Warping clamp, propeller and water area movable equipment

CN119343296AActive Publication Date: 2025-01-21DONGGUAN EPROPULSION INTELLIGENCE TECH LTD
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Patent Information

Application Number
CN202380035132.5
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2023-05-30
Publication Date
2025-01-21
Estimated Expiration
2043-05-30

AI Technical Summary

Technical Problem

When the movable equipment in the water is running, the vibration of the thruster is easily transmitted to the thruster structure, resulting in damage to the thruster structure and shortening the service life.

Method used

A shaking fixture is designed, including a fixed bracket, a shaking bracket, a connecting assembly and a vibration-absorbing structure. The vibration-absorbing structure is located between the shaking bracket and the connecting assembly to absorb vibration of the main machine and reduce vibration transmission.

Benefits of technology

It effectively reduces the vibration of the lifting bracket and the fixed bracket, extends the service life of the lifting clamp, and improves the operating stability and driving experience of movable equipment in the water.

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Abstract

A tilting clamp (10) of a propeller (200) comprises a fixing support (11), a tilting support (12), a connecting assembly (13) and a vibration reduction structure (14), one side of the fixing support (11) is used for being connected with a water area carrier (301), the tilting support (12) is rotatably connected to the other side of the fixing support (11), the connecting assembly (13) is used for being connected with a main machine (201) of the propeller (200), and the vibration reduction structure (14) is arranged between the tilting support (12) and the connecting assembly (13). The vibration absorber is used for absorbing vibration of the main machine (201). The use safety of the tilting clamp is improved, and the service life of the tilting clamp is prolonged.
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Description

Lifting fixtures, thrusters and movable equipment in water areas Technical Field

[0001] The present application relates to the technical field of movable equipment in water areas, and in particular to a lifting clamp, a propeller and a movable equipment in water areas. Background Art

[0002] Some known outboard motors feature a tilting mechanism that uses this mechanism to generate tilting power, allowing the propeller to lift out of the water and protect it from corrosion caused by prolonged immersion. However, when operating mobile equipment in water, the propeller's propulsion power generates vibrations that can be easily transmitted to the tilting mechanism, causing damage and failure, thereby shortening the outboard motor's service life.

[0003] Summary of the Invention

[0004] The present application provides a lifting fixture, a propeller and a movable device in water areas, which can prevent vibration from being transmitted to the lifting structure and extend the service life of the outboard motor.

[0005] The embodiment of the present application is implemented as follows:

[0006] In a first aspect, the present application provides a lifting fixture for connecting a propeller to a water body. The lifting fixture comprises a fixed bracket, a lifting bracket, a connecting assembly, and a vibration damping structure. One side of the fixed bracket is used to connect to the water body. The lifting bracket is rotatably connected to the other side of the fixed bracket. The connecting assembly is used to connect to the main unit of the propeller. The vibration damping structure is disposed between the lifting bracket and the connecting assembly and is used to absorb vibrations of the main unit.

[0007] The lifting clamp of the present application has a vibration-damping structure connected between the lifting bracket and the connecting component. The vibration-damping structure can significantly reduce the vibration transmitted from the connecting component to the lifting bracket, thereby significantly reducing the vibration of the lifting bracket and the fixed bracket, ensuring the rotation safety of the lifting bracket relative to the fixed bracket, and extending the service life.

[0008] In a second aspect, the present application provides a propeller, comprising a main unit and the aforementioned lifting fixture, wherein the main unit is connected to a connecting component of the lifting fixture.

[0009] In a third aspect, the present application provides a movable device in water areas, comprising a water area carrier and the aforementioned propeller, wherein a fixed bracket of the propeller is connected to the water area carrier. BRIEF DESCRIPTION OF THE DRAWINGS

[0010] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings in the embodiments will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without paying any creative work.

[0011] FIG1 is a schematic structural diagram of a mobile device for use in water areas according to an embodiment of the present application;

[0012] FIG2 is a schematic structural diagram of a propeller according to an embodiment of the present application;

[0013] FIG3 is a schematic diagram of the local structure in FIG2 ;

[0014] FIG4 is a schematic structural diagram of a lifting fixture according to an embodiment of the present application;

[0015] FIG5 is a cross-sectional view of a warping fixture according to an embodiment of the present application;

[0016] FIG6 is a schematic diagram of the exploded structure of a lifting fixture according to an embodiment of the present application;

[0017] FIG7 is a partial cross-sectional view of a first pull rod of a lifting fixture according to an embodiment of the present application;

[0018] FIG8 is a partial cross-sectional view of a second pull rod of a lifting fixture according to an embodiment of the present application;

[0019] FIG9 is a schematic structural diagram of a propeller according to another embodiment of the present application;

[0020] FIG10 is a schematic structural diagram of a warping fixture according to another embodiment of the present application;

[0021] FIG11 is a schematic diagram of an exploded structure of a lifting fixture according to another embodiment of the present application;

[0022] FIG12 is a partial cross-sectional view of a warping fixture according to another embodiment of the present application;

[0023] FIG13 is a schematic structural diagram of a propeller according to another embodiment of the present application.

[0024] : Description of the main component symbols: Lifting fixture 10 Fixed bracket 11 Lifting bracket 12 Connecting assembly 13 Vibration damping structure 14 Connecting rod 15 First end 16 Second end 17 Rotation axis 18 First vibration damper 19 Second vibration damper 20 First pull rod 21 Second pull rod 22 First matching hole 23 Second matching hole 24 First sealing cover 25 Second sealing cover 26 First sealing block 27 First external thread 28 First internal thread 29 Second sealing block 30 Second external thread 31 Second internal thread 32 First groove 33 First connecting block 34 Locking rod 35 Limiting block 36 Second groove 37 Second connecting block 38 Locking member 39 Third connecting block 40 Third pull rod 41 Third matching hole 42 Third groove 43 Adapter block 44 Mounting column 45 Mounting groove 46 Fixing screw 47 Fixing gasket 48 Buffer pad 49 Rotation hole 50 Steering shaft 51 First steering gear 52 Steering protrusion 53 Steering bearing 54 Seal 55 Support bushing 56 rotating section57 Connecting section 58 Mounting rod 59 Fourth connecting block 60 Straight hole 61 Fourth pull rod 62 Fourth matching hole 63 Tilt-up driving member 64 Rotating shaft 65 Avoidance groove 66 Pull rod connecting block 67 Connecting portion 68 Propulsion direction 69 Mounting hole 70 Propeller 200 Main engine 201 Above-water part 202 Underwater part 203 Steering actuator 204 Second steering gear 205 Steering shaft hole 206 Drive bearing 207 Power part 208 Propulsion motor 209 Propeller 210 Frame 211 Movable equipment in water area 300 Water area carrier 301 DETAILED DESCRIPTION

[0025] The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments.

