Radar installation device and automatic guided vehicle

Abstract

The invention relates to a radar installation device and an automatic guided vehicle, and relates to the technical field of damping. The radar installation device comprises a fixing assembly, a supporting assembly and a first damping assembly. The fixing assembly is installed on the sports equipment. The supporting assembly is rotatably arranged on the fixing assembly with the joint of the supporting assembly and the fixing assembly as a fulcrum, and the supporting assembly is provided with a first end and a second end which are located at the two opposite ends of the fulcrum. The second end is provided with the radar. The first damping assembly is installed on the sports equipment and connected with the first end of the supporting assembly. Damping of the radar mounting device in the moving process can be reduced, and the stability of the radar is improved.

Description

Technical Field

[0001] The present application relates to the field of shock absorption technology, and in particular to a radar installation device and an automatic guided vehicle. Background Art

[0002] In the related technology, the installation methods of radar are mostly divided into two types: pure mechanical installation structure and installation with electronic components. The pure mechanical installation structure adopts a fixed rigid body connection, and the radar is installed on the mounting frame, or a simple mounting bracket is used with a shock-absorbing spring. The shock-absorbing effect is very limited, and it does not have the function of adjusting the level and scanning angle. The leveling method used with components requires the use of leveling sensors and hydraulic devices, and the structure is relatively complicated. Summary of the invention

[0003] Based on this, it is necessary to provide a radar installation device and an automatic guided vehicle to address the problem of poor radar shock absorption effect.

[0004] To achieve the above objectives, the technical solutions adopted in this application are as follows:

[0005] In a first aspect, an embodiment of the present application provides a radar installation device for installing a radar on a sports device, the radar installation device comprising:

[0006] A fixing assembly mounted on the sports equipment;

[0007] a supporting component, rotatably disposed on the fixing component with its connection with the fixing component as a fulcrum, and the supporting component has a first end and a second end located at opposite ends of the fulcrum; the radar is mounted on the second end; and

[0008] A first shock absorbing assembly is mounted on the sports equipment and connected to the first end of the supporting assembly.

[0009] Through the above design, due to the shock-absorbing effect of the first shock-absorbing component, the up and down vibration amplitude generated at one end of the support component connected to the moving device is reduced. Correspondingly, the vibration amplitude of the radar located at the opposite end is reduced, which meets the scanning angle adjustment of the radar during the movement and reduces the vibration of the radar, thereby maintaining operational stability.

[0010] In one embodiment of the first aspect, the first shock absorbing assembly includes a first mounting plate and a plurality of first buffer members, the first mounting plate is connected to the sports equipment, and each of the first buffer members is mounted on the first mounting plate and connected to the first end of the support assembly.

[0011] Through the above design, the first buffer component provides a shock-absorbing effect to the supporting assembly during the movement of the sports equipment.

[0012] In one embodiment of the first aspect, the radar mounting device further includes a second shock absorbing assembly, wherein the second shock absorbing assembly is mounted on the second end of the supporting assembly, and the radar is mounted on the second shock absorbing assembly.

[0013] Through the above design, the second shock absorbing component can cooperate with the first shock absorbing component to further reduce the vibration amplitude of the radar.

[0014] In one embodiment of the first aspect, the second shock absorbing assembly includes a second mounting plate and a plurality of second buffer members, the radar is mounted on the second mounting plate, and two ends of each of the second buffer members are respectively connected to the second mounting plate and the second end of the supporting assembly.

[0015] Through the above design, during the vibration of the support assembly, the second buffer member reduces the vibration of the second mounting plate and the radar.

[0016] In one embodiment of the first aspect, the second shock absorbing assembly further includes a mounting seat, a third mounting plate and a third buffer member, the mounting seat and each of the third buffer members are fixed to a side of the second mounting plate facing away from the second buffer member, the third mounting plate is arranged on a side of the third buffer member facing away from the second mounting plate and abuts against the mounting seat, and the radar is mounted on a side of the mounting seat facing away from the second mounting plate and exposed to the third mounting plate.

[0017] Through the above design, the third mounting plate can limit the top side of the mounting seat, fix the mounting seat, and maintain the stability of the mounting seat.

