 211 to form a wiring channel on the side of the first reinforcing rib 2012 facing the inner periphery of the core assembly 211 .

[0392] In some embodiments, as shown in FIG24 , a plurality of slots 2019 and a plurality of first reinforcing ribs 2012 that can constrain the direction of the wire output are evenly distributed on the circumference of the core assembly 211 , and the connecting wires 2121 of different phases of the winding assembly 212 are output from the designated slots 2019 along the routing channels therein.

[0393] At the same time, according to the principle that the three-phase lines must be connected together, the connecting lines 2121 of the same phase of the winding assembly 212 are connected from the same slot 2019, so that the connecting lines 2121 of the same phase can be connected from the outside of the core assembly 211 from top to bottom (as shown in Figure 24), the tool operation space is not restricted, and problems can be easily and intuitively discovered during subsequent maintenance, thereby reducing maintenance costs.

[0394] It should be noted that since the slot 2019 limits the direction of the wire output, and the core assembly 211 and the center rod 300 have cylindrical pins to limit the core assembly 211 from rotating around the center rod 300, the connecting wire 2121 of the winding assembly 212 is relatively fixed, the position deviation is small, and the connection is reliable.

[0395] In some embodiments, in combination with Figures 22, 23, 24 and 25, the three connecting wires 2121 respectively pass through the three wire channels 330 on the wire outlet device 230, and the three outlets of the three wire channels 330 are evenly distributed in the circumferential direction. Three wire outlets 311 are provided on the center rod 300. The three outlets of the wire channels 330, the three wire outlets 311 and the three slots 2019 correspond one to one. During assembly, the wire outlet device 230 is assembled to the center rod 300, and the three connecting wires 2121 pass through the wire outlet device 230, the wire outlet 311 and the winding assembly 212.

[0396] Through the above arrangement, the connecting wire 2121 comes out from the outside of the core assembly 211 and then passes through the inner side of the center rod 300 and the wire channel 330 to reach the outside of the casing 100. The wire is fixed during the whole process. Among them, the wire channel 330 plays a role in fixing and protecting the connecting wire 2121, which effectively solves the problem of the risk of extrusion and scratching in the prior art.

[0397] In some embodiments, as shown in FIG. 22 , a first limiting member 380 is sleeved on the top of the center rod 300 , and the first limiting member 380 and the outlet of the center rod 300 jointly fix the connecting line 2121 .

[0398] In some embodiments, the first limiting member 380 is made of rubber, which can buffer the impact of surrounding components on the connecting line 2121 under extreme working conditions, thereby protecting the connecting line 2121 and ensuring the reliability of the electrical system.

[0399] In this embodiment, the actuator assembly of the electromagnetic actuator 1000 is located outside the overall structure and includes: a bearing 170, a housing 100, a first assembly 220, a second stopper 390, a guide rod 400, and a mounting bracket 192. The mounting bracket 192 is assembled to the wheel end and connected to the housing 100 via a plurality of bolts, forming a closed operating environment within the electromagnetic actuator 1000. The guide rod 400 provides guidance. The second stopper 390, which fits over the guide rod 400, can cushion the impact of the first assembly 220 on the second assembly 210 under extreme operating conditions, thereby effectively protecting the second assembly 210. The first assembly 220 is evenly distributed on the inner side of the housing 100 to provide a fixed magnetic field. The housing 100 primarily serves a protective function. The local raised features on the housing 100 (such as the mounting seat 191 and the second reinforcing rib 195) primarily support the spring 600 and provide overall heat dissipation.

[0400] With the above arrangement, during the movement of the electromagnetic actuator 1000 , the first assembly 220 moves axially up and down along the center line through the bearing 170 , the guide bearing 840 , the housing 100 , the mounting bracket 192 and the center rod 300 . Since the interior of the entire casing 100 is sealed and the casing 100 is moving, the winding assembly 212 needs to pass through the center rod 300 to reach the outside of the casing 100 when it is output, and the outer side of the upper end of the center rod 300 has relative movement with the bearing 170, and the inner side of the lower end is embedded with a guide bearing 840, and the guide bearing 840 has relative movement with the mounting bracket 192. Therefore, as shown in Figure 24, the winding assembly 212 is sleeved under the center rod 300 and the winding assembly 212 is output from the outside, avoiding the relative movement area between the bearing 170 and the mounting bracket 192 below the center rod 300. The connecting wire 2121 passes through the center rod 300 and the wire output device 230 to reach the outside of the casing 100, avoiding the relative movement area between the upper part of the center rod 300 and the bearing 170. This design prevents the connecting wire 2121 from being squeezed or scratched during operation.

[0401] In some embodiments, a tower top is disposed above the electromagnetic actuator 1000, comprising an upper support 500, an assembly nut 830, a spring 600, a dust cover 820, and a cooling structure 810. The electromagnetic actuator 1000 is assembled to the tower top by engaging the first threaded section 831 on the center rod 300 with the assembly nut 830. The tower top is then secured to the vehicle body. The center rod 300 passes through the middle of the upper support 500, and the connecting wire 2121 also passes through the vehicle body to the front compartment. The wire is then coupled to the electronic control terminal via a quick-change connector, thereby connecting to the motor and electronic control, ultimately achieving electromagnetic shock absorber control.

[0402] Among them, the spring 600 can buffer the impact of the road, the dust cover 820 can prevent dust from entering the interior of the electromagnetic actuator 1000, the upper support 500 cooperates with the vehicle body to fix one end of the electromagnetic actuator 1000 on the vehicle body, and the cooling structure 810 can perform heat exchange circulation with the coolant in the center rod 300 to reduce the temperature of the coolant.

[0403] In some embodiments, after the winding assembly 212 and the core assembly 211 are assembled to the center rod 300, the limiting nut 850 and the second threaded segment 851 cooperate to thread the core assembly 211 onto the center rod 300. This design ensures that the entire core assembly 211 is fixed to the center rod 300 as designed.

[0404] In summary, the wire outlet structure of the electromagnetic actuator 1000 of this embodiment utilizes the relative relationship of the surrounding components and is cleverly designed to solve the problem of wire outlet difficulties. It has the advantages of safety and reliability, easy assembly and disassembly, and compact space design.

[0405] In some embodiments, as shown in Figures 21-25 , the center rod 300 is provided with a first anti-rotation portion 370, and the housing 100 is provided with a second anti-rotation portion. The first anti-rotation portion 370 and the second anti-rotation portion cooperate to limit the rotational freedom of the center rod 300. This prevents the center rod 300 and the housing 100 from rotating relatively significantly, ensuring that the center rod 300 and the housing 100 can effectively move relative to each other, thereby maintaining the operating performance of the electromagnetic actuator 1000.

[0406] In some embodiments, as shown in Figures 21-25 , the first anti-rotation portion 370 is a long slot extending axially along the center rod 300, and the second anti-rotation portion is fixed to the housing 100 and extends into the first anti-rotation portion 370. This achieves the purpose of utilizing the first anti-rotation portion 370 and the second anti-rotation portion to cooperate to limit the rotational freedom of the center rod 300, preventing relative rotation between the center rod 300 and the housing 100, and ensuring the operating performance of the electromagnetic actuator 1000.

[0407] In some embodiments, as shown in Figure 21, an anti-rotation hole 193 is provided on the housing 100, and the second anti-rotation part is an anti-rotation column, which passes through the anti-rotation hole 193 and extends into the first anti-rotation part 370 to achieve the cooperation between the first anti-rotation part 370 and the second anti-rotation part, so as to facilitate limiting the rotational freedom of the center rod 300.

[0408] In some embodiments, the anti-rotation column is fixed to the anti-rotation hole 193 to ensure the position stability of the anti-rotation column, thereby facilitating the use of the first anti-rotation portion 370 and the second anti-rotation portion to cooperate to limit the rotational freedom of the center rod 300.

[0409] In some embodiments, as shown in Figures 27-35 , the winding assembly 212 has a first outlet 2018, at least part of which is located between the core assembly 211 and the housing 100. This allows wires to be routed from the outside of the winding assembly 212, reducing the difficulty of routing the winding assembly 212 and the routing of the connecting wires 2121.

[0410] In addition, the above arrangement frees up space inside the core assembly 211, facilitating cooling design.

[0411] In some embodiments, the first outlet terminal 2018 is connected to the connecting wire 2121 to ensure the working performance of the winding assembly 212 .

[0412] It should be noted that the electromagnetic actuator 1000 of this embodiment is part of the suspension system 10000 of vehicle 20000. Installed in place of conventional vehicle shock absorbers, it primarily functions to reduce vibrations transmitted from the road surface and control energy flow, thereby improving vehicle comfort and energy efficiency. Compared to conventional shock absorbers, it incorporates a complete linear motor structure capable of linear motion, replacing the hydraulic damping mechanism of conventional shock absorbers.

[0413] Among them, the output wire structure is for the linear motor part in the electromagnetic actuator 1000. This linear motor is an electric motor in which the first component 220 and the second component 210 can perform linear displacement relative to each other, which includes a mover component and a stator component in the usual sense of the motor.

[0414] In some embodiments, as shown in conjunction with Figures 27-35, the electromagnetic actuator 1000 of this embodiment includes an upper support 500, an assembly nut 830, a center rod 300, a connecting wire 2121, a housing 100, a first component 220, a second component 210, and a mounting bracket 192. The upper support 500 is locked to the center rod 300 via the assembly nut 830. The connecting wire 2121 includes three phases A, B, and C. The connecting wire 2121, the center rod 300, and the second component 210 constitute the stator assembly of the electromagnetic actuator 1000. The first component 220 and the housing 100 constitute the mover assembly of the electromagnetic actuator 1000. The mounting bracket 192 serves to connect the suspension system 10000.

[0415] In some embodiments, as shown in Figures 28 and 29, the core assembly 211 has a tooth slot, and the winding assembly 212 is arranged in the tooth slot. A wire end outlet groove 2015 is opened on the surface of each tooth slot, which is used for the wire end of the winding assembly 212 in each tooth slot to pass through between the core assembly 211 and the housing 100, so that at least part of the structure of the first outlet head 2018 of the winding assembly 212 can be located between the core assembly 211 and the housing 100, thereby realizing the outlet of the wire from the outside of the winding assembly 212, reducing the difficulty of outlet of the winding assembly 212 and the difficulty of arranging the connecting wire 2121.

[0416] In some embodiments, as shown in FIG. 28 , a groove 20111 is formed on the outer surface of the core assembly 211 for cross-phase connection between the winding assemblies 212 .

[0417] Optionally, as shown in Figure 31, the winding assembly 212 includes a first phase winding 21214, a second phase winding 21215 and a third phase winding 21216. The first phase winding 21214 and the first phase winding 21214, the second phase winding 21215 and the second phase winding 21215, and the second phase winding 21216 and the second phase winding 21216 need to connect the first output terminals 2018 at one end to form a series structure. In this embodiment, a groove 20111 is provided on the outer surface of the core assembly 211, which is conducive to the passage of the first output terminals 2018 between phases, and welding or crimping processes are required between the first output terminals 2018. The groove 20111 can ensure that the first output terminals 2018 are unobstructed when connected, with a large operating space and low implementation difficulty, which is conducive to mass production.

[0418] In some embodiments, as shown in FIG30 , a cable trough 2013 is provided on the top of the core assembly 211. When the wiring between the three first outlet terminals 2018 is completed, the final connecting wire 2121 will reach the upper surface of the core assembly 211, and the three-phase wires will be directly buried in the cable trough 2013 on the upper surface to ensure smooth wiring.

[0419] In some embodiments, a wire passage 330 is provided on the center rod 300 , and the connecting wire 2121 passes through the wire passage 330 and extends to the outside of the housing 100 .

[0420] In some embodiments, as shown in Figures 28 and 32, the wire channel 330 is formed on the outer wall of the center rod 300. In this way, the connecting wire 2121 does not need to pass inside or outside, and fits perfectly with the outer wall of the center rod 300, reducing the difficulty of connecting the connecting wire 2121.

[0421] In some embodiments, the connecting wire 2121 can be fixed by gluing, injection molding, or covered with a protective shell to enhance the fit between the connecting wire 2121 and the center rod 300, and the operation is convenient and the operating space is sufficient.

[0422] In some embodiments, as shown in Figures 30 and 32, the cable trough 2013 can be linear, spiral, or curved, and the cable trough 2013 can be one or multiple, multiple can merge into one or one can branch into multiple, all of which are covered by this embodiment.

[0423] In addition, as shown in FIG33 , the arrangement order of the first phase winding 21214 , the second phase winding 21215 and the third phase winding 21216 can be changed arbitrarily, and there is a wiring operation.

[0424] At the same time, in combination with Figures 27, 34 and 35, the core assembly 211 and the center rod 300 can be integrated or split, and the outer surface of the core assembly 211 is provided with a groove 20111, which is used for cross-phase connection between the winding assemblies 212.