[0026] It should be noted that when an element is referred to as being "fixed to" another element, it may be directly on the other element or there may also be an element centered therein. When an element is considered to be "connected to" another element, it may be directly connected to the other element or there may also be an element centered therein. When an element is considered to be "set on" another element, it may be directly set on the other element or there may also be an element centered therein. The terms "vertical", "horizontal", "left", "right" and similar expressions used herein are for illustrative purposes only.

[0027] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by those skilled in the art to which this application belongs. The terms used herein in the specification of this application are only for the purpose of describing specific embodiments and are not intended to limit this application. The term "or / and" as used herein includes any and all combinations of one or more of the relevant listed items.

[0028] Some embodiments of the present application are described in detail. In the absence of conflict, the following embodiments and features of the embodiments can be combined with each other.

[0029] Example 1

[0030] Referring to Figure 1 , this embodiment provides a mobile water vehicle 300, comprising a water vehicle 301 and a propeller 200. The propeller 200 is connected to the water vehicle 301 and is used to propel the mobile water vehicle 300. In this embodiment, the propeller 200 is mounted at the rear of the water vehicle 301. In other embodiments, the connection position of the propeller and the water vehicle 301 may be adjusted accordingly, depending on the specific requirements of the propeller's installation location on the water vehicle 301.

[0031] The mobile device 300 in this embodiment can be any water vehicle, such as a passenger ship, yacht, fishing boat, or sailboat. This embodiment uses the water vehicle 301 as a ship hull and the propeller 200 as an outboard motor as an example. Of course, the mobile device 300 can also be an amphibious vehicle, an unmanned patrol boat, a water drone, or the like, without limitation.

[0032] Referring to Figure 2, the propeller 200 of this embodiment includes a main unit 201 and a lifting fixture 10. The lifting fixture 10 includes a fixed bracket 11, a lifting bracket 12, a connecting assembly 13 and a vibration reduction structure 14. The fixed bracket 11 is connected to the water carrier 301. The lifting bracket 12 is rotatably connected to the fixed bracket 11. The lifting bracket 12 and the fixed bracket 11 are rotatably connected through a rotating shaft 65 (see Figures 5 and 11), and the rotating axis 18 of the two is the axial direction of the rotating shaft 65. The rotating shaft 65 can be fixed to one of the lifting bracket 12 and the fixed bracket 11, and the other of the lifting bracket 12 and the fixed bracket 11 is rotatably matched with the rotating shaft 65. The rotating axis 18 of the lifting bracket 12 rotating relative to the fixed bracket 11 is parallel to the midline plane of the water carrier 301. The connecting assembly 13 is connected to the lifting bracket 12 and is used to connect the main unit 201. The vibration-damping structure 14 is disposed between the tilting bracket 12 and the connecting assembly 13 , and is used to absorb vibration of the host 201 .

[0033] In this embodiment, referring to Figure 1 , the main machine 201 includes a frame 211, a steering actuator 204, and a power unit 208. The frame 211 is connected to the connecting assembly 13. The steering actuator 204 is mounted on the frame 211 and cooperates with the connecting assembly 13 to drive the frame 211 to rotate relative to the lifting fixture 10. The power unit 208 is mounted on the frame 211 and is used to output propulsion power.

[0034] In this embodiment, referring to Figures 2 and 3 , the connecting assembly 13 includes a steering shaft 51 rotatably connected to the frame 211. The steering shaft 51 is connected to the water body 301 via the tilting bracket 12 and the fixed bracket 11, enabling the steering shaft 51 to tilt relative to the water body 301. The steering shaft 51 is provided with a first steering gear 52. The steering actuator 204 includes a steering motor fixed to the frame 211. A second steering gear 205 is provided at the output end of the steering motor. The second steering gear 205 engages with the first steering gear 52. The steering torque output by the steering motor forces the steering motor and the frame 211 to rotate relative to the tilting fixture 10 about the steering shaft 51, thereby changing the orientation of the power unit 208 connected to the frame 211, thereby changing the direction of the propulsion power output by the power unit 208 and thereby driving the water body 301 to steer. In other embodiments, the first steering gear 52 and the second steering gear 205 may also be coupled via a reduction gear mechanism. In this embodiment, the output shaft of the steering actuator 204 is rotatably engaged with the driving bearing 207 on the frame 211 to improve the reliability of the steering actuator 204 in outputting the steering torque.

[0035] It is understood that in other embodiments, the steering force driven by the steering actuator 204 to the frame 211 can be replaced by a tiller that receives the driver's manual turning force, thereby driving the frame 211 to steer. In other embodiments, the steering actuator 204 configured as a steering motor can be replaced with a steering actuator 204 configured as an electro-hydraulic cylinder. In other embodiments, the steering actuator 204 can be mounted on the tilting bracket 12, and the steering shaft 51 can be fixed to the frame 211. The steering actuator 204 drives the steering shaft 51 to rotate relative to the tilting bracket 12, thereby driving the frame 211 to rotate.

[0036] In this embodiment, referring to FIG1 , the power section 208 includes a propulsion motor 209 and a propeller 210. The propulsion motor 209 is connected to the propeller 210 in a transmission manner and is used to drive the propeller 210 to rotate to generate propulsion. Specifically, the propulsion motor 209 is fixed to the frame 211, and the propeller 210 is structurally connected to the underwater portion 203 of the frame 211 by a rotating shaft. The propulsion motor 209 can output the rotational torque to the propeller 210 directly via the rotating shaft, or it can output the rotational torque to the propeller 210 via a transmission mechanism or a reduction assembly. In this embodiment, referring to FIG1 and FIG2 , the tilting fixture 10 also includes a tilting drive 64. The tilting drive 64 is connected between the fixed bracket 11 and the tilting bracket 12 and is used to drive the tilting bracket 12 to rotate relative to the fixed bracket 11. The tilting bracket 12 includes a rotating section 57 and a connecting section 58. The rotating section 57 is rotatably connected to the fixed bracket 11, and the connecting section 58 is bent and connected to the rotating section 57 to form a "7"-shaped tilting bracket 12. The length direction of the connecting section 58 is perpendicular to the rotation axis 18 of the rotating section 57 , and the connecting assembly 13 is connected to the connecting section 58 via the vibration-damping structure 14 .