[0018] In one of the embodiments of the first aspect, the second shock absorbing assembly further comprises a plurality of locking members, the second mounting plate is correspondingly provided with a plurality of waist-shaped grooves, and each of the locking members passes through the third mounting plate, the third buffer member and the waist-shaped groove in sequence.

[0019] Through the above design, the locking position can be synchronously adjusted according to the rotation of the mounting seat, the locking member moves in the waist-shaped groove, and is locked after reaching the set angle, thereby satisfying the horizontal viewing angle adjustment of the radar.

[0020] In one embodiment of the first aspect, the support assembly includes a support frame and a rotating shaft, the support frame includes a first plane section and an inclined surface section located at the first end, and a second plane section located at the second end, the first plane section and the second plane section are respectively connected to two ends of the inclined surface section, and the rotating shaft is fixed to one side of the inclined surface section and is rotatably connected to the fixing assembly;

[0021] The first plane section is connected to the first shock absorbing assembly, and the second plane section is installed with the radar; the length from one end of the inclined section close to the first plane section to the rotating axis is greater than the length from one end of the inclined section close to the second plane section to the rotating axis.

[0022] Through the above design, the vibration force applied to the radar is greater than the vibration force of the first plane segment, so that the radar can be significantly damped through the second buffer and the third buffer, and the radar can maintain corresponding visual angle tracking during the vibration process.

[0023] In one embodiment of the first aspect, the rotating shaft is an eccentric shaft.

[0024] Through the above design, the connection height of the support base relative to the fixed component is adjusted, so as to adjust the scanning area of ​​the radar within a certain upper and lower angle range.

[0025] In a second aspect, an embodiment of the present application further provides an automatic guided vehicle, comprising the radar installation device described in any of the above embodiments.

[0026] Through the above design, the radar vibration reduction of the automatic guided vehicle during its movement is achieved, thereby ensuring the normal operation of the radar.

[0027] In one embodiment of the second aspect, the automatic guided vehicle further includes a walking shock absorbing part and a rigid body part, the first shock absorbing assembly is installed on the walking shock absorbing part, and the fixing assembly is installed on the rigid body part.

[0028] Through the above design, the first shock absorbing component can be regarded as being stationary relative to the vehicle body, and the second shock absorbing component equipped with the radar works to achieve the shock absorbing effect of the radar during the moving process.

[0029] In one embodiment of the second aspect, the automatic guided vehicle further includes a walking shock absorbing part and a rigid body part, and the first shock absorbing assembly and the fixing assembly are simultaneously installed on either the walking shock absorbing part or the rigid body part.

[0030] Through the above design, the first shock absorbing assembly and the second shock absorbing assembly operate synchronously to reduce the vibration amplitude of the radar.

[0031] Compared with the related art, the beneficial effect of the present application is as follows: the present application provides a radar installation device and an automatic guided vehicle, which can be used to reduce the shock of a moving radar. The radar installation device includes a fixing component, a supporting component and a first shock absorbing component. Among them, the fixing component is installed on the moving device, the supporting component is rotatably connected to the fixing component, and the radar and the first shock absorbing component are respectively installed at both ends of the supporting component. In this way, during the movement of the moving device, the radar installation device moves with the moving device, thereby generating vibration. Through the lever structure formed by the supporting component, the radar can adjust the angle during the vibration process to maintain stable operation. At the same time, the first shock absorbing component can synchronously reduce the shock absorption of the radar installation device during the movement process, further improving the stability of the radar. BRIEF DESCRIPTION OF THE DRAWINGS

[0032] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0033] Figure 1 This is a schematic diagram of the axonometric structure of a radar installation device in some embodiments of the present application;

[0034] Figure 2 This is a schematic diagram of the side structure of a radar installation device in some embodiments of the present application;

[0035] Figure 3 For this application Figure 1 A schematic diagram of the enlarged structure of part A;

[0036] Figure 4 This is a schematic diagram of the structure of the support assembly in some embodiments of the present application;

[0037] Figure 5 This is a schematic diagram of the top view of the radar installation device in some embodiments of the present application.