[0425] In summary, this embodiment buries the connecting wire 2121 in the outer wall of the core assembly 211, which will not interfere with the first component 220, and also avoids the inner wall of the upper support 500 and the assembly nut 830. It does not affect the assembly of the upper support 500 and the center rod 300, and will not cause interference problems. It makes the lead inspection of the winding assembly 212 convenient and the operating space ample. It is friendly to the arrangement of the connecting wire 2121, and at the same time makes room for the internal space of the core assembly 211 to facilitate cooling design.

[0426] In some embodiments, as shown in conjunction with Figures 36-40, the winding assembly 212 has a second wire outlet 214, at least part of which is located between the core assembly 211 and the center rod 300. This allows the wires to be routed from the inside of the winding assembly 212, making it easier to route the wires from the winding assembly 212, reducing the space occupied by the second component 210, and reducing the difficulty in molding the second component 210.

[0427] In some embodiments, the second outlet 214 is connected to the connecting wire 2121 to ensure the working performance of the winding assembly 212 .

[0428] In some embodiments, as shown in FIG40 , the wire passage 330 includes a radial hole 333 and an axial hole 334, and the radial hole 333 is connected to the axial hole 334. Here, the wire passage 330 includes the radial hole 333 extending radially along the electromagnetic actuator 1000 and the axial hole 334 extending axially along the electromagnetic actuator 1000. The radial hole 333 is connected to the axial hole 334 to allow the connecting wire 2121 to effectively pass through the wire passage 330 and extend out, thereby reducing the difficulty of leading out the connecting wire 2121.

[0429] In some embodiments, the connecting wire 2121 passes through the axial hole 334 and the radial hole 333 and is connected to the second outlet head 214 of the winding assembly 212 to achieve connection between the second outlet head 214 and the connecting wire 2121 .

[0430] In some embodiments, as shown in conjunction with Figures 36-40, the electromagnetic actuator 1000 of this embodiment includes a center rod 300, an iron core assembly 211, a winding assembly 212, a first assembly 220, and a housing 100. The center rod 300, the iron core assembly 211, and the winding assembly 212 together constitute the stator assembly of the electromagnetic actuator 1000, and the first assembly 220 and the housing 100 together constitute the mover assembly of the electromagnetic actuator 1000.

[0431] In some embodiments, the core assembly 211 is pressed or screwed onto the center rod 300, and the winding assembly 212 is wound or placed on the core assembly 211. The three-phase wires of the winding assembly 212 need to be led out from the core assembly 211 and from the top of the center rod 300 to facilitate connection to the motor controller.

[0432] In some embodiments, in combination with Figures 38 and 39, a wire end outlet groove 2015 and a radial hole 333 are respectively provided on the core assembly 211, wherein the outer wire end of the winding assembly 212 passes through the wire end outlet groove 2015 from the outermost edge of the core assembly 211 back to the interior to reach the radial hole 333, and is internally outlet through the radial hole 333, while the inner wire end of the winding assembly 212 can be directly outlet through the radial hole 333, thereby realizing that at least part of the structure of the second outlet head 214 is set between the core assembly 211 and the center rod 300.

[0433] It should be noted that each core assembly 211 and winding assembly 212 on the second component 210 is connected to the output line in this way, and the wiring between the wire ends can be performed according to the design of the three-phase line.

[0434] It should also be noted that compared with arranging at least part of the structure of the outlet end of the winding assembly 212 between the core assembly 211 and the casing 100, this embodiment occupies a small space and does not affect the winding space of the winding assembly 212. The slot fill rate is greatly improved compared with the external outlet method, so that more electromagnetic thrust can be obtained in the same space, which ensures that the performance of the electromagnetic actuator 1000 can be greatly improved to a certain extent.

[0435] In some embodiments, the wire outlet groove 2015 can be a straight groove or an inclined groove. The number of wire outlet grooves 2015 can be single or multiple according to needs. Multiple wire outlet grooves 2015 are usually evenly distributed to achieve better results, and the width of the wire outlet groove 2015 depends on the diameter of the wire used in the electromagnetic actuator 1000. The shape of the groove of the wire outlet groove 2015 can be an arc mouth or a square mouth, etc.

[0436] In some embodiments, the central rod 300 is provided with a connecting rod end outlet groove 331 and a winding segment outlet groove 332 in the axial direction thereof. The guide rod end outlet groove 331 and the winding segment outlet groove 332 are both provided on the outer wall surface of the central rod 300. The second outlet ends 214 of the winding assembly 212 are all fed into the winding segment outlet groove 332 for alternate wiring operations, and finally the winding segment outlet is completed. By providing the guide rod end outlet groove 331 on the central rod 300, the connecting wire 214 led out from the winding assembly 212 is connected to the winding segment outlet groove 332. 21 can be directly buried in the center rod 300 without changing the overall direction of the outgoing line, so that the outgoing operation of the connecting line 2121 is convenient and quick, without changing the natural direction of the connecting line 2121, and there is no need to penetrate the internal space of the center rod 300 for outgoing line, retaining the natural outgoing state of the three-phase line, causing little damage to the connecting line 2121 itself, effectively improving the durability of the connecting line 2121, and the internal space of the center rod 300 can be vacated for cooling arrangement, thereby improving the performance of the electromagnetic actuator 1000.

[0437] It should be noted that if the diameter of the connecting wire 2121 used in the winding assembly 212 is small, the winding segment outlet groove 332 may not be provided, and the wire can be directly outlet along the outer wall of the center rod 300.

[0438] In some embodiments, as shown in FIG40 , when the center rod 300 and the core assembly 211 are integrally formed, the core assembly 211 includes a plurality of placement slots 2119 spaced apart along the axial direction of the center rod 300 , and the winding assembly 212 is placed in the plurality of placement slots 2119 , thereby achieving a mating connection between the winding assembly 212 and the core assembly 211 , thereby facilitating the formation of the second assembly 210 .

[0439] In some embodiments, as shown in FIG40 , a wiring space 2011 is provided in the middle of the core assembly 211 , and each slot 2119 is provided with a radial hole 333 communicating with the wiring space 2011 , so as to realize internal wiring of the winding assembly 212 .

[0440] In summary, this embodiment can effectively improve the slot fill rate of the electromagnetic actuator 1000, thereby improving the performance of the electromagnetic actuator 1000, and burying the connecting wire 2121 in the wall thickness of the center rod 300 does not occupy additional space and does not change the natural direction of the connecting wire 2121 itself, which is beneficial to extending the service life of the connecting wire 2121 and is convenient and quick to operate.

[0441] In some embodiments, as shown in Figures 41 to 48, the core assembly 211 includes a plurality of stator cores 2014, which are arranged axially along the center rod 300. The stator core 2014 includes: a stator tooth portion 2141 and a stator yoke portion 2142. The stator tooth portion 2141 includes a plurality of first laminations 21411 stacked axially along the center rod 300. The stator yoke portion 2142 is formed into a ring shape and is provided on the stator tooth portion 2141. At least a portion of the stator yoke portion 2142 is located on one side of the stator tooth portion 2141 so that a winding slot 2133 is formed between the stator tooth portion 2141 and the stator yoke portion 2142. The winding assembly 212 includes a multi-phase winding, and the coils 2123 of the winding (the specific structure of the coil 2123 can be seen in Figure 65) are all placed on the winding slot 2133. Thereby, the winding assembly 212 is arranged on the core assembly 211 to ensure the working performance of the second component 210 and reduce the difficulty of assembling the second component 210 .

[0442] It should be noted that by configuring the stator tooth portion 2141 to include a plurality of first laminations 21411 stacked axially along the center rod 300, the plurality of first laminations 21411 can effectively reduce the eddy current loss of the stator tooth portion 2141 compared to a structure in which the stator tooth portion 2141 is configured as a whole conductor, thereby improving the thrust and efficiency of the electromagnetic actuator 1000.

[0443] In some embodiments, the winding slots 2133 are formed on one axial side of the stator teeth 2141 and located on the radial outer periphery of the stator yoke 2142 , thereby facilitating placement of the coils 2123 of the winding on the winding slots 2133 .

[0444] In some embodiments, as shown in Figures 41-48 , the stator yoke 2142 is disposed on one axial side of the stator teeth 2141. This forms a winding slot 2133 between the stator teeth 2141 and the stator yoke 2142, thereby facilitating placement of the coils 2123 of the winding in the winding slot 2133. This reduces the difficulty in aligning the winding assembly 212 with the core assembly 211, thereby ensuring the operating performance of the second assembly 210.

[0445] In some embodiments, as shown in FIG. 41 to FIG. 46 , the stator yoke 2142 includes a plurality of stacked second laminations 21422 , which are stacked radially along the center rod 300 to effectively reduce eddy current losses in the stator teeth 2141 .

[0446] That is to say, the multiple first laminations 21411 of the stator tooth portion 2141 are stacked along the axial direction of the center rod 300, and the multiple second laminations 21422 of the stator yoke portion 2142 are stacked along the radial direction of the center rod 300. The axially stacked teeth and the radially stacked yoke portions can significantly weaken the eddy current loss in the stator tooth portion 2141.

[0447] In some embodiments, as shown in Figures 41 and 42, the stator teeth 2141 and the stator yoke 2142 are made of one-piece silicon steel sheets stamped and laminated. The one-piece stamping structure can also ensure the thrust and efficiency of the electromagnetic actuator 1000 while weakening the thrust fluctuation of the electromagnetic actuator 1000.

[0448] At the same time, the integrated stamping structure also has the advantages of fewer structural sections, less gluing, high assembly precision, and no impact on the thrust efficiency of the electromagnetic actuator 1000.

[0449] Of course, in other embodiments, as shown in Figures 44 and 45, the stator yoke 2142 can also be fixed on the stator teeth 2141 to form the stator core 2014, that is, the stator core 2014 can also be made by fixing independent stator yokes 2142 and stator teeth 2141.

[0450] In some embodiments, the stator yoke 2142 is connected to the stator teeth 2141 so that the relative positions of the stator yoke 2142 and the stator teeth 2141 are stable, thereby ensuring the working performance of the stator core 2014 .

[0451] In some embodiments, the stator yoke 2142 and the stator teeth 2141 are reinforced by laser welding.

[0452] It should be noted that the above-mentioned assembly method of the stator yoke 2142 and the stator teeth 2141 can make the stator core 2014 have the advantages of separate lamination and mature technology, and the stator core 2014 can be applicable to complex core assembly 211 structures.

[0453] In some other embodiments, as shown in Figures 45 and 46 , the stator yoke 2142 is axially inserted into and fixed in the axially stacked stator teeth 2141. The stator core 2014 can also be made by fixing independent stator yokes 2142 and stator teeth 2141.

[0454] In some embodiments, the stator yoke 2142 is inserted into the stator teeth 2141 and is reinforced with the stator teeth 2141 by laser welding, which ensures that the stator yoke 2142 and the stator teeth 2141 are firmly connected while ensuring a certain assembly accuracy.

[0455] In addition, the above-mentioned matching form can significantly reduce the eddy current loss of the core assembly 211 while improving the installation accuracy, reducing the impact on the thrust and efficiency of the linear motor, and weakening the thrust fluctuation.

[0456] In some embodiments, as shown in conjunction with FIG47 and FIG48 , the stator yoke 2142 includes a plurality of stacked second laminations 21422, which are stacked along the axial direction of the center rod 300. In other words, the plurality of second laminations 21422 are not limited to being stacked along the radial direction of the center rod 300; the plurality of second laminations 21422 can also be stacked along the axial direction of the center rod 300. Since the axial stamping and lamination process of silicon steel sheets is very mature, this technical solution has high process feasibility.

[0457] In summary, the stator core 2014 is made of axially laminated silicon steel sheets fixed on axially laminated silicon steel sheets.

[0458] In some embodiments, the stator yoke 2142 and the stator teeth 2141 are connected by laser welding.

[0459] Through the above-mentioned matching method, the stator yoke 2142 and the stator tooth 2141 can be separately stacked, with high axial installation accuracy, without affecting the thrust and efficiency of the linear motor, and weakening thrust fluctuations.

[0460] In some embodiments, as shown in Figures 41-46 , the stator yoke 2142 is a winding member that is wound circumferentially around the center rod 300. It should be noted that the winding member herein refers to the stator yoke 2142 being formed by spirally winding a single silicon steel sheet around an axis. This winding member functions equivalently to the effect of axially stacking silicon steel sheets in reducing eddy current losses in the stator teeth 2141, i.e., it can significantly reduce eddy current losses in the stator yoke 2142.

[0461] In some embodiments, as shown in Figures 41 to 46 , a first center hole 21412 is formed on the stator tooth 2141, and the stator yoke 2142 is located in the first center hole 21412. This allows the stator yoke 2142 to be positioned on the stator tooth 2141, reducing the difficulty of mating the stator tooth 2141 with the stator yoke 2142.

[0462] In some embodiments, as shown in Figures 41 to 46 , a second center hole 21421 is formed on the stator yoke 2142. Both the first center hole 21412 and the second center hole 21421 serve as mounting holes for the stator core 2014 and the center rod 300. This facilitates assembly of the stator core 2014 on the center rod 300, achieving a mating connection between the stator core 2014 and the center rod 300.