[0037] One end of the tilting drive member 64 is rotatably connected to the fixed bracket 11, and the other end is rotatably connected to the tilting bracket 12. The rotation axis of the tilting drive member 64 is parallel and spaced from the rotation axis of the tilting bracket 12 relative to the fixed bracket 11. The tilting drive member 64 is retractable to drive the frame 211 to tilt relative to the water body 301. The fixed bracket 11 can be fixedly connected to the water body 301 by welding, bolting, or locking clamps. The tilting drive member 64 can be a hydraulic cylinder, an electro-hydraulic cylinder, or other device capable of outputting power. For example, when the lifting drive component 64 is an electro-hydraulic push rod, one end thereof is connected to the fixed bracket 11 and is provided with a motor, a hydraulic cylinder and an oil storage chamber, and the other end is a telescopic end. The motor at the telescopic end controls the oil in the oil storage chamber to enter the hydraulic cylinder to adjust the hydraulic size of the hydraulic cylinder, thereby utilizing the hydraulic pressure to drive the telescopic end to extend and retract relative to the fixed bracket 11, and then the telescopic end is connected to the lifting bracket 12. The telescopic end can push the lifting bracket 12 to rotate relative to the fixed bracket 11, that is, to push the frame 211 to lift and rotate relative to the water carrier 301, thereby driving the connecting component 13, the steering shaft 51, the steering actuator 204 and the power part 208 to rotate and lift together.

[0038] It is understandable that the power part 208 outputs propulsion power, and the power part 208 is prone to vibration due to the interaction with the water area, that is, the power part 208 forms the vibration source of the propeller 200. Since the frame 211 is rigidly connected to the power part 208, the vibration of the power part 208 will be transmitted to the frame 211, and the frame 211 is rigidly matched in the axial direction of the steering shaft 51, which causes the steering shaft 51 to easily vibrate in the axial direction, and then the steering shaft 51 is at risk of transmitting the vibration to the lifting bracket 12. In order to avoid the vibration of the power part 208 from being transmitted to the lifting clamp 10, and also to prevent it from being transmitted to the water area carrier 301 through the lifting clamp 10, to avoid damage to the lifting clamp 10, and to avoid the vibration on the water area carrier 301 affecting the driving experience, a vibration reduction structure 14 is set between the connecting component 13 and the lifting bracket 12. The vibration reduction structure 14 is used to absorb vibration, thereby eliminating the vibration on the lifting clamp 10 and the water area carrier 301, ensuring the safety of the lifting clamp 10, and improving the driving experience. In the lifting fixture 10 of this embodiment, a vibration-damping structure 14 is connected between the lifting bracket 12 and the connecting assembly 13. This structure significantly reduces vibration transmitted from the connecting assembly 13 to the lifting bracket 12, thereby significantly reducing the amount of vibration between the lifting bracket 12 and the fixed bracket 11. This structure protects the connection between the lifting bracket 12 and the fixed bracket 11, and the connection between the fixed bracket 11 and the water body 301, ensuring the safe rotation of the lifting bracket 12 relative to the fixed bracket 11. It also eliminates vibration of the lifting drive element 64, ensuring safety, thereby ensuring the safety of the entire lifting fixture 10 and extending the service life of the propeller 200. Furthermore, since the amount of vibration received and transmitted by the fixed bracket 11 to the water body 301 is significantly reduced, the vibration of the water body 301 during operation of the water movable device 300 is also reduced, improving the riding experience for the driver and passengers. Furthermore, due to the improved vibration resistance of the lifting fixture 10, a more powerful power unit 208 can be selected, expanding the selection range of the main unit 201.

[0039] In this embodiment, referring to Figures 2 to 4, the connecting assembly 13 is provided with a connecting rod 15, which has a first end 16 and a second end 17 distributed along its length direction, and the length direction is perpendicular to the rotation axis 18 of the tilting bracket 12, and the first end 16 and the second end 17 are respectively used to connect the main unit 201 to the above-water part 202 away from the underwater and the underwater part 203 close to the underwater.

[0040] Specifically, referring to FIG3 , the first end portion 16 is fixedly connected to the steering shaft 51. The frame 211 is provided with a steering bearing 54. The steering shaft 51 is assembled within the steering bearing 54. A seal 55 is provided on the side of the steering bearing 54 near the second end portion 17. The seal 55 is sleeved on the steering shaft 51 and abuts against the end face of the steering bearing 54. The seal 55 prevents water from entering through the mating point between the frame 211 and the steering shaft 51, thereby ensuring the safety of the electronic components within the frame 211. Specifically, the first end portion 16 is provided with an axially disposed socket into which the steering shaft 51 is inserted. The portion of the steering shaft 51 inserted into the socket is provided with a rotation-stopping structure that cooperates with the inner wall of the socket to limit the rotation of the steering shaft 51 relative to the first end portion 16. Of course, in other embodiments, a socket may also be provided at the end of the steering shaft 51.

[0041] In this embodiment, referring to Figure 3 , a steering protrusion 53 is provided on the side of the steering shaft 51 and is received in a steering bearing 54. The steering protrusion 53 is disposed opposite the first steering tooth portion 52. The steering bearing 54 is a thrust bearing, thereby transmitting the load of the main unit 201 to the steering shaft 51, thereby providing axial support for the main unit 201.

[0042] The main unit 201 also has a steering shaft hole 206 near the underwater portion 203. The second end portion 17 fits within the steering shaft hole 206. The tilting fixture 10 also includes a support bushing 56 that is sleeved over the second end portion 17 and fits within the steering shaft hole 206. The support bushing 56 is used to support the connecting rod 15. The second end portion 17 can be rotatably fitted within the support bushing 56 via its outer circumferential surface. The support bushing 56 provides radial support for the connecting rod 15 during the tilting process of the tilting bracket 12, thereby providing stable support.

[0043] In this embodiment, referring to FIG5 , the vibration damping structure 14 includes a first vibration damper 19 and a second vibration damper 20. The first end portion 16 is connected to the portion of the connecting section 58 of the tilting bracket 12 near the rotation section 57 via the first vibration damper 19, and the second end portion 17 is connected to the portion of the connecting section 58 of the tilting bracket 12 away from the rotation section 57 via the second vibration damper 20. The first vibration damper 19 is connected to one end of the connecting rod 15 and the end of the connecting section 58 near the rotation section 57, while the second vibration damper 20 is connected to the other end of the connecting rod 15 and the end of the connecting section 58 away from the rotation section 57. This allows the first vibration damper 19 to absorb vibration at the connection between the one end of the connecting rod 15 and the end of the connecting section 58 near the rotation section 57, while the second vibration damper 20 to absorb vibration at the connection between the other end of the connecting rod 15 and the end of the connecting section 58 away from the rotation section 57, thereby improving the vibration damping effect. At the same time, during the process of the lifting bracket 12 lifting relative to the fixed bracket 11, the connecting rod 15 is provided with two spaced connection points in the direction perpendicular to the rotation axis 18 of the lifting bracket 12, and the two connection points are connected to the lifting bracket 12, one of the connection points is formed by the first end 16, the first vibration damper 19 and one end of the connecting section 58, and the other connection point is formed by the second end 17, the second vibration damper 20 and the other end of the connecting section 58. When the lifting bracket 12 is lifted relative to the fixed bracket 11, the lifting bracket 12 drives the connecting component 13 and the host 201 connected to the connecting component 13 to lift. The connecting component 13 mainly bears the weight of the host 201 through the connection between the first vibration damper 19 and the lifting bracket 12. The connection between the connecting component 13 and the lifting bracket 12 through the second vibration damper 20 forms a fulcrum to balance the torque at both ends of the connecting component 13. In this way, the first vibration damper 19 bears the force and the second vibration damper 20 forms a fulcrum to balance the gravity of the host 201 and drive the host 201 to lift, thereby better overcoming the weight of the host 201, making the lifting action of the host 201 more stable, and reducing the amount of vibration along the gravity direction generated during the lifting process of the host 201.