[0038] Description of reference numerals:

[0039] 100, radar installation device; 110, fixing assembly; 111, fixing seat; 120, supporting assembly; 121, supporting frame; 1211, inclined section; 1212, first plane section; 1213, second plane section; 122, rotating shaft; 130, first shock absorbing assembly; 131, first mounting plate; 132, first buffer; 140, second shock absorbing assembly; 141, second mounting plate; 142, second buffer; 143, third buffer; 144, mounting seat; 145, third mounting plate; 146, waist groove;

[0040] 200. Radar. DETAILED DESCRIPTION

[0041] In order to make the above-mentioned purposes, features and advantages of the present application more obvious and easy to understand, the specific implementation methods of the present application are described in detail below in conjunction with the accompanying drawings. In the following description, many specific details are set forth to facilitate a full understanding of the present application. However, the present application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without violating the connotation of the present application, so the present application is not limited by the specific embodiments disclosed below.

[0042] In the description of the present application, it should be understood that if the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. appear, the orientation or position relationship indicated by these terms is based on the orientation or position relationship shown in the accompanying drawings, which is only for the convenience of describing the present application and simplifying the description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present application.

[0043] In addition, if the term "and / or" appears, "and / or" is merely a description of the association relationship of associated objects, indicating that three relationships may exist, for example, A and / or B can represent: A exists alone, A and B exist at the same time, and B exists alone. In addition, the character " / " in this article generally indicates that the objects associated before and after are in an "or" relationship. If the terms "first" and "second" appear, these terms are only used for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In the description of this application, if the term "multiple" appears, the meaning of "multiple" is at least two, such as two, three, etc., unless otherwise clearly and specifically defined.

[0044] In this application, unless otherwise clearly specified and limited, if the terms "installed", "connected", "connected", "fixed" and the like appear, these terms should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integrated connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements, unless otherwise clearly defined. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to the specific circumstances.

[0045] In the present application, unless otherwise clearly specified and limited, if there is a description that a first feature is "above" or "below" a second feature, etc., or similar descriptions appear, it may mean that the first and second features are in direct contact, or that the first and second features are in indirect contact through an intermediate medium. Moreover, the first feature being "above", "above" and "above" the second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. The first feature being "below", "below" and "below" the second feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature is lower in level than the second feature.

[0046] It should be noted that if an element is referred to as being "fixed to" or "disposed on" another element, it may be directly on the other element or there may be a central element. If an element is considered to be "connected to" another element, it may be directly connected to the other element or there may be a central element at the same time. If any, the terms "vertical", "horizontal", "upper", "lower", "left", "right" and similar expressions used in this application are for illustrative purposes only and do not represent the only implementation method.

[0047] See also Figure 1 As shown, an embodiment of the present application provides a radar installation device 100 for installing a radar 200 on a moving device to improve the operating stability of the radar 200 in a moving state.

[0048] It is understandable that in the embodiments of the present application, the motion equipment may include AGV (Automated Guided Vehicle), AMR (Autonomous Mobile Robot), automobile, transport vehicle and other equipment with mobile functions. For ease of understanding, the motion equipment in the embodiments of the present application can be an automatic guided vehicle as an application scenario.

[0049] Specifically, the radar installation device 100 includes a fixing component 110, a supporting component 120 and a first shock absorbing component 130. The fixing component 110 is installed on the moving device. The supporting component 120 is rotatably arranged on the fixing component 110 with the connection between the fixing component 110 and the fixing component 110 as a fulcrum, and the supporting component 120 has a first end and a second end located at opposite ends of the fulcrum, and the second end of the supporting component 120 is installed with the radar 200. The first shock absorbing component 130 is installed on the moving device and connected to the first end of the supporting component 120 away from the radar 200.