[0463] In some embodiments, as shown in conjunction with Figures 41-48 , at least one of the stator yoke 2142 and the stator teeth 2141 is formed with a positioning protrusion 21415 that mates with the center rod 300. This allows the stator yoke 2142 and the stator teeth 2141 to form an interference fit with the center rod 300 during assembly, ensuring the connection strength and relative position stability between the core assembly 211 and the center rod 300, preventing the core assembly 211 from rotating circumferentially on the structure of the center rod 300 during movement, and improving the assembly accuracy of the stator yoke 2142 and the center rod 300. This significantly reduces eddy current losses and reduces the impact on the thrust and efficiency of the linear motor.

[0464] In some embodiments, as shown in Figures 41 to 48 , positioning protrusions 21415 that cooperate with the center rod 300 are formed on the stator yoke 2142 and the stator teeth 2141 so that the stator yoke 2142 and the stator teeth 2141 can form a tight fit with the center rod 300.

[0465] In some embodiments, as shown in Figures 41 to 48, grooves 20111 are formed on the stator teeth 2141 for cross-phase connection between the coils 2123.

[0466] At the same time, by forming positioning protrusions 21415 that cooperate with the center rod 300 on both the stator yoke 2142 and the stator tooth 2141, the alignment of the grooves 20111 can be ensured, thereby reducing the difficulty of wiring the coil 2123.

[0467] In some embodiments, as shown in Figures 49-53 , the stator yoke 2142 is formed as a single piece. In other words, the stator yoke 2142 is not limited to being formed as a wound piece, but can also be formed as a single piece to reduce the difficulty of forming the stator yoke 2142.

[0468] In some embodiments, as shown in conjunction with Figures 49 to 53, the stator yoke 2142 includes a body 21427 and a plug-in portion 21428. The plug-in portion 21428 is formed on one side of the body 21427 along the axial direction of the center rod 300. The plug-in portion 21428 facilitates the fixed connection between the stator yoke 2142 and the stator teeth 2141, and reduces the difficulty of connecting the stator yoke 2142 and the stator teeth 2141.

[0469] In some embodiments, as shown in Figures 49 to 53, the stator tooth portion 2141 is made of axially laminated silicon steel sheets, and the stator yoke portion 2142 is machined from solid material, wherein the material of the stator yoke portion 2142 is soft magnetic material, and positioning protrusions 21415 that cooperate with the center rod 300 are formed on the stator yoke portion 2142 and the stator tooth portion 2141, and a groove 20111 is formed on the stator tooth portion 2141 for cross-phase connection between the coils 2123.

[0470] In some embodiments, in combination with Figures 49, 50 and 51, the plug-in portion 21428 is formed as a boss on the main body 21427, and a first connecting structure 21416 is formed on the stator tooth portion 2141. The first connecting structure 21416 is formed to be a dovetail groove, and the boss is inserted into the dovetail groove and fixed to the stator tooth portion 2141. At the same time, laser welding is used to strengthen the connection strength between the stator yoke portion 2142 and the stator tooth portion 2141, thereby achieving a fixed connection between the stator yoke portion 2142 and the stator tooth portion 2141.

[0471] At the same time, the above structure can also enable the stator teeth 2141 to significantly reduce the eddy current loss in the core assembly 211, while also ensuring the thrust and efficiency of the linear motor.

[0472] In some embodiments, the same trapezoidal punch is used to punch out a first connecting structure 21416 formed as a dovetail groove, so that the slot of the first connecting structure 21416 becomes wider the closer it is to the outer edge of the stator tooth portion 2141. In this way, when the plug-in portion 21428 is inserted into the first connecting structure 21416, because the slot width of the dovetail groove is smaller than the bottom width of the dovetail groove, it can be ensured that the plug-in portion 21428 cannot slip out of the first connecting structure 21416, thereby strengthening the fixing strength of the stator yoke portion 2142 and the stator tooth portion 2141.

[0473] In some embodiments, the opposite ends of the bottom of the dovetail groove are chamfered toward the inside away from the dovetail groove. The chamfer is formed by a punch with a chamfer. Using a punch with a chamfer can increase the service life of the punch. At the same time, by setting the chamfer on the dovetail groove, interference between the plug-in portion 21428 and the first connecting structure 21416 during the assembly process can be avoided, ensuring that the plug-in portion 21428 can be normally inserted into the first connecting structure 21416 along the axial direction and complete the fixation of the stator yoke portion 2142 and the stator tooth portion 2141.

[0474] In addition, when the plug-in portion 21428 is inserted into the first connecting structure 21416, since the side surface of the plug-in portion 21428 and the bottom end surface of the main body 21427 form a chamfer, the bottom end surface of the main body 21427 and the end surface of the stator tooth portion 2141 cannot fit together. Therefore, in this embodiment, an inclined surface inclined toward the center line of the plug-in portion 2142 is formed between the bottom end surface of the main body 21427 and the side surface of the plug-in portion 21428. When the side surface of the plug-in portion 21428 and the bottom end surface of the main body 21427 have a chamfer, the stator yoke portion 2142 and the stator tooth portion 2141 can be ensured to fit together, thereby ensuring the reliability of the structure.

[0475] In some embodiments, in combination with Figures 52 and 53, the stator yoke 2142 includes a main body 21427 and a plug-in portion 21428. The main body 21427 is arranged on the axial side of the plurality of first laminations 21411. The planar size of the main body 21427 is equal to the inner and outer diameters of the first laminations 21411. The plug-in portion 21428 is plugged into the first center hole 21412, thereby achieving a fixed connection between the stator yoke 2142 and the stator tooth portion 2141.

[0476] Optionally, in combination with Figures 52 and 53, a second anti-rotation protrusion 21417 is provided on the stator tooth portion 2141, and an anti-rotation groove 21425 is provided on the stator yoke portion 2142. The second anti-rotation protrusion 21417 is engaged in the anti-rotation groove 21425 to achieve fixed engagement between the stator tooth portion 2141 and the stator yoke portion 2142, preventing the stator tooth portion 2141 from rotating, ensuring that the groove 20111 is aligned, and reducing the difficulty of wiring the coil 2123.

[0477] In some embodiments, after the stator yoke 2142 and the stator teeth 2141 are connected by the second anti-rotation protrusion 21417 and the anti-rotation groove 21425, laser welding is used to strengthen the connection strength between the stator yoke 2142 and the stator teeth 2141.

[0478] In some embodiments, as shown in Figures 52 and 53, a first boss structure 21426 is provided at the connection between the main body 21427 and the plug-in portion 21428 to prevent the connection between the main body 21427 and the plug-in portion 21428 from breaking and to enhance the mechanical strength of the connection.

[0479] In some embodiments, as shown in FIG. 54 to FIG. 58 , a first connection structure 21416 and a second connection structure 21423 are formed on the stator yoke 2142 and the stator teeth 2141, respectively. The first connection structure 21416 cooperates with the second connection structure 21423 to achieve a cooperative connection between the stator yoke 2142 and the stator teeth 2141.

[0480] In some embodiments, as shown in Figures 54-58 , the first connection structure 21416 is plugged into the second connection structure 21423. This allows for plugged engagement between the stator yoke 2142 and the stator teeth 2141, reduces the difficulty of securing the stator yoke 2142 and the stator teeth 2141, ensures the quality of the securing, and stabilizes the relative positions of the stator yoke 2142 and the stator teeth 2141.

[0481] In some embodiments, as shown in Figures 54 to 58, a plurality of second connecting structures 21423 are provided below the stator yoke 2142. The second connecting structure 21423 is formed as a column structure. The thickness of the column is the same as the thickness of the stator tooth 2141. The stator tooth 2141 is provided with a plurality of first connecting structures 21416 that cooperate with the column structure. The first connecting structure 21416 is formed as a dovetail groove. The column structure is inserted into the dovetail groove at the corresponding position of the stator tooth 2141, so as to fix the stator yoke 2142 and the stator tooth 2141.

[0482] It should be noted that since the coil 2123 surrounds the stator yoke 2142 and is coiled and placed on the stator teeth 2141, when the electromagnetic actuator 1000 is running, the magnetic lines of force mainly move along the radial direction within the stator teeth 2141 and the axial direction within the stator yoke 2142. Among them, the stator teeth 2141 can largely weaken the eddy current loss generated in the teeth through the axially stacked silicon steel sheets, and the stator yoke 2142 can weaken the eddy current loss of the stator yoke 2142 through the circumferentially wound silicon steel sheets.

[0483] In some embodiments, the stator yoke 2142 is formed by a stamping and then winding process, wherein the same punch is used for stamping the column, and the punch shape is trapezoidal. If a square punch is used, assembly interference will form at the connection between the column structure and the stator yoke 2142 and the local area of ​​the stator tooth 2141. At the same time, if the chamfered corners are not designed, the life of the punch will be greatly shortened, thereby increasing costs.

[0484] Therefore, this embodiment uses the same trapezoidal punch with rounded corners to process the second connecting structure 21423, which can reduce process costs and meet process assembly requirements.

[0485] In addition, when the second connecting structure 21423 cooperates with the first connecting structure 21416, when the second connecting structure 21423 is inserted into the dovetail groove opened by the stator tooth portion 214, since the side surface of the second connecting structure 21423 and the bottom end surface of the stator yoke portion 2142 form a chamfer, there is a risk that the bottom end surface of the stator yoke portion 2142 and the end surface of the stator tooth portion 2141 will not fit together. By adopting a trapezoidal punch, an inclined surface 21424 inclined toward the center line of the second connecting structure 21423 can be formed on the bottom end surface of the stator yoke portion 2142 and the side surface of the second connecting structure 21423 (as shown in Figure 58). This can ensure that the stator yoke portion 2142 and the stator tooth portion 2141 can fit together when there is a chamfer between the second connecting structure 21423 and the bottom end surface of the stator yoke portion 2142, thereby ensuring the reliability of the structure.

[0486] It should also be noted that since the same punch is used when stamping the second connecting structure 21423, the width of the rolled second connecting structure 21423 will vary radially, wherein the closer to the radial outer edge of the stator yoke 2142, the wider the width of the second connecting structure 21423, thereby forming the stator yoke 2142 into a dovetail trapezoidal shape.

[0487] In some embodiments, as shown in Figure 57, the stator tooth portion 2141 is punched out at a fixed position to form a plurality of first connection structures 21416 forming dovetail grooves. When the second connection structure 21423 is inserted into the first connection structure 21416, because the groove width of the dovetail groove is smaller than the bottom width of the dovetail groove, it can be ensured that the second connection structure 21423 cannot slip out of the first connection structure 21416, thereby strengthening the fixing strength between the stator yoke portion 2142 and the stator tooth portion 2141.

[0488] In some embodiments, as shown in Figure 57, the inner corner of the slot of the first connecting structure 21416 is provided with a chamfered corner. If the second connecting structure 21423 is provided with a structure that matches the chamfered corner, it can avoid interference between the stator yoke 2142 and the stator tooth 2141 during installation, thereby ensuring that the second connecting structure 21423 on the stator yoke 2142 can be normally inserted into the first connecting structure 21416 of the stator tooth 2141 and complete the fixed connection between the stator yoke 2142 and the stator tooth 2141.

[0489] In summary, the stator yoke 2142 and the stator tooth 2141 of this embodiment are combined with the column structure of the second connection structure 21423 and the dovetail groove structure design of the first connection structure 21416, so that the spirally wound stator yoke 2142 and the axially stacked stator tooth 2141 can form a mechanical connection. At the same time, laser welding is used to enhance the connection strength between the stator yoke 2142 and the stator tooth 2141.

[0490] In some embodiments, as shown in Figures 59-66 , the core assembly 211 includes a first type of core 2111 and a second type of core 2112. In the axial direction of the center rod 300, there are multiple second type cores 2112, and both ends of the multiple second type cores 2112 are provided with a first type core 2111. The end surface of the first type core 2111 facing the second type core 2112 is provided with a coil 2123, and both end surfaces of the second type core 2112 are provided with a coil 2123. The coils 2123 on both sides of the second type core 2112 have the same number of phases. This achieves a coordinated connection between the core assembly 211 and the winding assembly 212, and reduces the difficulty of connecting the coils 2123 of each phase.

[0491] In some embodiments, the coils 2123 at both ends of each second-type iron core 2112 are connected in series, and the coils 2123 of the same phase, which are spaced apart axially along the center rod 300, are welded together via connecting wires 2121. This achieves a welded connection of the coils 2123 of the same phase, ensuring the performance of the winding assembly 212.

[0492] In some embodiments, in combination with Figures 59-66, this embodiment uses a clever design to set the iron core assembly 211 to be composed of a first type of iron core 2111 and a second type of iron core 2112. The coils 2123 on the same second type of iron core 2112 are in-phase coils, and the coils 2123 on the same second type of iron core 2112 are connected by welding. In this way, it surpasses traditional designs in many aspects such as layout space, production efficiency, processing difficulty, maintenance convenience, structural complexity, and consistency of parts.