[0044] In this embodiment, referring to Figures 5 and 6, the first vibration damper 19 is a columnar vibration damper, the geometric center axis of the first vibration damper 19 is parallel to the rotation axis 18 of the tilting bracket 12, and the first vibration damper 19 is used to absorb the vibration of the propeller 200 in its radial direction, and the second vibration damper 20 is a columnar vibration damper, the geometric center axis of the second vibration damper 20 is parallel to the rotation axis 18 of the tilting bracket 12, and the second vibration damper 20 is used to absorb the vibration of the propeller 200 in its radial direction.

[0045] In this embodiment, the cross-section of the columnar vibration damper can be circular, rectangular, polygonal, or other special shapes. The columnar vibration damper can be made of rubber, meaning that both the first vibration damper 19 and the second vibration damper 20 are rubber-mounted. In other embodiments, both the first vibration damper 19 and the second vibration damper 20 can be hydraulically mounted.

[0046] In this embodiment, both the first vibration damper 19 and the second vibration damper 20 can absorb radial vibrations of the propeller 200. They can also absorb vibrations generated by the power unit 208. The vibrations generated by the gravity of the main engine 201 during the tilting process, as well as the currents or waves of the water body, also exert forces in the direction of gravity on the main engine 201. Furthermore, they can absorb a certain amount of vibration generated when the steering actuator 204 outputs a steering torque. In other embodiments, the geometric center axes of the first vibration damper 19 and the second vibration damper 20 can also be perpendicular to the rotation axis 18 of the tilting bracket 12 (i.e., the axis of the steering shaft 51), thereby improving the ability of the first vibration damper 19 and the second vibration damper 20 to absorb vibrations generated when the steering actuator 204 outputs a steering torque.

[0047] In this embodiment, referring to FIG6 , the connecting assembly 13 is provided with a first tie rod 21 and a second tie rod 22. The first tie rod 21 is provided at the first end 16, and the second tie rod 22 is provided at the second end 17. The tilting bracket 12 defines a first mating hole 23 and a second mating hole 24 spaced apart. The first vibration damper 19 defines an axial hole along its axis. The first tie rod 21 passes through the axial hole and tightly fits with the inner wall of the axial hole. The first vibration damper 19 is assembled into the first mating hole 23 and tightly fits with the inner wall of the first mating hole 23. The second vibration damper 20 defines an axial hole along its axis. The second tie rod 22 passes through the axial hole and tightly fits with the inner wall of the axial hole. The second vibration damper 20 is assembled into the second mating hole 24 and tightly fits with the inner wall of the second mating hole 24. The first and second pull rods 21 and 22 are respectively fixedly connected to the first and second vibration dampers 19 and 20, so that the inner side of the first vibration damper 19 abuts against the connecting assembly 13, the outer side of the first vibration damper 19 abuts against the tilting bracket 12, the inner side of the second vibration damper 20 abuts against the connecting assembly 13, and the outer side of the second vibration damper 20 abuts against the tilting bracket 12, thereby enabling the first and second vibration dampers 19 and 20 to absorb vibration. In other embodiments, the first and second pull rods 21 and 22 may also be provided on the tilting bracket 12, the connecting assembly 13 defines corresponding first and second mating holes 23 and 24, the first vibration damper 19 fits between the outer wall of the first pull rod 21 and the inner wall of the first mating hole 23, and the second vibration damper 20 fits between the outer wall of the second pull rod 22 and the inner wall of the second mating hole 24, thereby similarly achieving the vibration absorption function of the first and second vibration dampers 19 and 20.

[0048] In this embodiment, referring to FIG6 , the tilting bracket 12 is provided with a first groove 33. First mating holes 23 are provided on opposite side walls of the first groove 33. One end of the first pull rod 21 engages with one of the first mating holes 23, and the other end engages with the other first mating hole 23. In this embodiment, the first groove 33 is formed by a recessed portion on the side of the tilting bracket 12 facing the main body 201 and is located at the junction of the rotating section 57 and the connecting section 58. If the tilting bracket 12 does not have the first groove 33, the tilting bracket 12 and the connecting rod 15 do not overlap, which increases the overall stacking volume of the tilting bracket 12 and the connecting rod 15. In this embodiment, the provision of the first groove 33 allows the first vibration damper 19 to be accommodated within the first groove 33, allowing the connecting rod 15 to partially overlap the tilting bracket 12. This reduces the stacking volume of the connecting rod 15 and the tilting bracket 12, utilizing the internal space of the tilting bracket 12. This effectively reduces the size of the tilting fixture 10 in the propulsion direction 69 and expands the applicability of the tilting fixture 10. In addition, since the top surface of the rotating section 57 away from the fixed bracket 11 is concave to form a part of the first groove 33, the diameter of the first groove 33 in the rotating section 57 is larger than the diameter in the connecting section 58, which increases the assembly working space of the first vibration damper 19 and the first pull rod in the first groove 33, thereby facilitating the installation of the first vibration damper 19 and the first pull rod 21 in the first matching hole 23, improving the disassembly and assembly efficiency of the lifting clamp 10, and facilitating the maintenance and replacement of the first vibration damper 19.

[0049] In this embodiment, referring to FIG6 , the connecting assembly 13 further includes a first connecting block 34 connected to a sidewall of the first end portion 16 . The first pull rod 21 is provided with two locking rods 35 , which are located on either side of the first connecting block 34 along the rotation axis 18 of the tilting bracket 12 and respectively engage with the two first mating holes 23 . The outer surface of the first vibration damper 19 tightly engages with the first mating holes 23 , and the outer surface of the locking rods 35 tightly engages with the axial hole of the first vibration damper 19 . The first connecting block 34 has a connecting hole located away from the first end portion 16 . The locking rods 35 extend from the first mating hole 23 through the first vibration damper 19 within the first mating hole 23 and into the connecting hole, where they are threadedly connected to the first connecting block 34 to lock the first vibration damper 19 between the locking rods 35 and the first mating holes 23 . The locking rods 35 simultaneously lock the first vibration damper 19 and connect the first connecting block 34 to the tilting bracket 12 . In other embodiments, the locking rod 35 may be used only to install the first vibration damper 19, and other locking structures may be used to lock the first vibration damper 19. In other embodiments, the first pull rod 21 may also be configured as a separate rod, with both ends of the rod respectively engaged in the first engagement hole 23.