[0050] Exemplarily, the fixing assembly 110 may be a metal component, which may be fixed to the moving equipment by bolt locking or welding, so as to provide a mounting fulcrum for the radar installation device 100, and the radar installation device 100 may be installed as a whole on the moving equipment. The middle part of the support assembly 120 is rotatably connected to the fixing assembly 110, so that it can rotate relative to the fixing assembly 110. The radar 200 and the first shock absorbing assembly 130 are respectively installed at both ends of the support assembly 120, thereby forming a lever structure. When vibration occurs at one end, the opposite end moves synchronously in the opposite direction. The first shock absorbing assembly 130 is installed on the moving equipment and connected to one end of the support assembly 120. In this way, during the movement of the moving equipment, the radar installation device 100 will vibrate with the moving equipment, and due to the shock absorbing effect of the first shock absorbing assembly 130, the up and down vibration amplitude generated by the end of the support assembly 120 connected to the moving equipment is reduced, and accordingly, the vibration amplitude of the radar 200 located at the opposite end is reduced, which satisfies the scanning angle adjustment of the radar 200 during the movement and reduces the vibration of the radar 200, thereby maintaining the stability of the operation.

[0051] Continue reading Figure 2 As shown, in some embodiments, the first shock absorbing assembly 130 includes a first mounting plate 131 and a plurality of first buffer members 132 , the first mounting plate 131 is connected to the sports equipment, and each first buffer member 132 is mounted on the first mounting plate 131 and connected to the first end of the support assembly 120 .

[0052] Specifically, the first mounting plate 131 can be a flat plate or a seat structure, and is installed on the moving device by bolt locking or welding. The first buffer 132 is installed between the moving device and the support assembly 120 to provide a shock absorbing effect to the support assembly 120 during the movement of the moving device. When the support assembly 120 vibrates upward following the moving device, the first buffer 132 provides a downward buffering potential energy, and when the support assembly 120 vibrates downward following the moving device, the first buffer 132 provides an upward buffering potential energy, thereby offsetting part of the power of the support assembly 120, reducing the vibration amplitude of the support assembly 120, and further reducing the change amplitude of the viewing angle of the radar 200 fixed at the other end.

[0053] Exemplarily, the number of the first buffer members 132 may be two, three, four, five, etc., and may be specifically set according to actual needs. Preferably, the first mounting plate 131 may be a flat plate, and the first buffer member 132 is provided with four multi-layer polyurethane shock-absorbing balls. Each first buffer member 132 is evenly distributed at the four corners of the first mounting plate 131, and a through hole is provided in the middle of the shock-absorbing ball, so that a bolt can penetrate the support assembly 120 and the shock-absorbing ball, thereby locking the first shock-absorbing member between the support assembly 120 and the first mounting plate 131. At the same time, by providing the shock-absorbing ball, a larger buffering potential energy can be provided when a large vibration occurs, thereby improving the shock absorption effect.

[0054] In some embodiments, the radar mounting device 100 further includes a second shock absorbing assembly 140 . The second shock absorbing assembly 140 is mounted on one end of the supporting assembly 120 where the radar 200 is disposed. The radar 200 is mounted on the second shock absorbing assembly 140 .

[0055] Specifically, the second shock absorbing assembly 140 is installed at the upper end of the supporting assembly 120, and the first shock absorbing assembly 130 is installed at the lower end of the supporting assembly 120, so that when the radar 200 is installed on the second shock absorbing assembly 140, the radar 200 has a better scanning angle. At the same time, through the arrangement of the second shock absorbing assembly 140, the vibration amplitude of the radar 200 can be further reduced in cooperation with the first shock absorbing assembly 130.

[0056] Furthermore, the second shock absorbing assembly 140 includes a second mounting plate 141 and a plurality of second buffer members 142 , the radar 200 is mounted on the second mounting plate 141 , and two ends of each second buffer member 142 are respectively connected to the second mounting plate 141 and the second end of the supporting assembly 120 .

[0057] Preferably, the second mounting plate 141 is a flat plate, and four second buffer members 142 are provided and evenly distributed at the four corners of the second mounting plate 141. The second buffer member 142 is also a multi-layer polyurethane shock-absorbing ball to enhance the shock-absorbing effect of the radar 200. The radar 200 is mounted on the upper side of the second mounting plate 141, and the top end of the second buffer member 142 is connected to the lower side of the second mounting plate 141, and the bottom end is connected to the support assembly 120, so that during the vibration of the support assembly 120, the second buffer member 142 performs shock absorption on the second mounting plate 141 and the radar 200.