[0493] Among them, in combination with Figures 60, 61 and 62, the second component 210 of this embodiment is composed of connecting wires 2121, an iron core assembly 211, an insulating frame 213, a coil 2123 and insulating paper 2122. The connecting wires 2121 are three-phase A, B and C respectively, and the coils are flat wires to increase space utilization. The connecting wires 2121 are bent and led out at the end of the coil 2123 through the grooves 20111 opened on the surface of the iron core assembly 211 and the wire grooves 2132 opened on the surface of the insulating frame 213. The first type of iron core 2111 is a single-sided coil 2123.

[0494] Optionally, the axial middle part of the second component 210 is assembled by the second type iron core 2112, the insulating frame 213 and the coil 2123, and the end of the second component 210 is assembled by the first type iron core 2111, the coil 2123 and the insulating frame 213, wherein the coil 2123 on the first type iron core 2111 is the A-phase coil 2123.

[0495] In a specific example, the order of components on the second component 210 from the starting end is A-phase coil 2123, B-phase coil 2123 and C-phase coil 2123. The two adjacent out-of-phase coils 2123 are separated by insulating paper 2122, and the same-phase coils 2123 are connected in series. The bilateral coils inside the second component 210 are also connected in series. When wiring the coils 2123, the lead wires of the coils 2123 are welded to the connecting wire 2121 bent at the end of the coil 2123 to achieve circuit connection and reduce wiring errors.

[0496] In some embodiments, in combination with Figures 63, 64 and 65, the first type of iron core 2111 is provided with a first annular groove 21111, a wire groove 2013 and a groove 20111, and the structure of the insulating skeleton 213 is similar to that of the first type of iron core 2111. The insulating skeleton 213 is provided with a second annular groove 2138, a lead channel 2131 and a wire groove 2132. The insulating skeleton 213 is nested in the first annular groove 21111, and a lead wire 21231 and a first lead head 2018 are formed on the coil 2123. When the coil 2123 is processed, the lead wire 21231 and the first lead head 2018 are formed. The outgoing wire 21231 is bent at a right angle and wound from the inside to the outside, and is bent twice at the end of the coil 2123 to form a first outgoing wire end 2018. During assembly, the coil 2123 is nested in the first annular groove 21111, and the lead wire 21231 extends through the wire arrangement groove 2013 and the lead channel 2131 to the outside of the first type of iron core 2111 for wiring and power supply. This method has a simple structure, good consistency in processing methods, simple processing technology, fewer operating steps, and a large operating space, which is conducive to reducing costs and improving production efficiency.

[0497] In some embodiments, as shown in Figure 66, the second type of iron core 2112 is also provided with an insulating skeleton 213 and a coil 2123. Both sides of the second type of iron core 2112 have a first annular groove 21111, a wire groove 2013 and a groove 20111. The insulating skeleton 213 is nested in the first annular groove 21111, and the same-phase coil 2123 is nested on the insulating skeleton 213, wherein the two wire grooves 2013 are 180° apart. The coil 2123 on one side is connected in series with the first wire outlet 2018 of the coil 2123 on the other side at the welding point through the first wire outlet 2018, so that the parts have the same structure, the structure is simple, the production and processing efficiency is high, and it is conducive to mass production and cost control.

[0498] At the same time, by arranging the coils 2123 on both side end surfaces of the second type iron core 2112, the space utilization rate is high.

[0499] In some embodiments, the leads of coil 2123 can be bent in two different ways, depending on the orientation of the opening of lead channel 2131 of insulating frame 213. For example, lead wire 21231 can be bent from the top of coil 2123, or from the bottom of coil 2123. The winding method of coil 2123 is the same, from the inside out, which simplifies the winding method.

[0500] In some embodiments, the connection between the coils 2123 of the same phase is also in series, and the connection points are still welded, which has good operability and simple process, which is conducive to production and processing. Moreover, the welding points are on the outside, which is more intuitive during assembly and welding, which is conducive to avoiding wiring errors and improving production efficiency. This method has a large operating space, is easy to operate, and saves work time.

[0501] In summary, the core assembly 211 of this embodiment is composed of stacked independent modules, and the module units are separated by insulating paper 2122. The basic components of each module are the iron core, the insulating frame 213 and the coil 2123. The processing technology of each part is simple, the structure is basically the same, the structural complexity is low, and the assembly is convenient, which is convenient for mass production and processing, saving costs and working hours and improving production efficiency.

[0502] In some embodiments, in combination with Figures 67-71, the core assembly 211 of this embodiment is mainly used in the linear motor assembly of the electromagnetic suspension. The core assembly 211 belongs to the stator component. On the one hand, it provides support for the coil 2123, the insulating frame 213, etc. On the other hand, it provides a path for the magnetic field generated by the winding assembly 212 and withstands the interaction force generated between the magnetic field and the power magnet. Multiple core assemblies 211 and winding assemblies 212 are stacked and fixed along the axial direction to form a second component 210.

[0503] In some embodiments, in combination with Figures 67 and 68, the core assembly 211 includes a third-type core 2110, and the third-type core 2110 includes a support frame 2016 and a support core 2017. Multiple support cores 2017 are assembled and stacked along the circumferential direction to form a circular core, and the circular core and the support frame 2016 form a laminated third-type core 2110.

[0504] In some embodiments, as shown in Figures 68, 69 and 70, a protruding structure is provided on the inner end of the support core 2017, and a supporting groove is provided on the outer cylindrical surface of the support frame 2016. The supporting groove cooperates with the protruding structure of the support core 2017 to limit and support the root of the support core 2017, thereby ensuring the structural stability of the third type of core 2110.

[0505] It should be noted that, as shown in Figure 71, since the coil 2123 and the support core 2017 are axially stacked, the support frame 2016 is also used to bear the weight of the support core 2017 and the coil 2123. By providing a support groove on the outer cylindrical surface of the support frame 2016, it is also possible to avoid the weight being directly borne by the third type core 2110, thereby improving the reliability of the third type core 2110.

[0506] In some embodiments, the support frame 2016 can be designed as an integral structure, or can be designed as an upper and lower split structure connected by fasteners or the like.

[0507] In a specific example, the support frame 2016 adopts an integral design solution to reduce the difficulty of forming the support frame 2016 and improve the structural strength of the support frame 2016.

[0508] In some embodiments, as shown in FIG. 67 , a groove 20111 may be provided at the outer end of the support core 2017 as required for connection between different coils 2123 .

[0509] Among them, the position, shape and number of the grooves 20111 can be adjusted according to needs. It is recommended that the shapes of the grooves 20111 of the same third-type iron core 2110 be unified, which can reduce the specifications of the supporting iron core 2017.

[0510] In some embodiments, as shown in Figure 69, the support core 2017 is fan-shaped, thin on the inside and thick on the outside. At the same time, under the premise that the support core 2017 meets the requirements of process, use, etc., the thickness of the support core 2017 needs to be as thin as possible, and the shape of the single-piece support core 2017 can be adjusted according to needs, such as setting a groove 20111, but it must meet the matching relationship between the circular support cores 2017 and meet the requirements of the shape of the third type of core 2110, and the specifications of the support core 2017 should be minimized to facilitate production and assembly.

[0511] In some embodiments, the support core 2017 is made of magnetic conductive material, and materials with high resistivity are selected as much as possible. Insulating materials are set on the left and right sides along the circumferential lamination direction, such as insulating paint. In addition, adhesives are also required to be coated. Different support cores 2017 are reliably connected together through adhesives. The coating should be as thin as possible while meeting the requirements to reduce space occupation and avoid excessive reduction in the magnetic permeability of the third type core 2110.

[0512] In some embodiments, if the adhesive material satisfies the insulation requirements, there is no need to apply the insulating material.

[0513] In some embodiments, as shown in FIG70 , the support frame 2016 is annular and made of a magnetically conductive material, preferably a material with a high resistivity. The thickness of the support frame 2016 should be as thin as possible while meeting the process and usage requirements.

[0514] In some embodiments, as shown in Figure 70, the inner cylindrical surface of the support frame 2016 is provided with a second positioning portion 350, and the center rod 300 is provided with a first positioning portion 340 (the specific structure of the first positioning portion 340 can be seen in Figure 25). The first positioning portion 340 and the second positioning portion 350 cooperate to make the center rod 300 and the support frame 2016 relatively stationary, thereby achieving circumferential limitation of the third type iron core 2110 and the center rod 300, preventing the third type iron core 2110 from rotating around the center rod 300, and ensuring the working performance of the third type iron core 2110.

[0515] In some embodiments, the first positioning portion 340 is formed as a groove provided on the outer peripheral wall of the center rod 300, the second positioning portion 350 is a positioning slot, and the anti-rotation rod 360 is provided between the first positioning portion 340 and the second positioning portion 350. This is to limit the position of the center rod 300 and the support frame 2016, so that the center rod 300 and the support frame 2016 are relatively stationary, and the difficulty of limiting the position of the center rod 300 and the support frame 2016 is reduced.

[0516] Optionally, the shape and number of the second positioning portions 350 can be set according to requirements.

[0517] In some embodiments, as shown in FIG71 , the third type of iron core 2110 is stacked and installed axially along the stator center rod, and coils 2123 are placed between the third type of iron cores 2110. After the electromagnetic actuator 1000 is energized, the coils 2123 will be energized to generate a magnetic field. If the current changes, the magnetic field will also change. This change will cause an induced current, i.e., eddy current, to be generated inside the third type of iron core 2110. The eddy current will generate heat loss, thereby reducing the working efficiency of the electromagnetic actuator 1000. By arranging the third type of iron core 2110 to be divided into several supporting iron cores 2017 along the circumferential direction and performing insulation design between each supporting iron core 2017, the original longer eddy current circuit can be interrupted, so that it can only pass through a smaller cross-section in the narrow circuit of each supporting iron core 217, thereby increasing the resistance in the eddy current path, reducing the eddy current and thus reducing the eddy current loss. The selection of materials with high resistivity is also for increasing the resistance in the eddy current path.

[0518] In some embodiments, since the support frame 2 is a continuous structure in the circumferential direction, eddy current loss will be generated. Therefore, the thickness of the support frame 2 should be as thin as possible.

[0519] In some embodiments, as shown in conjunction with Figures 72 to 118 , the electromagnetic actuator 1000 further includes a wiring assembly 2113, through which the in-phase coils 2123 spaced axially along the center rod 300 are electrically connected. This enables electrical connection of the in-phase coils 2123 and reduces the difficulty of electrical connection of the in-phase coils 2123.

[0520] In some embodiments, as shown in conjunction with Figures 77-86 , the wiring assembly 2113 includes a conductive member 2114 and an insulating layer 2115. The insulating layer 2115 wraps the conductive member 2114. Both ends of the conductive member 2114 are provided with stoppers 2116 for positioning and electrically connecting the coil 2123. In other words, the stoppers 2116 are used to position the coil 2123 and electrically connect to the coil 2123, thereby achieving electrical connection between the coils 2123 of the same phase and ensuring the positional stability of the coil 2123.

[0521] At the same time, by providing an insulating layer 2115 to wrap the conductive member 2114, the service life of the conductive member 2114 can be extended and the safety of the conductive member 2114 can be improved.

[0522] In some embodiments, as shown in Figures 78-86 , the stopper 2116 forms a wire-gripping groove on the conductive member 2114. This facilitates positioning and electrically connecting the coil 2123 using the stopper 2116, thereby achieving electrical connection of the coils 2123 of the same phase and reducing the difficulty of electrically connecting the coils 2123 of the same phase.

[0523] It should be noted that the main innovation of this embodiment is a winding connection method applied to the electromagnetic actuator 1000, which is novel, simple, efficient and reliable.

[0524] 72 to 77 , the electromagnetic actuator 1000 of this embodiment includes a mover assembly and a stator assembly, which can move linearly relative to each other. The stator assembly includes a center rod 300, a guide bearing 840, a sealing cover 312, a first core unit 21114, multiple second-type cores 2112, a second core unit 21115, a wiring assembly 2113, an output assembly 216, and a connecting line 2121. The first core unit 21114, multiple second-type cores 2112, and the second core unit 21115 are all sleeved on the outside of the center rod 300, the guide bearing 840 is assembled inside the center rod 300, and the sealing cover 312 is assembled on the top of the center rod 300, which respectively play the role of limiting and sealing.

[0525] In some embodiments, as shown in Figure 77, the connecting wire 2121 includes a first phase lead 21211, a second phase lead 21212 and a third phase lead 21213. There are three wire outlets 311 on the upper part of the center pole 300. The first phase lead 21211, the second phase lead 21212 and the third phase lead 21213 pass through the three wire outlets 311 respectively to facilitate the connection between the connecting wire 2121 and the coil 2123.

[0526] In some embodiments, as shown in Figures 87-92, the first core unit 21114 includes a first type core 2111, a coil 2123, and an inner lead-out device 860. The coil 2123 is sleeved on the first type core 2111. The coil 2123 is a multi-layer ring-shaped conductor wound with a plurality of conductors. The radially outer joint is bent outward along the ring winding direction to form a first lead-out terminal 2018. The radially inner joint is bent inward along the ring winding direction to form a second lead-out terminal 214. The inner lead-out device 860 is embedded in the interior of the first type core 2111 and connected to the second lead-out terminal 214 of the coil 2123, facilitating in-phase electrical connection.