[0050] In this embodiment, referring to Figures 6 and 7 , first sealing covers 25 are provided at the openings of the first mating holes 23 on opposite sides of the tilting bracket 12. The first tie rod 21 and the first vibration damper 19 are located between the two first sealing covers 25. The first sealing covers 25 seal the openings on both sides of the tilting bracket 12, significantly reducing the possibility of water entering the first mating holes 23. This protects the first tie rod 21 and the first vibration damper 19, reducing the possibility of damage or shortening the life of the first vibration damper 19 due to water, thereby extending the service life of the first vibration damper 19 and ensuring its vibration absorption function.

[0051] In this embodiment, referring to FIG7 , the first sealing cover 25 is provided with a first sealing block 27 that extends into the first mating hole 23. A first external thread 28 is provided on the side of the first sealing block 27. A first internal thread 29 is provided in the first mating hole 23. The first external thread 28 and the first internal thread 29 are threadedly engaged to securely connect the first sealing cover 25 to the tilting bracket 12. In other embodiments, the first sealing cover 25 may alternatively be interference fit within the first mating hole 23 or secured to the tilting bracket 12 via set screws to seal the openings on both sides of the tilting bracket 12.

[0052] In this embodiment, referring to FIG6 , the connection assembly 13 is provided with a stopper 36, which protrudes from the first connection block 34. The stopper 36 fits within the first groove 33 and is supported on the bottom surface of the first groove 33 to support the first connection block 34 and the first pull rod 21. After the connection assembly 13 is connected to the host 201, it is pressed against the tilting bracket 12 under the action of the gravity of the host 201. The stopper 36 can reliably support the connection assembly 13 and the host 201, and can also buffer the collision between the first connection block 34 and the tilting bracket 12 during the tilting process of the tilting bracket 12.

[0053] In this embodiment, referring to Figures 6 and 8, the lifting bracket 12 is provided with a second groove 37, and second mating holes 24 are provided on opposite side walls of the second groove 37. The second pull rod 22 passes through one second mating hole 24, the second groove 37, and another second mating hole 24 in sequence along its rotation axis 18 to fit with the two second mating holes 24 and the second groove 37. The second groove 37 is formed by the connecting section 58 being concave toward the side of the main body 201. The connecting assembly 13 also includes a second connecting block 38, which is connected to the connecting rod 15 and fits into the second groove 37 to connect with the second pull rod 22. The second connecting block 38 is provided with a through hole at one end away from the connecting rod 15. The second pull rod 22 passes through the through hole and fits tightly with the inner wall of the through hole. In other embodiments, the second pull rod 22 can also be threadedly connected to the second connecting block 38. If the tilting bracket 12 does not have a second groove 37, a raised portion for mounting the second pull rod 22 is required on the surface of the tilting bracket 12. This will increase the size of the tilting fixture 10 equipped with the second vibration damper 20 along the propulsion direction 69. The provision of the second groove 37 allows the second vibration damper 20 to be accommodated within the second groove 37, utilizing the internal space of the tilting bracket 12 to reduce the size of the tilting fixture 10 along the propulsion direction 69 and increase the applicability of the tilting fixture 10. Furthermore, during assembly, the second connecting block 38 can be first placed into the second groove 37, and then the second pull rod 22 can be inserted into the second mating hole 24 and passed through the through hole of the second connecting block 38, thereby facilitating the assembly of the second pull rod 22 and the second connecting block 38. In other embodiments, the second groove 37 can also be formed by a concave portion at the junction of the side of the connecting section 58 facing the main body 201 and the bottom surface of the connecting section 58 parallel to the rotating section 57 (i.e., the surface facing downward in the direction of gravity).

[0054] In this embodiment, referring to FIG8 , the openings of the two second mating holes 24 on opposite sides of the tilting bracket 12 are each provided with a second sealing cover 26 . The second tie rod 22 and the two second vibration dampers 20 are located between the two second sealing covers 26 . The second sealing covers 26 seal the openings on both sides of the tilting bracket 12, significantly reducing the possibility of water entering the second mating holes 24 . This protects the second tie rod 22 and the second vibration damper 20, reducing the possibility of damage or shortening the life of the second vibration damper 20 due to water, thereby extending the service life of the second vibration damper 20 and ensuring its vibration absorption function.

[0055] In this embodiment, referring to FIG8 , the second sealing cover 26 is provided with a second sealing block 30 that extends into the second mating hole 24. A second external thread 31 is provided on the side of the second sealing block 30, and a second internal thread 32 is provided in the second mating hole 24. The second external thread 31 is threadedly engaged with the second internal thread 32 to securely connect the second sealing cover 26 to the tilting bracket 12. In other embodiments, the second sealing cover 26 may alternatively be interference fit within the second mating hole 24, or secured to the tilting bracket 12 via set screws to seal the openings on both sides of the tilting bracket 12.

[0056] In this embodiment, referring to FIG8 , a locking member 39 is provided at the end of the second pull rod 22. The locking member 39 is used to lock the second pull rod 22 to the tilting bracket 12, thereby fixing the second vibration damper 20 to the tilting bracket 12. One end of the second pull rod 22 passes through the second connecting block 38 from one second matching hole 24 and extends into the other second matching hole 24. Ultimately, the two ends of the second pull rod 22 are respectively located in the two second matching holes 24 and simultaneously engage with the two second vibration dampers 20. The locking member 39 is connected to the second pull rod 22 from one end and locked between one second vibration damper 20 and the first sealing cover 25 or the second sealing cover 26, thereby fixing the second pull rod 22, and thus the second pull rod 22 and the locking member 39 fix the two second vibration dampers 20. In this embodiment, the locking member 39 may be threadedly connected to the second pull rod 22 , may be interference-fitted to the second pull rod 22 , or may be fixedly connected to the second pull rod 22 by other connection means such as pins and screws.

[0057] In other embodiments, two locking members 39 are provided, and the two locking members 39 are respectively fixedly connected to the second pull rod 22 and abut against the opposite ends of the two second vibration dampers 20 to fix the two second vibration dampers 20 on the second pull rod 22.

[0058] In this embodiment, referring to Figure 6, an avoidance groove 66 is provided on the side of the connecting section 58 of the lifting bracket 12 facing the main unit 201. The length direction of the avoidance groove 66 is perpendicular to the rotation axis 18 of the lifting bracket 12. The connecting rod 15 is partially fitted in the avoidance groove 66 to reduce the size of the lifting clamp 10 in the propulsion direction 69 of the propeller 200, thereby improving the applicability of the lifting clamp 10.