[0058] Furthermore, the second shock absorbing assembly 140 also includes a mounting seat 144, a third mounting plate 145 and a third buffer member 143. The mounting seat 144 and each third buffer member 143 are fixed to the side of the second mounting plate 141 facing away from the second buffer member 142. The third mounting plate 145 is arranged on the side of the third buffer member 143 facing away from the second mounting plate 141 and abuts against the mounting seat 144. The radar 200 is installed on the side of the mounting seat 144 facing away from the second mounting plate 141 and exposed to the third mounting plate 145.

[0059] Specifically, the third mounting plate 145 is a frame structure with a through hole in the middle, and the size of the through hole in the middle is smaller than the size of the mounting seat 144. In this way, when the mounting seat 144 is installed on the second mounting plate 141, the third mounting plate 145 can limit the top side of the mounting seat 144, fix the mounting seat 144, and maintain the stability of the mounting seat 144. The radar 200 is fixed to the mounting seat 144 and extends out of the middle through hole of the third mounting plate 145, thereby ensuring the scanning operation of the radar 200.

[0060] Preferably, the third buffer member 143 is also provided with four and evenly distributed at the four corners of the third mounting plate 145. The third buffer member 143 is also a multi-layer polyurethane shock-absorbing ball, so as to cooperate with the second buffer member 142 to limit the up and down movement of the radar 200, and further enhance the shock-absorbing effect of the radar 200.

[0061] In summary, the operating principle of the radar installation device 100 provided in the present application is: when the moving device vibrates upward, the first shock absorbing assembly 130 has a tendency to move upward, and at this time, the first buffer 132 of the first shock absorbing assembly 130 is stretched to reduce the shaking amplitude of this position. At this time, the first shock absorbing assembly 130 rotates around the fulcrum of the fixed assembly 110, and the second buffer 142 of the second shock absorbing assembly 140 is compressed to reduce the amplitude of the downward vibration of the radar 200, thereby achieving the effect of shock reduction of the radar 200. Conversely, when the moving device vibrates downward, the first shock absorbing assembly 130 has a tendency to move downward, and at this time, the first buffer 132 of the first shock absorbing assembly 130 is compressed to reduce the shaking amplitude of this position. The third buffer 143 of the second shock absorbing assembly 140 is compressed to reduce the amplitude of the upward vibration of the radar 200, thereby achieving the shock reduction effect. In this way, under the action of the second buffer member 142 and the third buffer member 143, the second mounting plate 141 and the radar 200 are floatingly arranged, and can reduce the vibration amplitude of the radar 200 during the up and down vibration process, thereby ensuring that the radar 200 maintains a horizontal scanning angle as much as possible during the movement, thereby ensuring the normal use of the radar 200.

[0062] Continue reading Figure 3 As shown, further, the second shock absorbing assembly 140 also includes a plurality of locking members, the second mounting plate 141 is correspondingly provided with a plurality of waist-shaped grooves 146, and each locking member passes through the third mounting plate 145, the third buffer member 143 and the waist-shaped groove 146 in sequence.

[0063] Specifically, the mounting seat 144 is a truncated cone structure, which can adjust the scanning angle of the radar 200 by rotation to meet the multi-angle operation of the radar 200. The second buffer 142 is installed on the bottom side of the second mounting plate 141 through a screw and a bushing guide column. The locking member can be a fastening bolt, and the third mounting plate 145 and the third buffer 143 can synchronously adjust the locking position according to the rotation of the mounting seat 144 when the locking member is loosened. The locking member moves in the waist groove 146 and is locked after reaching the set angle, so as to meet the horizontal angle adjustment of the radar 200.

[0064] Continue reading Figure 4As shown, in some embodiments, the support assembly 120 includes a support frame 121 and a rotating shaft 122, the support frame 121 includes a first planar section 1212 located at the first end, an inclined section 1211 and a second planar section 1213 located at the second end, the first planar section 1212 and the second planar section 1213 are respectively connected to the two ends of the inclined section 1211, and the rotating shaft 122 is fixed to one side of the inclined section 1211 and is rotatably connected to the fixing assembly 110.