[0527] In some embodiments, as shown in FIG. 89 , a first internal mounting hole 21116 for assembling the inner wire outlet device 860 is provided in the first type iron core 2111 , so that the inner wire outlet device 860 can be embedded in the interior of the first type iron core 2111 .

[0528] In some embodiments, the outer layer of the coil 2123 is provided with an insulating paint coating to protect the coil 2123 .

[0529] It should be noted that since the bending direction of the first wire outlet 2018 and the second wire outlet 214 is the same as the winding direction of the coil 2123, and the bending is very smooth and will not cause any damage to other features of the coil 2123, the paint of the first wire outlet 2018 and the second wire outlet 214 can be peeled off to facilitate the connection between the inner wire outlet device 860 and the second wire outlet 214.

[0530] In some embodiments, as shown in Figures 89 and 90, the inner wire outlet device 860 includes a first insulating member 862 and a first conductive wire 863, and a first assembly member 861 is provided between the first insulating member 862 and the bottom of the first conductive wire 863. In the first core unit 21114, the second wire outlet head 214 of the coil 2123 is clamped in the first assembly member 861 of the inner wire outlet device 860 and connected to the first conductive wire 863. The top of the first conductive wire 863 is connected to the third phase lead 21213 to achieve the connection between the coil 2123 and the third phase lead 21213, thereby reducing the difficulty of connecting the coil 2123 and the third phase lead 21213.

[0531] In some embodiments, as shown in FIG89 , a plurality of grooves 20111 are provided on the outside of the first type iron core 2111 , and the first output terminal 2018 of the coil 2123 is located in one of the grooves 20111 , thereby reducing the difficulty of connecting the first output terminal 2018 .

[0532] In some embodiments, as shown in Figures 93, 94 and 95, the second type iron core 2112 includes a second type iron core 2112, two coils 2123 and an inner wiring device 870, the two coils 2123 are respectively placed on both sides of the second type iron core 2112, and the inner wiring device 870 is embedded in the second type iron core 2112 to realize electrical connection between the inner wiring device 870 and the coil 2123.

[0533] In some embodiments, as shown in FIG. 95 , a second internal mounting hole 21122 for assembling the inner wiring device 870 is provided in the second type iron core 2112 , so that the inner wiring device 870 can be embedded in the interior of the second type iron core 2112 .

[0534] In some embodiments, as shown in Figures 96 and 97, the inner wiring device 870 includes a second insulating member 872 and a second conductive wire 873, and two second assembly parts 871 are formed between the second insulating member 872 and the bottom of the second conductive wire 873. In the second type iron core 2112, the second outlet ends 214 of the upper and lower coils 2123 are respectively clamped in the two second assembly parts 871 of the inner wiring device 870 and connected to the second conductive wire 873, so that the two coils 2123 on the same second type iron core 2112 can be electrically connected through the inner wiring device 870, thereby forming a conductive path.

[0535] In some embodiments, as shown in FIG95 , a plurality of grooves 20111 are provided on the outside of the second type iron core 2112 , wherein the first terminal heads 2018 of the two coils 2123 are both located in one of the grooves 20111 to reduce the difficulty of connecting the first terminal heads 2018 .

[0536] In some embodiments, as shown in Figures 98, 99, and 100, the second core unit 21115 includes a first-type core 2111, a coil 2123, and a bottom wiring device 880. The coil 2123 is sheathed above the first-type core 2111, and the bottom wiring device 880 is located below the first-type core 2111. The first-type core 2111 has a third internal mounting hole 21117 defined therein, and three grooves 20111 defined on the outside of the first-type core 2111.

[0537] In some embodiments, as shown in Figures 101 and 102, the bottom wiring device 880 includes a third insulating member 881 and a third conductor 882. The third conductor 882 is provided with a first phase connector 8821, a second phase connector 8822, and a third phase connector 8823. In the second core unit 21115, the third phase connector 8823 is embedded in the third internal mounting hole 21117 within the first type of core 2111 and connects to the second terminal 214 of the coil 2123. The first phase connector 8821 and the second phase connector 8822 are respectively located in two grooves 20111 on the outside of the first type of core 2111.

[0538] In some embodiments, in combination with Figures 78-86, the wiring assembly 2113 includes a long wiring assembly 21131, a middle wiring assembly 21132 and a short wiring assembly 21133, wherein the long wiring assembly 21131, the middle wiring assembly 21132 and the short wiring assembly 21133 have the same functions and similar characteristics, the length of the long wiring assembly 21131 is greater than the length of the middle wiring assembly 21132, and the length of the middle wiring assembly 21132 is greater than the length of the short wiring assembly 21133.

[0539] In some embodiments, as shown in Figures 78, 79 and 80, a first limiting feature 21151 is further provided on the insulating layer 2115 of the wiring assembly 2113 to facilitate positioning of the wiring assembly 2113.

[0540] In some embodiments, in combination with Figures 103-106, the outgoing line assembly 216 includes a long outgoing line assembly 2161 and a short outgoing line assembly 2162. The wiring devices of the long outgoing line assembly 2161 and the short outgoing line assembly 2162 have the same functions and similar features, and the length of the long outgoing line assembly 2161 is greater than the length of the short outgoing line assembly 2162.

[0541] In some embodiments, as shown in Figures 103-106, the long-outlet assembly 2161 and the short-outlet assembly 2162 both include a fourth insulating member 2163 and a fourth conductive wire 2164. A wire-holding groove 2166 is formed at the bottom of the fourth insulating member 2163 and the fourth conductive wire 2164. The groove 2166 is used to connect to the coil 2123.

[0542] In some embodiments, as shown in Figures 103 to 106 , a second limiting feature 2165 is provided on the fourth insulating member 2163 to facilitate positioning of the outlet assembly 216 .

[0543] In some embodiments, as shown in Figures 107 to 110, multiple second-type iron cores 2112, multiple long wiring components 21131, short wiring components 21133, and long outlet components 2161 constitute a first phase structure of the second component 210. In the first phase structure, the first outlet ends 2018 of the coils 2123 of each second-type iron core 2112 are located in the same direction when viewed from top to bottom. The first outlet ends 2018 of the upper coils 2123 of the first layer of second-type iron cores 2112 are connected to the first phase lead 21211 through the fourth conductor 2161 of the long outlet component 2161 to form a first-phase winding outlet structure. The first outlet ends 2018 of the lower coils 2123 of the first layer of second-type iron cores 2112 are located in the same direction when viewed from top to bottom. 018 is connected up and down with the first outlet 2018 of the upper coil 2123 of the second layer of the second type iron core 2112 through the conductive part 2114 of the first long wiring component 21131, and the first outlet 2018 of the lower coil 2123 of the second layer of the second type iron core 2112 is connected up and down with the first outlet 2018 of the upper coil 2123 of the third layer of the second type iron core 2112 through the conductive part 2114 of the second long wiring component 21131, and so on, until the first outlet 2018 of the lower coil 2123 of the last layer of the second type iron core 2112 is connected to the first phase connector 8821 of the bottom wiring device 880, thereby forming the first phase structure of the second component 210.

[0544] In some embodiments, in combination with Figures 111-114, multiple second-type iron cores 2112, multiple long wiring components 21131, middle wiring components 21132 and short-outlet components 2162 constitute the second phase structure of the second component 210. In the second phase structure, the first outlet ends 2018 of the coils 2123 of each second-type iron core 2112 are located in the same direction when viewed from top to bottom, and are staggered with the first phase structure. Similar to the first phase structure, the first outlet ends 2018 of the upper coils 2123 of the first layer of the second-type iron cores 2112 are connected to the second phase lead 21212 through the fourth conductor 2164 of the short-outlet component 2162, forming a second-phase winding outlet structure. The first layer of the second-type iron core The first lead 2018 of the lower coil 2123 of the second-type iron core 2112 is vertically connected to the first lead 2018 of the upper coil 2123 of the second-type iron core 2112 via the conductive member 2114 of the first long wiring assembly 21131. The first lead 2018 of the lower coil 2123 of the second-type iron core 2112 is vertically connected to the first lead 2018 of the upper coil 2123 of the third-type iron core 2112 via the conductive member 2114 of the second long wiring assembly 21131. This continues in this manner until the first lead 2018 of the lower coil 2123 of the last-type iron core 2112 is connected to the second phase connector 8822 of the bottom wiring device 880. This forms the second phase structure of the second assembly 210.

[0545] In some embodiments, in combination with Figures 115-118, the first core unit 21114, multiple second-type cores 2112, the second core unit 21115, and multiple long wiring components 21131 constitute the third phase structure of the second component 210. In the third phase structure, the first outlet 2018 of each coil 2123 is located in the same direction when viewed from top to bottom, and is staggered with the first phase structure and the second phase structure. In the third phase structure, the first core unit 21114 is located in the first layer, and the second outlet 214 of the coil 2123 of the first core unit 21114 is connected to the third phase lead 21213 through the inner outlet device 860, forming a third-phase winding outlet structure. The second layer to the penultimate layer are all composed of the second-type core 2112, and the last layer is the second core unit 21115, wherein the first outlet 2018 of the coil 2123 below the first layer of the second-type core 2112 is connected through The conductive part 2114 of the first long wiring component 21131 is connected up and down with the first outlet 2018 of the upper coil 2123 of the second layer of the second type iron core 2112, and the first outlet 2018 of the lower coil 2123 of the second layer of the second type iron core 2112 is connected up and down with the first outlet 2018 of the upper coil 2123 of the third layer of the second type iron core 2112 through the conductive part 2114 of the second long wiring component 21131, and so on, until the first outlet 2018 of the lower coil 2123 of the last layer of the second type iron core 2112 is connected up and down with the first outlet 2018 of the coil 2123 of the bottom second iron core unit 21115 through the conductive part 2114 of the long wiring component 21131, and the third phase connector 8823 of the bottom wiring device 880 is connected to the second outlet 214 of the coil 2123, thereby forming the third phase structure of the second component 210.

[0546] In summary, the outer edges of the wiring assembly 2113 and the outgoing wire assembly 216 of this embodiment will not exceed the outer boundary of the core assembly 211, and both the wiring assembly 2113 and the outgoing wire assembly 216 have limiting features, which can be positioned during assembly.

[0547] In some embodiments, as shown in conjunction with Figures 119-122, the wiring assembly 2113 includes a first connector 2117 and a second connector 2118. The first connector 2117 and the second connector 2118 are pluggable and mated. The first connector 2117 and the second connector 2118 are both provided on the core assembly 211 and electrically connected to the coil 2123. In other words, the wiring assembly 2113 is not limited to the above-described embodiments. The wiring assembly 2113 may also include a first connector 2117 and a second connector 2118. The first connector 2117 and the second connector 2118 are provided on the core assembly 211 and electrically connected to the coil 2123. In this way, when the first connector 2117 and the second connector 2118 are connected to an external component, the electrical connection between the coil 2123 and the external structural component can be achieved, reducing the difficulty of connecting the coil 2123.

[0548] In some embodiments, one of the first connector 2117 and the second connector 2118 is a jack and the other is a plug. The jack and the plug are plugged together to facilitate the electrical connection between the coil 2123 and the external structural component, reducing the difficulty of connecting the coil 2123.

[0549] It should be noted that the wire-out structure of this embodiment refers to the related structure designed for the winding assembly 212 to be wired out from the inside to the outside of the electromagnetic actuator 1000 .

[0550] Among them, the second component 210 is a part of the stator component of the electromagnetic actuator 1000. The stator component is on the inside of the entire structure, including a connecting wire 2121, a wire channel 330, a center rod 300, a first limiter 380, a winding assembly 212, an iron core assembly 211, a guide bearing 840 and a limit nut 850, wherein the winding assembly 212 and the iron core assembly 211 constitute the second component 210 (the specific structure of the electromagnetic actuator 1000 can be seen in Figure 22).

[0551] In some embodiments, as shown in Figures 119, 120 and 121, the winding assembly 212 and the core assembly 211 are both annular, and the winding assembly 212 is assembled on both the upper and lower surfaces of the core assembly 211. The second component 210 is composed of several winding assemblies 212 and core assemblies 211 stacked one layer on top of another (as shown in Figure 122). After stacking, they are put on the center rod 300 and finally become cylindrical.

[0552] In some embodiments, three grooves 20111 are evenly distributed on the circumference of the core assembly 211, and the three grooves 20111 correspond to the three-phase lines of the motor respectively. Three second connectors 2118 are provided on the core assembly 211, and the winding of the winding assembly 212 passes through one of the second connectors 2118 and forms a first connector 2117 to realize the first connector 2117 on the core assembly 211, while the other two second connectors 2118 are through-connected, and the other side also has a second connector 2118 outlet, and the other two outlets are through-connected. The first connectors 2117 on both sides of the core assembly 211 are respectively formed as convex and concave female and male end fittings.