[0059] In this embodiment, referring to Figures 6 to 8 , two first vibration dampers 19 are provided. Two first vibration dampers 19 connect the first end 16 to the tilting bracket 12 on either side. Two second vibration dampers 20 are provided. Two second vibration dampers 20 connect the second end 17 to the tilting bracket 12 on either side. Specifically, the two first vibration dampers 19 are spaced apart along the rotation axis 18 of the tilting bracket 12, and the two second vibration dampers 20 are spaced apart along the rotation axis 18 of the tilting bracket 12. This increases the vibration-damping contact area between the ends of the connecting rod 15 and the tilting bracket 12, enhancing the vibration absorption effect of the vibration-damping structure 14. Furthermore, the first end 16 is connected to the tilting bracket 12 via two fulcrums, and the second end 17 is connected to the tilting bracket 12 via two fulcrums. This improves the connection stability between the connecting rod 15 and the tilting bracket 12, allowing the tilting bracket 12 to stably and reliably drive the main unit 201 connected to the connecting rod 15 to tilt during tilting, ensuring reliable and secure tilting.

[0060] Example 2

[0061] FIG9 shows another lifting jig 10 , which is different from the aforementioned lifting jig 10 in that the specific structure of the vibration reduction structure 14 of the lifting jig 10 is different.

[0062] In this embodiment, the second vibration damper 20 is a cylindrical damper, with its geometric center axis perpendicular to the rotation axis 18 of the tilting bracket 12. The second vibration damper 20 is used to absorb radial vibrations of the propeller 200. Two first vibration dampers 19 are provided. Both of these first vibration dampers 19 are cylindrical dampers, with their geometric center axes perpendicular to the rotation axis 18 of the tilting bracket 12. The first vibration dampers 19 are used to absorb radial vibrations of the propeller 200. The second vibration damper 20 can absorb steering-direction vibrations generated by the steering actuator 204 when it outputs steering torque, steering-direction vibrations imposed on the main engine 201 by waves, and vibrations in the propulsion direction 69 generated by the power unit 208. The first vibration damper 19 can absorb vibrations generated by the power unit 208 along the propulsion direction 69, as well as vibrations caused by the main engine 201's gravity during the tilting process. Thus, the first vibration damper 19 and the second vibration damper 20 cooperate to absorb the vibration in the X, Y, and Z directions of the three-dimensional coordinate system, thereby improving the comprehensiveness of vibration damping.

[0063] In this embodiment, two first vibration dampers 19 are provided, spaced apart along the rotational axis 18 of the tilting bracket 12. A single second vibration damper 20 is provided. During the tilting process of the tilting fixture 10, the moment arms at the first end 16 and underwater portion 203 on either side of the second end 17 are relatively large. The first vibration dampers 19 experience greater lateral tension, while the second vibration dampers 20 experience relatively less thrust. The second vibration damper 20 forms the intermediate fulcrum of the moment-balancing moment arm. This results in relatively less force on the second vibration damper 20, allowing only one second vibration damper 20 at the second end 17 to meet vibration absorption requirements and balance torque during the tilting process. In other embodiments, three or more first vibration dampers 19 may also be provided. In this embodiment, the first vibration dampers 19 are provided on either side of the connecting rod 15 along the rotational axis 18 of the tilting bracket 12, while the second vibration damper 20 is sleeved onto the connecting rod 15. In this way, the two first vibration dampers 19 and the second vibration dampers 20 are symmetrically distributed about the connecting rod 15, so that the fulcrum formed by the second vibration damper 20 can provide relatively balanced support for the force arms at the two first vibration dampers 19. In other embodiments, the distribution of the two first vibration dampers 19 and the second vibration damper 20 can also be adjusted according to actual needs.

[0064] In this embodiment, the tilting bracket 12 is provided with a rotation hole 50, the length of which is perpendicular to the rotation axis 18 of the tilting bracket 12. The connecting rod 15 fits within the rotation hole 50, and the second vibration damper 20 fits between the second end 17 of the connecting rod 15 and the rotation hole 50. Specifically, the second vibration damper 20 defines an axial hole along its axis, and the second end 17 penetrates into the axial hole and tightly fits with the inner wall of the axial hole. The second vibration damper 20 is assembled within the rotation hole 50 and tightly fits with the inner wall of the rotation hole 50. The rotation hole 50 serves as a position limit for the connecting rod 15 and also facilitates the installation of the second vibration damper 20, whose geometric center axis is perpendicular to the rotation axis 18 of the tilting bracket 12, between the connecting rod 15 and the tilting bracket 12. In other embodiments, instead of providing the rotation hole 50 on the tilting bracket 12, a boss can be provided on the end of the connecting section 58 facing away from the rotation section 57, and a connecting structure can be provided at the second end 17. The connecting structure engages with the boss, and the second vibration damper 20 engages between the boss and the connecting structure to facilitate installation of the second vibration damper 20. The connection between the second vibration damper 20, the boss, and the connecting structure can be referenced to the connection between the second vibration damper 20, the second mating hole 24, and the second pull rod 22 in the first embodiment, and will not be further described here. Therefore, there are many ways to install the second vibration damper 20 with the tilting bracket 12 and the connecting rod 15, which are not specifically limited here.

[0065] In this embodiment, the connecting assembly 13 further includes a third connecting block 40 and a third pull rod 41. The third connecting block 40 is protruded from the first end 16 along the propulsion direction 69. The third pull rod 41 is provided on the third connecting block 40. The tilting bracket 12 is provided with a third mating hole 42. The first vibration damper 19 is fitted between the third mating hole 42 and the third pull rod 41. Specifically, the first vibration damper 19 has an axial hole along its axis. The third pull rod 41 passes through the axial hole and tightly fits with the inner wall of the axial hole. The first vibration damper 19 is assembled in the third mating hole 42 and tightly fits with the inner wall of the third mating hole 42. In this embodiment, the third pull rod 41 can be threadedly connected to the third connecting block 40 or locked to the third connecting block 40 by a locking structure. In other embodiments, the third connecting block 40 can be provided on the tilting bracket 12, and the third mating hole 42 can be provided on the connecting assembly 13. In this embodiment, a cover may be provided at the opening of the third matching hole 42 to seal the opening of the third matching hole 42 and protect the third pull rod 41 and the first vibration damper 19 .

[0066] In this embodiment, the tilting bracket 12 is provided with a third groove 43. Third mating holes 42 are provided on opposite sides of the third groove 43. The ends of the third pull rod 41 respectively engage with the two third mating holes 42. The two first vibration dampers 19 respectively engage between the two third mating holes 42 and the two third pull rods 41. In this embodiment, the third groove 43 is formed by an inward depression on the side of the tilting bracket 12 facing the main unit 201 and is located at the junction of the rotating section 57 and the connecting section 58.

[0067] Example 3

[0068] FIG10 to FIG12 show another lifting jig 10 , which is different from the lifting jig 10 of the second embodiment in that the specific structure of the first vibration damping member 19 of the lifting jig 10 is different.