[0065] Specifically, the support frame 121 has a Z-shaped structure, and both ends thereof are horizontal plane structures to facilitate the installation of the first shock absorbing assembly 130 and the second shock absorbing assembly 140. At the same time, the rotating shaft 122 is arranged on the bottom side of the support frame 121, so as to be rotatably connected to the fixed assembly 110 through axonometric measurement, so that the inclined support frame 121 forms a lever structure with the axis of the rotating shaft 122 as the fulcrum, and the vibration amplitude of the second plane section 1213 connected to the second shock absorbing assembly 140 is adjusted through the first plane section 1212 connected to the first shock absorbing assembly 130, thereby reducing the vibration of the radar 200 installed on the second plane section 1213.

[0066] Furthermore, the first plane section 1212 is connected to the first shock absorbing assembly 130, and the second plane section 1213 is installed with the radar 200. The length from the end of the inclined plane section 1211 close to the first plane section 1212 to the rotating shaft 122 is greater than the length from the end of the inclined plane section 1211 close to the second plane section 1213 to the rotating shaft 122. In this way, according to the principle of lever, the magnitude of the vibration force received by the radar 200 is greater than the vibration force of the first plane section 1212, so that the second buffer 142 and the third buffer 143 can realize a large-scale vibration reduction of the radar 200, and the radar 200 can maintain the corresponding visual angle tracking during the vibration process.

[0067] Furthermore, the rotating shaft 122 is an eccentric shaft. Thus, the connection height of the support base relative to the fixing assembly 110 can be adjusted by rotating the eccentric shaft, thereby adjusting the scanning area of ​​the radar 200 within a certain range of upper and lower angles.

[0068] Continue reading Figure 5 As shown, in some embodiments, the fixing assembly 110 includes two fixing seats 111 arranged opposite to each other, and the two fixing seats 111 are arranged opposite to each other on both sides of the support frame 121, and both ends of the rotating shaft 122 are rotatably connected to the two fixing seats 111 at the same time to improve the installation stability of the support frame 121. The fixing seat 111 can be designed as a bearing seat structure, and is connected to the motion device by bolts, and the fastening bolts are tightened along the radial direction of the rotating shaft 122 to improve the connection strength between the fixing seat 111 and the rotating shaft 122.

[0069] An embodiment of the present application further provides an automatic guided vehicle, comprising the radar installation device 100 in any of the above embodiments.

[0070] For example, the automatic guided vehicle adopts a differential dual-drive four-wheel driven drive mode. Two driving wheels are installed in the middle of the vehicle body, equipped with a drive motor, and there are two universal wheels at the front and rear of the vehicle, which can rotate 360° on the spot. A touch screen is installed at the rear of the vehicle to facilitate debugging during the development process and later installation and maintenance. The entire vehicle body can be equipped with navigation code readers, inertial sensors, and laser sensors according to the selected visual + inertial navigation mode and safety devices to realize the multi-functional application of the automatic guided vehicle.

[0071] In addition, the automatic guided vehicle also includes a travel damping part and a rigid body part. It can be understood that the travel damping part is a part of the automatic guided vehicle that can be deformed during driving, such as shock absorbers at the wheels, cushioning pads of the vehicle body and other shock absorbing components. The rigid body part is a part of the automatic guided vehicle that does not deform during driving, such as a frame, an outer shell and other components.

[0072] This embodiment has the radar installation device 100 in any of the above embodiments, and therefore has all the beneficial effects of the radar installation device 100 in any of the above embodiments, which will not be described in detail here.

[0073] In some embodiments, the first shock absorbing assembly 130 is installed on the walking shock absorbing part, and the fixing assembly 110 is installed on the rigid body part.

[0074] Specifically, the first shock absorbing assembly 130 is fixedly mounted on the traveling shock absorbing part of the automatic guided vehicle, where the vibration intensity is relatively small and can be regarded as stationary relative to the vehicle body. The fixed assembly 110 is mounted on the rigid body of the automatic guided vehicle, where the vibration is relatively large. At this time, the second shock absorbing assembly 140 with the radar 200 installed works to achieve the shock absorbing effect of the radar 200 during the moving process.

[0075] In other embodiments, the first shock absorbing assembly 130 and the fixing assembly 110 are simultaneously installed on either the walking shock absorbing part or the rigid body part.