[0553] In some embodiments, the winding assembly 212 and the core assembly 211 are stacked in sequence according to the three phases A, B, and C, that is, the winding assemblies 212 of the same phase are not adjacent. Therefore, as shown in Figure 122, the first connector 2117 on one side of the core assembly 211 needs to pass through multiple core assemblies 211 assembled with winding assemblies 212 of other phases to be connected to the core assembly 211 assembled with the winding assembly 212 of the same phase, so the first connector 2117 is longer.

[0554] It should be noted that in this embodiment, the connection of the same-phase winding assembly 212 is achieved through the first connector 2117, so that the same-phase winding connection does not require welding and is firm and reliable. The first connector 2117 passes through the inner side of the core assembly 211 without affecting the mutual movement between the second component 210 and the first component 220, thereby avoiding damage to the winding due to movement between the second component 210 and the first component 220, thereby ensuring the performance of the coil 2123.

[0555] In some embodiments, the connecting line 2121 respectively enters from the top and exits from the bottom of the wire passing channel 330. Three pipe outlets are provided at the bottom of the wire passing channel 330, and there are three wire outlets 311 on the center pole 300. The three pipe outlets of the wire passing channel 330, the three wire outlets of the center pole 300 and the three second joints 2118 on the core assembly 211 correspond one to one. During assembly, the wire passing channel 330 is provided on the center pole 300, and the connecting line 2121 respectively passes through the wire passing channel 330 and the wire outlet 311 of the center pole 300.

[0556] Through the above-mentioned arrangement, the output line can be fixed throughout the entire process, wherein the center rod 300 plays the role of fixing and protecting the wiring, which effectively solves the problem of the risk of extrusion and scratching in the prior art. In addition, a first limiting member 380 is provided on the top of the center rod 300, and the first limiting member 380 and the outlet of the center rod 300 jointly fix the connecting line 2121. At the same time, the first limiting member 380 is made of rubber material, which can buffer the impact of surrounding components on the connecting line 2121 under extreme working conditions, thereby protecting the connecting line 2121 and ensuring the reliability of the electrical system.

[0557] In summary, the wire outlet structure of the electromagnetic actuator 1000 of this embodiment utilizes the relative relationship of the surrounding components and is cleverly designed to solve the problem of wire outlet difficulties. It has the advantages of safety and reliability, easy assembly and disassembly, and compact space design.

[0558] In some embodiments, as shown in Figures 60, 61, and 62, an insulating frame 213 is provided between the core assembly 211 and the winding assembly 212. A lead wire channel 2131 is provided on the axial end surface of the insulating frame 213. The lead wire channel 2131 extends radially along the core assembly 211. The insulating frame 213 is provided between the core assembly 211 and the winding assembly 212 to achieve insulation coordination between the core assembly 211 and the winding assembly 212, thereby ensuring the performance of the second component 210.

[0559] At the same time, a lead channel 2131 extending radially along the core assembly 211 is set on the axial end face of the insulating skeleton 213, so that the lead wire 21231 of the coil 2123 can be led out to the outside of the core assembly 211, thereby facilitating the wiring of the coil 2123 and connecting to the power supply.

[0560] In some embodiments, as shown in Figures 123-127 , the outer peripheral wall of the insulating frame 213 is provided with a plurality of evenly spaced wire grooves 2132 , at least one of which is connected to the lead channel 2131 , thereby facilitating the extraction of the connecting wire 2121 connected to the coil 2123 .

[0561] It should be noted that by setting the insulating skeleton 213 of this embodiment, the core assembly 211, the winding assembly 212 and the insulating skeleton 213 can all be formed into independent components, reducing the design difficulty of the core assembly 211, the winding assembly 212 and the insulating skeleton 213. At the same time, the insulating skeleton 213 of this embodiment has the advantages of low processing difficulty, convenient maintenance, simple structure and high consistency in terms of layout space and production efficiency.

[0562] In some embodiments, as shown in Figures 123 to 127 , the insulating skeleton 213 is mainly composed of a lead channel 2131 , a second annular groove 2138 and a wire groove 2132 .

[0563] In some embodiments, as shown in Figures 123 and 126, the insulating skeleton 213 has six wire-passing grooves 2132 along its circumferential direction, and the positions of the six wire-passing grooves 2132 are evenly distributed, that is, the interval between two grooves is 60°. A second annular groove 2138 is provided on the surface of the insulating skeleton 213, and a winding space is formed between the second annular groove 2138, the inner wall 2136 of the second annular groove 2138 and the outer wall of the second annular groove 2138. The winding space is used to assemble the coil 2123.

[0564] In some embodiments, a second boss structure 2134 formed by the lead channel 2131 and an insulating portion 2135 formed by the wire groove 2132 are provided on the opposite side of the insulating skeleton 213 where the second annular groove 2138 is provided. The second boss structure 2134 and the insulating portion 2135 are mainly used to be nested with the structural parts on the core assembly 211, which greatly improves the space utilization and reduces the volume occupied by parts. Therefore, the volume of the entire structure can be reduced and the matching strength between the insulating skeleton 213 and the core assembly 211 is ensured.

[0565] Through the above-mentioned arrangement, when in use, the core assembly 211, the winding assembly 212 and the insulating skeleton 213 are assembled and combined into a separate module (as shown in FIG127 ), wherein the insulating skeleton 213 is nested in the first annular groove 21111 on the surface of the core assembly 211, wherein the second boss structure 2134 of the insulating skeleton 213 is combined with the wire arrangement groove 2013 in the first annular groove 21111, and the insulating portion 2135 formed by the wire groove 2132 is aligned with the groove 20111 in the circumferential direction of the core assembly 211, so that the coil 2123 has a larger operating space when connected in series outside the core assembly 211, which is beneficial to the subsequent welding connection between the coils 2123 and facilitates operation.

[0566] It should be noted that, in some embodiments, since the second component 210 is composed of stacked modules, and the modules are assembled by the core assembly 211, the winding assembly 212 and the insulating frame 213, the module located at the end of the second component 210 has the winding assembly 212 and the insulating frame 213 on only one side, and the module located in the axial middle of the second component 210 has the winding assembly 212 and the insulating frame 213 on both ends of the core assembly 211. When the three-phase power supply is connected, the same module The coils 2123 of the winding assembly 212 are in phase, and the lead and outlet positions of the coils 2123 differ by 180°. The lead of the coil 2123 passes through the lead channel 2131 on the insulating frame 213, and then extends to the periphery of the core assembly 211 through the wire groove 2132. The series wiring inside the module is carried out at the part where the wire grooves 2132 of the insulating frames 213 on both sides are connected, and the wiring is carried out by welding. Wiring at the wire groove 2132 has a larger operating space.

[0567] At the same time, since the lead channel 2131 is provided on the surface of the insulating frame 213, the structure of the insulating frame 213 is unique, which can effectively avoid assembly and wiring errors and improve production efficiency.

[0568] In some embodiments, when connected to a three-phase power supply, not only do the winding coils inside the module need to be connected in series, but the modules connected to the same-phase power supply also need to be connected in series. Both the lead spacing angle and the lead and output angle are multiples of 60°. Therefore, six evenly distributed wire slots 2132 are set along the circumferential direction of the extension on the insulating frame 213, which improves the versatility and utilization of parts, can greatly increase production efficiency, save costs, and facilitate mass production.

[0569] In some embodiments, an assembly hole 2137 is centrally defined in the insulating frame 213 to facilitate assembly of the insulating frame 213 with the core assembly 211. In the axial direction of the assembly hole 2137, the outer edge of the insulating frame 213 protrudes from the first annular groove 21111, and the inner edge of the insulating fixture 213 protrudes from the first annular groove 21111, thereby achieving insulation between the coil winding and the stator core.

[0570] In some embodiments, the inner sidewall 2136 is disposed around the outer periphery of the assembly hole 2137 to form a hollow cylinder with a certain wall thickness between the assembly hole 2137 of the insulating frame 213 and the second annular groove 2138 .

[0571] In some embodiments, a stepped limit platform is provided on the surface of the hollow cylinder, and two adjacent out-of-phase coils 2123 are separated by insulating paper 2122. The insulating paper 2122 is nested on the hollow cylinder where the wall thickness is thinner to facilitate fixing the insulating paper 2122. The structure is compact and the material utilization rate is high.

[0572] In some embodiments, the center rod 300 is provided with a first limiting structure, and the core assembly 211 is provided with a limiting portion. The limiting portion cooperates with the first limiting structure to limit the rotation of the core assembly 211 relative to the center rod 300. This improves the positional stability of the core assembly 211 and enables the center rod 300 and the housing 100 to effectively generate relative motion under the coupling of the first component 220 and the second component 210, thereby ensuring the operating performance of the electromagnetic actuator 1000.

[0573] In some embodiments, the limiting portion on the core assembly 211 can be understood as the positioning protrusion 21415 mentioned above.

[0574] In some embodiments, a cylindrical pin is provided between the core assembly 211 and the center rod 300 to limit the rotation of the core assembly 211 relative to the center rod 300 .

[0575] In some embodiments, as shown in Figures 128-131 , the center rod 300 is provided with a first positioning portion 340 (the specific structure of the first positioning portion 340 can be seen in Figure 25 ), and the core assembly 211 is provided with a second positioning portion 350. The first positioning portion 340 and the second positioning portion 350 cooperate to keep the center rod 300 and the core assembly 211 relatively stationary. This achieves circumferential positioning of the core assembly 211 and the center rod 300, preventing the core assembly 211 from rotating around the center rod 300 and ensuring the working performance of the core assembly 211.

[0576] In some embodiments, as shown in Figures 128-131 , the first positioning portion 340 is formed as a groove provided on the outer peripheral wall of the center rod 300, the second positioning portion 350 is formed as a groove provided on the core assembly 211, and the anti-rotation rod 360 is provided between the first positioning portion 340 and the second positioning portion 350. This is to limit the position of the center rod 300 and the core assembly 211, so that the center rod 300 and the core assembly 211 are relatively stationary, and the difficulty of limiting the position of the center rod 300 and the core assembly 211 is reduced, while ensuring that the output of the coil 2123 is consistent with the designed state.

[0577] It should be noted that the above arrangement can also avoid the problem that when the center rod 300 is mated with the tower top, the core assembly 211 rotates around the central axis of the center rod 300 together with the assembly nut 830, resulting in failure to tighten.

[0578] In some embodiments, as shown in conjunction with Figures 132-136 , the electromagnetic actuator 1000 further includes a first stopper 380 and a second stopper 390. The first stopper 380 and the second stopper 390 are spaced apart and arranged on the center rod 300 along the axial direction of the center rod 300. The first stopper 380 and the second stopper 390 respectively abut against the core assembly 211 to limit the axial displacement of the core assembly 211. This prevents the core assembly 211 from moving relative to the center rod 300 along the axial direction of the center rod 300, thereby facilitating a more stable installation of the core assembly 211 on the center rod 300 and preventing the magnetic core 211 from falling off the center rod 300, thereby ensuring stable and reliable installation of the core assembly 211 on the center rod 300.

[0579] In some embodiments, as shown in conjunction with Figures 132-136 , the first stopper 380 and the second stopper 390 are respectively adapted to abut against the inner wall of the housing 100 to limit the range of movement of the housing 100. This means that during movement of the housing 100, the first stopper 380 and the second stopper 390 can respectively abut against the inner wall of the housing 100, thereby limiting the range of movement of the housing 100 and ensuring the positional stability of the housing 100 during movement, thereby ensuring the operating performance of the electromagnetic actuator 1000.

[0580] In some embodiments, as shown in Figures 132-136 , one of the first stopper 380 and the second stopper 390 is integral with the center rod 300, while the other is separate from the center rod 300. The integral structure can reduce the number of components of the electromagnetic actuator 1000 and reduce the structural complexity of the electromagnetic actuator 1000.

[0581] In some embodiments, as shown in Figures 132 and 133, the first limiting member 380 and the center rod 300 are integrally formed. Since the relative position of the first limiting member 380 and the center rod 300 is unchanged, when the core assembly 211 is mounted on the center rod 300, it is convenient to achieve the coordination between the first limiting member 380 and the core assembly 211, so as to use the first limiting member 380 to limit the position of the core assembly 211 along the axial direction of the center rod 300.

[0582] In some embodiments, as shown in Figures 132 and 133, the center rod 300 is provided with a protrusion protruding radially outward to define the first limiting member 380, so that the first limiting member 380 and the center rod 300 are an integrally formed part, and the connection between the first limiting member 380 and the center rod 300 is eliminated.

[0583] In some embodiments, the other of the first limiting member 380 and the second limiting member 390 is threadedly engaged with the center rod 300. This means that when one of the first limiting member 380 and the second limiting member 390 is integral with the center rod 300, the other of the first limiting member 380 and the second limiting member 390 is threadedly engaged with the center rod 300 to achieve a fixed connection between the other of the first limiting member 380 and the second limiting member 390 and the center rod 300, ensuring the positional stability of the other of the first limiting member 380 and the second limiting member 390, thereby facilitating the first limiting member 380 and the second limiting member 390 to cooperate with each other to limit the axial displacement of the core assembly 211.