[0069] Referring to Figures 10 and 11 , in this embodiment, the second vibration damper 20 is a cylindrical damper, with its geometric center axis perpendicular to the rotation axis 18 of the tilting bracket 12. The second vibration damper 20 is used to absorb radial vibration of the propeller 200. The two first vibration dampers 19 are cylindrical dampers, with their geometric center axes perpendicular to the rotation axis 18 of the tilting bracket 12. The first vibration dampers 19 are used to absorb radial vibration of the propeller 200. In this embodiment, both the first and second vibration dampers 19 and 20 can absorb steering-direction vibration generated by the steering actuator 204 outputting steering torque, steering-direction vibration imposed on the main unit 201 by waves, and propulsion-direction vibration 69 generated by the power section 208. Furthermore, when the tilting bracket 12 drives the connecting assembly 13 to rotate, the first and second vibration dampers 19 and 20 can also absorb vibration caused by gravity during the tilting of the main unit 201. In this embodiment, the steering shaft 51 is connected to the first end portion 16 , and a first steering gear portion 52 is provided on a side of the steering shaft 51 away from the first end portion 16 .

[0070] In this embodiment, referring to Figures 10 and 11 , the connecting assembly 13 further includes an adapter block 44, one end of which is connected to the first end portion 16. The other end of the adapter block 44 is provided with two mounting holes 70. The tilting bracket 12 is provided with two mounting posts 45, which are spaced apart along the rotation axis 18 of the tilting bracket 12. The two mounting posts 45 respectively fit within the two mounting holes 70, and the first vibration damper 19 fits between the mounting holes 70 and the mounting posts 45. Specifically, the first vibration damper 19 defines an axial hole along its axis, and the mounting posts 45 extend through the axial hole and tightly fit within the inner wall of the axial hole. The first vibration damper 19 is assembled within the mounting hole 70 and tightly fits within the inner wall of the mounting hole 70. In other embodiments, the mounting hole 70 may be provided on the tilting bracket 12, and the mounting posts 45 may be provided at the end of the adapter block 44. This can also achieve the installation of the first vibration damper 19 between the tilting bracket 12 and the connecting assembly 13.

[0071] In this embodiment, referring to Figures 11 and 12, the lifting clamp 10 also includes a fixing screw 47 and a fixing gasket 48. The fixing gasket 48 cooperates with the first vibration damper 19 and abuts against the mounting column 45. The fixing screw 47 is threadedly connected to the mounting column 45 and locks the fixing gasket 48 to the mounting column 45 to fix the first vibration damper 19 to the mounting column 45, thereby realizing the fixed installation of the first vibration damper 19 between the lifting bracket 12 and the adapter block 44.

[0072] In this embodiment, the lifting bracket 12 is provided with a mounting groove 46, two mounting posts 45 protruding from the bottom surface of the mounting groove 46, and the adapter block 44 is mounted within the mounting groove 46. The mounting groove 46 helps reduce the size of the lifting bracket 12 in the direction of gravity, thereby reducing the size of the lifting fixture 10 in the direction of gravity and increasing the applicability of the lifting fixture 10. In this embodiment, a buffer pad 49 is also provided between the adapter block 44 and the bottom surface of the mounting groove 46. The buffer pad 49 provides reliable support for the connecting assembly 13 and the main unit 201, and also provides a buffering and support function for collisions between the adapter block 44 and the lifting bracket 12 during the lifting process of the lifting bracket 12.

[0073] In this embodiment, referring to FIG11 , a connection portion 68 is provided at the lower end of the tilting bracket 12, and the rotation hole 50 is disposed within the connection portion 68. A sidewall of the tilting bracket 12 is also provided with an escape groove 66, which communicates with the rotation hole 50. In other embodiments, the tilting bracket 12 may also be provided with a complete rotation hole 50 that accommodates the first end 16 and the second end 17 of the connecting rod 15.

[0074] Example 4

[0075] FIG13 shows another lifting jig 10 , which is different from the lifting jig 10 of the previous embodiment in that the specific structures of the first vibration damping member 19 and the second vibration damping member 20 of the lifting jig 10 are different.

[0076] In this embodiment, the first vibration damper 19 is a cylindrical damper with its geometric center axis perpendicular to the rotation axis 18 of the tilting bracket 12. The first vibration damper 19 is used to absorb vibration of the propeller 200 in its radial direction. The second vibration damper 20 is a cylindrical damper with its geometric center axis parallel to the rotation axis 18 of the tilting bracket 12. The second vibration damper 20 is used to absorb vibration of the propeller 200 in its radial direction. The first vibration damper 19 can absorb the steering vibration generated by the steering actuator 204 when it outputs steering torque, the steering vibration exerted on the main engine 201 by waves, and the vibration in the propulsion direction 69 generated by the power section 208. The second vibration damper 20 can absorb the vibration generated by the power section 208 along the propulsion direction 69 and the vibration caused by the weight of the main engine 201 during the tilting process. Thus, the first vibration damper 19 and the second vibration damper 20 work together to absorb vibration in the X, Y, and Z directions of the three-dimensional coordinate system, improving comprehensive vibration reduction.

[0077] In this embodiment, two first vibration dampers 19 are provided, and one second vibration damper 20 is provided. The first vibration dampers 19 are located on both sides of the connecting rod 15 along the rotation axis 18 , and the projection of the second vibration damper 20 in the propulsion direction 69 is located on the connecting rod 15 . In other embodiments, three or more first vibration dampers 19 may be provided, and two, three, or more second vibration dampers 20 may be provided.

[0078] In this embodiment, referring to FIG13 , the tilting bracket 12 is provided with a protruding mounting rod 59, the length of which is perpendicular to the rotation axis 18 of the tilting bracket 12. The connecting assembly 13 further includes a fourth connecting block 60 disposed at the first end 16. The fourth connecting block 60 defines a straight hole 61, into which the mounting rod 59 fits, and a first vibration damper 19 fits between the mounting rod 59 and the straight hole 61. Specifically, the first vibration damper 19 defines an axial hole along its axis, into which the mounting rod 59 passes and tightly fits the inner wall of the axial hole. The first vibration damper 19 is assembled within the straight hole 61 and tightly fits the inner wall of the straight hole 61. In this embodiment, the first vibration damper 19 can be fastened to the mounting rod 59 by screws. The connection structure between the first vibration damper 19, the tilting bracket 12, and the connecting assembly 13 can be referred to in the connection structure of the first vibration damper 19, the tilting bracket 12, and the connecting assembly 13 in the third embodiment, and will not be further described here.