[0076] Specifically, the radar installation device 100 can be designed according to a certain ratio so that the radar installation device 100 can be installed as a whole on the same part of the automatic guided vehicle. That is, the first shock absorbing component 130 and the fixing component 110 are both installed on the walking shock absorbing part or the rigid body part. During the movement of the automatic guided vehicle, when passing through an obstacle section, according to the principle of inertia, the radar installation device 100 as a whole follows the vibration, so that the first shock absorbing component 130 and the second shock absorbing component 140 work synchronously to reduce the vibration amplitude of the radar 200.

[0077] The technical features of the above-described embodiments may be arbitrarily combined. To make the description concise, not all possible combinations of the technical features in the above-described embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0078] The above-described embodiments only express several implementation methods of the present application, and the descriptions thereof are relatively specific and detailed, but they cannot be construed as limiting the scope of the patent application. It should be pointed out that, for a person of ordinary skill in the art, several variations and improvements can be made without departing from the concept of the present application, and these all belong to the protection scope of the present application. Therefore, the protection scope of the patent application shall be subject to the attached claims.

Claims

1. A radar mounting device, used for mounting a radar on a sports device, characterized in that: The radar installation device comprises: A fixing assembly mounted on the sports equipment; a supporting component, rotatably disposed on the fixing component with its connection with the fixing component as a fulcrum, and the supporting component has a first end and a second end located at opposite ends of the fulcrum; the radar is mounted on the second end; and A first shock absorbing assembly is mounted on the sports equipment and connected to the first end of the supporting assembly.

2. The radar installation device according to claim 1, characterized in that: The radar mounting device further comprises a second shock absorbing assembly, wherein the second shock absorbing assembly is mounted on the second end of the supporting assembly, and the radar is mounted on the second shock absorbing assembly.

3. The radar installation device according to claim 2, characterized in that: The second shock absorbing assembly includes a second mounting plate and a plurality of second buffer members, the radar is mounted on the second mounting plate, and two ends of each of the second buffer members are respectively connected to the second mounting plate and the second end of the supporting assembly.

4. The radar installation device according to claim 3, characterized in that: The second shock absorbing assembly also includes a mounting seat, a third mounting plate and a third buffer member, the mounting seat and each of the third buffer members are fixed to a side of the second mounting plate facing away from the second buffer member, the third mounting plate is arranged on a side of the third buffer member facing away from the second mounting plate and abuts against the mounting seat, and the radar is installed on a side of the mounting seat facing away from the second mounting plate and exposed to the third mounting plate.

5. The radar installation device according to claim 4, characterized in that: The second shock absorbing assembly further comprises a plurality of locking members, the second mounting plate is correspondingly provided with a plurality of waist-shaped grooves, and each of the locking members passes through the third mounting plate, the third buffer member and the waist-shaped groove in sequence.

6. The radar installation device according to claim 1, characterized in that: The support assembly includes a support frame and a rotating shaft, the support frame includes a first plane section and an inclined surface section located at the first end, and a second plane section located at the second end, the first plane section and the second plane section are respectively connected to two ends of the inclined surface section, and the rotating shaft is fixed to one side of the inclined surface section and is rotatably connected to the fixing assembly; The first plane section is connected to the first shock absorbing assembly, and the second plane section is installed with the radar; the length from one end of the inclined section close to the first plane section to the rotating axis is greater than the length from one end of the inclined section close to the second plane section to the rotating axis.

7. The radar installation device according to claim 6, characterized in that: The rotating shaft is an eccentric shaft.

8. An automatic guided vehicle, characterized in that: A radar mounting device comprising any one of claims 1 to 7.

9. The automated guided vehicle according to claim 8, characterized in that: The automatic guided vehicle further comprises a travel shock absorbing part and a rigid body part, the first shock absorbing assembly is mounted on the travel shock absorbing part, and the fixing assembly is mounted on the rigid body part.

10. The automated guided vehicle according to claim 8, characterized in that: The automatic guided vehicle further comprises a travel shock absorbing part and a rigid body part, and the first shock absorbing assembly and the fixing assembly are simultaneously installed on either the travel shock absorbing part or the rigid body part.

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