[0584] In some embodiments, the second limiting member 390 is formed as a threaded member, which is threadably engaged with the central rod 3000 so that the second limiting member 390 can be detachably disposed on the central rod 300 .

[0585] In some embodiments, in combination with Figures 132 and 134, the other of the first limit member 380 and the second limit member 390 includes a first part 391 and a second part 392, the first part 391 cooperates with the center rod 300, and in the radial direction of the center rod 300, the second part 392 is located radially outside the first part 391; in the axial direction of the center rod 300, the axial length of the first part 391 is greater than the axial length of the second part 392, a part of the second part 392 stops at the core assembly 211 and the other part is spaced apart from the core assembly 211. Among them, by setting the axial length of the first part 391 to be greater than the axial length of the second part 392, the area of ​​cooperation between the first part 391 and the center rod 300 is increased, thereby facilitating the other of the first limit member 380 and the second limit member 390 to be firmly set on the center rod 300. And because the core assembly 211 contains a wire outlet groove and a wiring harness, by setting the axial length of the first part 391 to be greater than the axial length of the second part 392, the axial length of the second part 392 can also be made smaller, which is convenient for avoiding the wiring harness.

[0586] At the same time, by positioning the second part 392 radially outward of the first part 391, it is possible to achieve a stop between a portion of the second part 392 and the core assembly 211, thereby utilizing the other of the first limiting member 380 and the second limiting member 390 to limit the axial displacement of the core assembly 211.

[0587] In addition, by spacing the other part of the second portion 392 from the core assembly 211, heat dissipation of the core assembly 211 is facilitated, and a gap exists between the other part of the second portion 392 and the core assembly 211, thereby avoiding stress concentration.

[0588] It needs to be explained here that, with respect to the inner and outer sides being the axis of the center rod 300 , the first part 391 is closer to the center rod 300 , and the second part 392 is farther from the center rod 300 . Therefore, in the radial direction of the center rod 300 , the second part 392 is located radially outside the first part 391 .

[0589] In some embodiments, in combination with Figures 135 and 136, the other of the first limit member 380 and the second limit member 390 is installed to the end of the center rod 300 and a portion of it extends into the center rod 300, so that the other of the first limit member 380 and the second limit member 390 can be detachably set in the center rod 300. In this way, after the core assembly 211 is axially sleeved on the center rod 300, at least one of the first limit member 380 and the second limit member 390 is installed on the center rod 300 to limit the axial displacement of the core assembly 211 along the center rod 300 after the core assembly 211 is installed in place.

[0590] In some embodiments, the second portion 392 of the other of the first and second stoppers 380 and 390 is formed as a mounting structure having a buffer. This allows the other of the first and second stoppers 380 and 390 to be fixedly mounted to the center rod 300 while also providing a buffering effect.

[0591] In some embodiments, the first limiting member 380 and the second limiting member 390 are made of rubber material, so that the first limiting member 380 and the second limiting member 390 can play a buffering role.

[0592] In some embodiments, as shown in Figures 135 and 136, the second limit member 390 is installed to the end of the center rod 300 and a portion of it extends into the center rod 300. The second limit member 390 includes a piston portion 393. The piston portion 393 is made of an elastic material. When the piston portion 393 is extended into the center rod 300, the piston portion 393 is elastically deformed and compressed to have an interference fit with the center rod 300 to fix the piston portion 393 on the center rod 300.

[0593] Part of the structure of the second limiter 390 protrudes from the piston portion 393 along the radial direction of the center rod 300 , and part of the structure of the second limiter 390 cooperates with the core assembly 211 to limit the displacement of the core assembly 211 along the axial direction of the center rod 300 .

[0594] In some embodiments, the first limiting member 380 and the second limiting member 390 are further formed as limiting members of the second component 210 to limit the relative displacement of the second component 210 .

[0595] In some embodiments, during the operation of the electromagnetic actuator 1000, the core assembly 211 and the housing 100 will undergo relative linear motion. The first limit member 380 can simultaneously serve as a lower limit for limiting the movement of the housing 100, and the second limit member 390 can simultaneously serve as an upper limit for limiting the movement of the housing 100.

[0596] In a specific embodiment, the first limiter 380 serves to limit the press-fitting depth of the core assembly 211. After the press-fitting is completed, the second limiter 390 is connected to the bottom of the center rod 300 to prevent the core assembly 211 from falling off axially downward.

[0597] It should be noted that specific implementation forms of the first limiting member 380 and the second limiting member 390 include but are not limited to nuts, pistons, integrated step surfaces, etc.

[0598] In some embodiments, as shown in Figures 128, 129, and 130, at least one cooling chamber 320 for accommodating a cooling medium is provided within the center rod 300. This allows the center rod 300 to be filled with the cooling medium, which facilitates heat dissipation from the core assembly 211, thereby ensuring long-term and efficient operation of the electromagnetic actuator 1000 and preventing damage to internal components of the electromagnetic actuator 1000.

[0599] In some embodiments, the inner wall of the center rod 300 is hollow to form a cooling chamber 320. Before assembly, the cooling medium is added from the filling port 323 (the specific structure of the filling port 323 can be seen in Figure 25), and then the filling port 323 is sealed to make the cooling chamber 320 a sealed cavity. When the electromagnetic actuator 1000 is running, the heat on the core assembly 211 is transferred to the cooling medium through the center rod 300, and the cooling medium transfers the heat to the air through a heat exchange cycle, thereby ensuring the long-term and efficient operation of the electromagnetic actuator 1000 and avoiding damage to internal components.

[0600] At the same time, this design does not require additional components such as cooling pipes, and the entire cooling solution has a compact structure.

[0601] In some embodiments, the radial projection of at least a portion of the cooling chamber 320 is arranged to overlap with the core assembly 211. This allows at least a portion of the cooling chamber 320 to be radially directed toward the core assembly 211, facilitating heat dissipation from the core assembly 211 using the cooling medium within the cooling chamber 320. This ensures that the electromagnetic actuator 1000 can operate efficiently and long-term, and prevents damage to internal components of the electromagnetic actuator 1000.

[0602] In some embodiments, at least a portion of the cooling chamber 320 is located outside the accommodating chamber 130. This facilitates the delivery of the cooling medium to the cooling chamber 320 and also helps cool the cooling medium, thereby ensuring the heat dissipation performance of the cooling medium.

[0603] In some embodiments, the electromagnetic actuator 1000 further includes a first cooling pipe disposed within the cooling chamber 320, with a first cooling cavity formed between the first cooling pipe and the cooling chamber 320. One of the first cooling cavity and the first cooling pipe is adapted to communicate with the first water inlet, and the other is adapted to communicate with the first water outlet (not shown in this example figure). This allows the cooling medium to circulate between the first cooling cavity and the first cooling pipe, thereby facilitating the use of the cooling medium to dissipate heat from the core assembly 211 and ensuring the cooling performance of the cooling medium.

[0604] In some embodiments, the first cooling tube is spaced apart from the inner wall of the cooling chamber 320 so that a connecting channel is formed between the first cooling tube and the cooling chamber 320. The connecting channel is used to connect the first cooling chamber and the first cooling tube. In this way, when one of the first cooling chamber and the first cooling tube is connected to the first water inlet and the other is connected to the first water outlet, the cooling medium between the first water inlet and the first water outlet can flow through the first cooling chamber and the first cooling tube in sequence, which is conducive to the circulation of the cooling medium and facilitates the use of the cooling medium to dissipate heat from the core assembly 211.

[0605] In some embodiments, as shown in conjunction with Figures 137-140, the electromagnetic actuator 1000 further includes a second cooling pipe 32111 and a third cooling pipe 32121. The second cooling pipe 32111 and the third cooling pipe 32121 are both disposed within the cooling chamber 320 and communicate with the cooling chamber 320. One of the second cooling pipe 32111 and the third cooling pipe 32121 is adapted to communicate with the second water inlet 3211, and the other is adapted to communicate with the second water outlet 3212. In this way, the cooling medium can enter the cooling chamber 320 through the second water inlet 3211 and be discharged from the cooling chamber 320 through the second water outlet 3212, thereby facilitating the circulation of the cooling medium.

[0606] In some embodiments, as shown in Figures 138 and 139, the second cooling pipe 32111 is connected to the second water inlet 3211, and the third cooling pipe 32121 is connected to the second water outlet 3212, so that the cooling medium can enter the cooling chamber 320 through the second cooling pipe 32111 and be discharged from the cooling chamber 320 through the third cooling pipe 32121, which is conducive to the circulation of the cooling medium.

[0607] In some embodiments, as shown in conjunction with FIG. 139 and FIG. 140 , the cooling chamber 320 is provided in a plurality and includes a first cooling chamber 321 and a second cooling chamber 322. In the axial direction of the center rod 300, the first cooling chamber 321 is located on one side of the core assembly 211, and at least a portion of the second cooling chamber 322 is disposed directly opposite the core assembly 211. This allows at least a portion of the cooling chamber 320 to overlap with the core assembly 211 in the radial direction, facilitating heat dissipation from the core assembly 211 using the cooling medium within the cooling chamber 320, thereby ensuring long-term, efficient operation of the electromagnetic actuator 1000 and preventing damage to internal components of the electromagnetic actuator 1000.

[0608] Through the unfamiliar setting, the first cooling chamber 321 and the second cooling chamber 322 can be used to dissipate heat from different parts of the electromagnetic actuator 1000 respectively, and interact with each other to ultimately ensure that the electromagnetic actuator 1000 maintains efficient operation. The center rod 300 plays a role in rapid heat conduction and heat dissipation during the entire cooling process.

[0609] In some embodiments, the second cooling chamber 322 is formed as a closed chamber and is filled with a cooling medium.

[0610] In some embodiments, as shown in FIG139 and FIG140 , there are multiple second cooling chambers 322 spaced apart along the circumference of the central rod 300 , and each second cooling chamber 322 includes multiple sub-chambers 3221 spaced apart along the circumference of the central rod 300 , to ensure the heat dissipation performance of the cooling chamber 320 .

[0611] In some embodiments, the ends of the multiple sub-chambers 3221 of each second cooling chamber 322 are connected in the axial direction of the central rod 300. This allows the cooling medium in each second cooling chamber 322 to circulate among the multiple sub-chambers 3221, thereby ensuring the heat dissipation performance of the second cooling chamber 322.

[0612] In some embodiments, at least a portion of the cooling chamber 320 is formed as a heat pipe, so that the cooling chamber 320 itself has heat dissipation capabilities, thereby reducing the temperature of the cooling medium and ensuring the cooling effect of the cooling medium.

[0613] In some embodiments, a cooling structure 810 is provided on the central rod 300 (the specific structure of the cooling structure 810 can be seen in FIG22 ). The cooling structure 810 is provided on the portion of the central rod 300 extending out of the accommodating cavity 130. The cooling structure 810 is used to reduce the temperature of the cooling medium and ensure the cooling effect of the cooling medium.

[0614] In some embodiments, the cooling structure 810 includes a heat sink to improve the heat dissipation performance of the cooling structure 810 , thereby utilizing the cooling structure 810 to reduce the temperature of the cooling medium and ensure the cooling effect of the cooling medium.

[0615] In some embodiments, the cooling structure 810 includes a cooling pipeline having a third water inlet and a third water outlet formed therein, which are connected to the outside world. The third water inlet and the third water outlet are used to transport a cooling medium with a lower external temperature into the cooling structure 810, thereby lowering the temperature of the cooling medium within the cooling structure 810. This also ensures the heat dissipation performance of the cooling structure 810, thereby enabling the cooling structure 810 to effectively lower the temperature of the cooling medium and ensure the cooling effect of the cooling medium.

[0616] In some embodiments, as shown in FIG137 , the housing 100 is provided with a guide rod 400, and the center rod 300 is formed with a guide hole 310, with the guide rod 400 engaging with the guide hole 310. This prevents the housing 100 from deflecting during movement, that is, ensures that the housing 100 can move in a predetermined direction and ensures the accuracy of the movement of the housing 100.

[0617] In some embodiments, a cooling cavity is provided on the guide rod 400 and is adapted to contain a coolant. This allows the coolant to dissipate heat from the core assembly 211, thereby ensuring that the electromagnetic actuator 1000 can operate efficiently and for a long time without damaging internal components of the electromagnetic actuator 1000.

[0618] In some embodiments, the volume of the cooling cavity is greater than the volume of the coolant. That is, the coolant does not fill the entire cooling cavity, so that the coolant in the cooling cavity can undergo a gas-liquid conversion process to ensure the cooling performance of the coolant.

[0619] In some embodiments, the radial projection of the cooling cavity is at least partially overlapped with the core assembly 211. This allows the cooling cavity to be radially directed toward the core assembly 211, facilitating heat dissipation from the core assembly 211 using the coolant in the cooling cavity, thereby ensuring long-term and efficient operation of the electromagnetic actuator 1000 and preventing damage to internal components of the electromagnetic actuator 1000.

[0620] In some embodiments, the radial projections of the core assembly 211 that overlap with the cooling cavity partially overlap with the radial projections of the cooling chamber 320. In other words, a portion of the core assembly 211 faces both the cooling cavity on the guide rod 400 and the cooling chamber 320 on the center rod 300, maximizing the heat dissipation performance of the core assembly 211.

[0621] The vibration reduction device 5000 according to an embodiment of the present application is described below.

[0622] A vibration reduction device 5000 according to an embodiment of the present application includes: an electromagnetic actuator 1000 .

[0623] The electromagnetic actuator 1000 is the aforementioned electromagnetic actuator 1000 , and the specific structure of the electromagnetic actuator 1000 is not described here in detail. The electromagnetic actuator 1000 is suitable for being connected between the wheel 2000 and the vehicle body.

[0624] It can be seen from the above structure that the vibration reduction device 5000 of the embodiment of the present application can ensure the working performance of the vibration reduction device 5000 by adopting the aforementioned electromagnetic actuator 1000.

[0625] In some embodiments, one of the wheel 2000 and the vehicle body is adapted to be connected to the other of the first assembly 220 and the second assembly 210, and the other of the wheel 2000 and the vehicle body is adapted to be connected to the housing 100. This allows the wheel 2000 and the vehicle body to move relative to each other, thereby achieving a buffering and vibration-absorbing effect, ensuring the performance of the vibration reduction device 5000, and improving the comfort of the vehicle 20000.

[0626] In some embodiments, the housing 100 is adapted to be connected to the wheel 2000, and the other of the first assembly 220 and the second assembly 210 is adapted to be connected to the vehicle body. This allows the electromagnetic actuator 1000 to be connected between the wheel 2000 and the vehicle body, facilitating the use of the electromagnetic actuator 1000 for vibration absorption and ensuring the performance of the vibration reduction device 5000.

[0627] In some embodiments, as shown in Figures 20-26 , the vibration damping device 5000 further includes a center rod 300, with a portion of the center rod 300 extending out of the housing 100. This facilitates a fixed connection between the center rod 300 and the vehicle body, reducing the difficulty of connecting the center rod 300 to the vehicle body. This allows the electromagnetic actuator 1000 to be connected between the wheel 2000 and the vehicle body, ensuring the operating performance of the vibration damping device 5000 and improving the comfort of the vehicle 20000.

[0628] In some embodiments, as shown in Figures 21 and 22 , the second assembly 210 includes a core assembly 211 and a winding assembly 212. The core assembly 211 is disposed on the center rod 300, and the winding assembly 212 is disposed on the core assembly 211. The first assembly 220 is connected to the housing 100. This allows relative movement between the second assembly 210 and the first assembly 220, allowing the vibration damping device 5000 to buffer impacts transmitted from the road surface while isolating noise input from the road surface and the wheels 2000 to ensure the comfort of the vehicle 20000.

[0629] In some embodiments, the center rod 300 is adapted to be connected to the vehicle body via the upper support 500 , so as to realize the connection between the vibration reduction device 5000 and the vehicle body and reduce the difficulty of connecting the vibration reduction device 5000 and the vehicle body.

[0630] In some embodiments, the upper support 500 is adapted to be integrated with the vehicle body, so as to realize the connection between the vibration damping device 5000 and the vehicle body and reduce the difficulty of connecting the vibration damping device 5000 and the vehicle body.

[0631] In some embodiments, as shown in FIG7 , a mounting seat 191 is formed on the housing 100, and the vibration damping device 5000 further includes a spring 600. One end of the spring 600 is adapted to connect to the mounting seat 191, and the other end of the spring 600 is adapted to connect to the vehicle body. The spring 600 is used to provide a portion of the damping force and withstand some of the vibration impact, thereby improving the performance of the vibration damping device 5000 and ensuring the comfort of the vehicle 20000.

[0632] In some embodiments, the spring 600 includes at least one of an air spring and a coil spring to ensure the working performance of the spring 600 and ensure that the spring 600 can effectively provide a partial damping force and withstand a partial vibration impact.

[0633] In some embodiments, as shown in FIG22 , the housing 100 has an end cap 1012 , on which a mounting bracket 192 is disposed. The mounting bracket 192 is adapted to be connected to the wheel 2000 , and the mounting bracket 192 and the end cap 1012 are integrally formed. This allows the electromagnetic actuator 1000 to be connected to the wheel 2000 , and thus the vibration damping device 5000 to be connected to the wheel 2000 . This reduces the difficulty of connecting the vibration damping device 5000 to the wheel 2000 , facilitates the use of the vibration damping device 5000 to buffer impacts transmitted from the road surface, and simultaneously isolates noise input from the road surface and tires, thereby ensuring the comfort of the vehicle 20000 .

[0634] In some embodiments, a steering shaft avoidance structure is formed on the mounting bracket 192, so that the mounting bracket 192 can effectively avoid the steering shaft and ensure the performance of the steering shaft.

[0635] In some embodiments, the vibration reduction device 5000 further includes a vibration absorber, which is arranged in parallel with the electromagnetic actuator 1000 to maximize the vibration reduction effect of the vibration reduction device 5000.

[0636] The suspension system 10000 according to an embodiment of the present application will be described below with reference to the accompanying drawings.

[0637] As shown in Figures 174 and 175, a suspension system 10000 according to an embodiment of the present application includes: a vibration reduction device 5000.

[0638] The vibration reduction device 5000 is the aforementioned vibration reduction device 5000 , and the specific structure of the vibration reduction device 5000 is not described in detail here.

[0639] As can be seen from the above structure, the suspension system 10000 of the embodiment of the present application can ensure the working performance of the suspension system 10000 by adopting the aforementioned vibration reduction device 5000.

[0640] In some embodiments, at least one wheel 2000 is adapted to correspond to a vibration damping device 5000 , so that the vibration damping device 5000 can be used to cushion the impact transmitted by the road surface while isolating the noise input from the road surface and the wheel 2000 to ensure the comfort of the vehicle 20000 .

[0641] In some embodiments, the suspension system 10000 further includes a controller adapted to control the electromagnetic actuator 1000. This allows the electromagnetic actuator 1000 to operate effectively to cushion impacts transmitted from the road surface while isolating noise input from the road surface and the wheels 2000 to ensure the comfort of the vehicle 20000.

[0642] In some embodiments, the plurality of wheels 2000 are adapted to correspond to the vibration damping devices 5000. That is, each of the plurality of wheels 2000 is provided with a corresponding vibration damping device 5000, so that the vibration damping device 5000 can be used to cushion the impact transmitted by the road surface while isolating the noise input from the road surface and the wheels 2000 to ensure the comfort of the vehicle 20000.

[0643] In some embodiments, the suspension system 10000 further includes a controller adapted to control the plurality of wheels 2000 so that the plurality of corresponding vibration damping devices 5000 can all buffer the impact transmitted by the road surface, thereby ensuring the comfort of the vehicle 20000 .

[0644] In some embodiments, the suspension system 10000 further includes multiple controllers, each of which corresponds to each of the wheels 2000. This means that each wheel 2000 corresponds to a controller, so that the controller can individually control the vibration damping device 5000 corresponding to the wheel 2000 to ensure the performance of the vibration damping device 5000.

[0645] In some embodiments, the suspension system 10000 further includes multiple controllers, each of which is adapted to control at least one wheel 2000. In other words, one controller can control one wheel 2000 or multiple wheels 2000, so that the vibration damping device 5000 corresponding to each wheel 2000 can operate, thereby ensuring the performance of the vibration damping device 5000.

[0646] In some embodiments, as shown in Figures 174 and 175 , the suspension system 10000 further includes a leaf spring 3000, with both ends of the leaf spring 3000 adapted to connect to the steering knuckle 4000. This allows the leaf spring 3000 to effectively cushion the impact of road jolts and vibrations during vehicle 20000's travel by bending and deforming upward and downward, providing a more comfortable ride for the driver and passengers.

[0647] In some embodiments, the extension of the leaf spring 3000 in the width direction of the vehicle 20000 is greater than the distance between the two coaxial vibration damping devices 5000 in the width direction of the vehicle 20000 , so as to ensure the performance of the leaf spring 3000 .

[0648] In some embodiments, the leaf spring 3000 is formed with a first mounting point adapted to connect to the subframe 6000 and a second mounting point adapted to connect to the steering knuckle 4000, with the first mounting point being higher than the second mounting point. This increases the maximum vertical displacement of the leaf spring 3000 during deformation buffering, thereby reducing interference with the subframe 6000 and other structures when the wheel 2000 of the vehicle 20000 bounces. This effectively reduces fatigue damage to the leaf spring 3000, allowing the leaf spring 3000 to perform a stable buffering operation and extending its service life.

[0649] In some embodiments, the distance between the first mounting point and the second mounting point in the height direction of the vehicle 20000 is greater than the maximum deflection of the leaf spring 3000 at the second mounting point. This allows the leaf spring 3000 to remain stably within a suitable tensile deformation range during use, thereby effectively delaying fatigue damage of the leaf spring 3000 and extending the service life of the leaf spring 3000.

[0650] The vehicle 20000 of an embodiment of the present application is described below with reference to the accompanying drawings.

[0651] As shown in FIG. 176 , a vehicle 20000 according to an embodiment of the present application includes: a suspension system 10000 .

[0652] The suspension system 10000 is the aforementioned suspension system 10000 , and the specific structure of the suspension system 10000 is not described in detail here.

[0653] As can be seen from the above structure, the vehicle 20000 of the embodiment of the present application, by adopting the aforementioned suspension system 10000, can effectively reduce the difficulty of assembling the vehicle 20000 and ensure the working performance of the vehicle 20000.

[0654] The electromagnetic actuator 1000 , the vibration reduction device 5000 , the suspension system 10000 and other components of the vehicle 20000 according to the embodiment of the present application are well known to those skilled in the art and will not be described in detail here.

[0655] Throughout this specification, references to terms such as "embodiment" and "example" indicate that the specific features, structures, materials, or characteristics described in conjunction with that embodiment or example are included in at least one embodiment or example of the present application. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

[0656] Although the embodiments of the present application have been shown and described, those skilled in the art will appreciate that various changes, modifications, substitutions, and variations may be made to the embodiments without departing from the principles and intent of the present application, and that the scope of the present application is defined by the claims and their equivalents.

Claims

1. An electromagnetic actuator, wherein, Comprising: A first component; A second component, the second component being coupled to the first component such that the first component and the second component are relatively movable; A detection module for detecting the relative displacement between the first component and the second component.

2. The electromagnetic actuator according to claim 1, wherein, Further comprising a housing within which a receiving cavity is formed, the first component and the second component are both disposed within the receiving cavity, one of the first component and the second component is connected to the housing, and the first component and the second component are coupled such that one of the first component and the second component moves along an axis relative to the housing.

3. The electromagnetic actuator according to claim 2, wherein, The detection module includes a laser sensor disposed at the top or bottom of the receiving cavity.

4. The electromagnetic actuator according to claim 3, wherein, The housing is adapted to be fixed to an axle, and the electromagnetic actuator further includes a mounting bracket mounted to the outside of the housing and adapted to connect the axle to the housing. The laser sensor is disposed within the mounting bracket, and an avoidance hole for avoiding the optical path of the laser sensor is provided in the bottom wall of the receiving cavity.

5. The electromagnetic actuator according to claim 2, wherein, Further comprising a central rod connecting the other of the first component and the second component; The detection module includes a first detection member and a second detection member coupled to the first detection member, and one of the housing and the central rod is provided with the first detection member and the other is provided with the second detection member.

6. The electromagnetic actuator according to claim 5, wherein, The housing is adapted to be fixed to an axle, and the central rod passes through the top wall of the housing to be connected to the vehicle body; The first detection member is disposed on the housing, and the second detection member is disposed on the central rod.

7. The electromagnetic actuator according to claim 5 or 6, wherein, The first detection member is disposed on the outside of the housing.

8. The electromagnetic actuator according to any one of claims 5-7, wherein, A bearing is provided between the central rod and the housing, and a part of the projection of the first detection member that coincides with the housing in the radial direction overlaps with a part of the projection of the bearing in the radial direction.

9. The electromagnetic actuator according to any one of claims 5-7, wherein, A bearing is provided between the central rod and the housing, and the first detection member is spaced apart from the bearing.

10. The electromagnetic actuator according to any one of claims 5-9, wherein, The bottom of the housing is provided with a mounting bracket, and an avoidance channel communicating with the receiving cavity is provided within the mounting bracket; At least a part of the second detection member is located within the avoidance channel, and the first detection member can move into the avoidance channel to be coupled to the second detection member.

11. The electromagnetic actuator according to any one of claims 5-10, wherein, The second detection member is formed in an arc shape.

12. A vibration damping device, wherein, Comprising the electromagnetic actuator according to any one of claims 1-11, the electromagnetic actuator being adapted to be connected between a wheel and a vehicle body.

13. A suspension system, wherein, Comprising the shock absorber according to claim 12.

14. A vehicle, wherein, Comprising the suspension system according to claim 13.

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