[0079] In this embodiment, referring to FIG. 13 , the connecting assembly 13 further includes a fourth tie rod 62 disposed at the second end 17. The lifting bracket 12 defines a fourth mating hole 63, into which the fourth tie rod 62 engages. The second vibration damper 20 engages between the fourth tie rod 62 and the fourth mating hole 63. Specifically, the second vibration damper 20 defines an axial hole along its axis. The fourth tie rod 62 extends into the axial hole and tightly engages with the inner wall of the axial hole. The second vibration damper 20 is assembled within the fourth mating hole 63 and tightly engages with the inner wall of the fourth mating hole 63. Furthermore, the lifting fixture 10 further includes a tie rod connecting block 67 disposed at the second end 17 and connected to the fourth tie rod 62. The specific connection structure of the second vibration damper 20, the lifting bracket 12, and the connecting assembly 13 in this embodiment can be referred to in the connection structure of the second vibration damper 20, the lifting bracket 12, and the connecting assembly 13 in the first embodiment, and will not be further described here.

[0080] The above embodiments are only used to illustrate the technical solutions of the present application and are not intended to limit the present application. Although the present application has been described in detail with reference to the above preferred embodiments, those skilled in the art should understand that modifications or equivalent replacements of the technical solutions of the present application should not depart from the spirit and scope of the technical solutions of the present application.

Claims

1. A lifting fixture for connecting a propeller to a water body, characterized in that: The warping fixture comprises: A fixed bracket, one side of which is used to connect the water area carrier; A tilting bracket, rotatably connected to the other side of the fixed bracket; A connecting component, the connecting component is used to connect the main engine of the thruster; A vibration-damping structure is provided between the lifting bracket and the connecting assembly, and is used to absorb vibration of the host.

2. The warping fixture according to claim 1, characterized in that: The connecting assembly is provided with a connecting rod, and the connecting rod has a first end and a second end distributed along the length direction thereof, and the length direction is perpendicular to the rotation axis of the tilting bracket, and the first end and the second end are respectively used to connect the above-water part of the main engine away from the underwater and the underwater part close to the underwater, and the vibration-damping structure includes a first vibration-damping member and a second vibration-damping member, the first end is connected to the tilting bracket through the first vibration-damping member, and the second end is connected to the tilting bracket through the second vibration-damping member.

3. The warping fixture according to claim 2, characterized in that: The first vibration damper is a columnar vibration damper, the geometric center axis of the first vibration damper is parallel to the rotation axis of the tilting bracket, and the first vibration damper is used to absorb the vibration of the propeller in its radial direction. The second vibration damper is a columnar vibration damper, the geometric center axis of the second vibration damper is parallel to the rotation axis of the tilting bracket, and the second vibration damper is used to absorb the vibration of the propeller in its radial direction.

4. The warping fixture according to claim 3, characterized in that: The connecting component is provided with a first pull rod and a second pull rod, the first pull rod is provided at the first end, the second pull rod is provided at the second end, the lifting bracket is provided with a first matching hole and a second matching hole arranged at intervals, the first pull rod is matched with the first matching hole, the first shock absorber is matched between the first matching hole and the first pull rod, the second pull rod is matched with the second matching hole, and the second shock absorber is matched between the second matching hole and the second pull rod.

5. The warping fixture according to claim 4, characterized in that: The first matching hole is a through hole that penetrates in a direction parallel to the rotation axis of the tilting bracket. The first matching hole is provided with a first sealing cover at the openings on opposite sides of the tilting bracket. The first pull rod and the first vibration dampening member are located between the two first sealing covers.

6. The warping fixture according to claim 4, characterized in that: The second matching hole is a through hole that penetrates in a direction parallel to the rotation axis of the tilting bracket. The second matching hole is provided with a second sealing cover at the openings on opposite sides of the tilting bracket. The second pull rod and the second vibration damping member are located between the two second sealing covers.

7. The warping fixture according to claim 5, characterized in that: The lifting bracket is provided with a first groove, and the first matching holes are provided on the opposite side walls of the first groove. One end of the first pull rod matches with one of the first matching holes, and the other end matches with the other first matching hole.

8. The warping fixture according to claim 7, characterized in that: The connecting assembly also includes a first connecting block, which is connected to the side wall of the first end portion. The first pull rod is provided with two locking rods, which are provided on both sides of the first connecting block and respectively matched with the two first matching holes. The first vibration damping member is matched between the locking rod and the hole surface of the first matching hole.

9. The warping fixture according to claim 8, characterized in that: The locking rod passes through the first vibration damping member and is threadedly connected to the first connecting block to lock the first vibration damping member between the locking rod and the first matching hole.

10. The warping fixture according to claim 8, characterized in that: The connection assembly is provided with a limit block, which is protruding from the first connection block, fits in the first groove, and is supported on the bottom surface of the first groove to support the first connection block and the first pull rod.

11. The warping fixture according to claim 4, characterized in that: The lifting bracket is provided with a second groove, and the opposite side walls of the second groove are provided with the second matching holes, and the second pull rod is matched with the two second matching holes and the second groove; the connecting component also includes a second connecting block, which is connected to the connecting rod and matched in the second groove to connect with the second pull rod.

12. The warping fixture according to claim 10, characterized in that: The openings of the two second matching holes on opposite sides of the tilting bracket are both provided with second sealing covers, and the second pull rod And the two second vibration damping members are located between the two second sealing covers.

13. The warping fixture according to claim 4, characterized in that: A locking piece is provided at the end of the second pull rod, and the locking piece is used to lock the second pull rod to the tilting bracket to fix the second vibration damping piece.

14. The warping fixture according to claim 4, characterized in that: There are two first vibration dampers, and both sides of the first end are connected to the tilting bracket through the two first vibration dampers respectively; there are two second vibration dampers, and both sides of the second end are connected to the tilting bracket through the two second vibration dampers respectively.

15. The warping fixture according to claim 2, characterized in that: The second vibration damper is a columnar vibration damper, the geometric center axis of the second vibration damper is perpendicular to the rotation axis of the tilting bracket, and the second vibration damper is used to absorb the vibration of the propeller in its radial direction.

16. The warping fixture according to claim 15, characterized in that: There are two first vibration damping members, which are spaced apart along the rotation axis of the tilting bracket, and there is only one second vibration damping member.

17. The warping fixture according to claim 16, characterized in that: The two first vibration dampers are columnar vibration dampers, and the geometric center axes of the two first vibration dampers are parallel to the rotation axis of the tilting bracket. The first vibration dampers are used to absorb the vibration of the propeller in its radial direction.

18. The warping fixture according to claim 17, characterized in that: The connecting assembly also includes a third connecting block and a third pull rod. The third connecting block is protruded from the connecting rod along the thrust direction. The third pull rod is arranged on the third connecting block. The lifting bracket is provided with a third matching hole. The first vibration damping member is matched between the third matching hole and the third pull rod.

19. The warping fixture according to claim 18, characterized in that: The lifting bracket is provided with a third groove, and the opposite side walls of the third groove are provided with third matching holes, the two ends of the third pull rod are respectively matched with the two third matching holes, and the two first vibration damping members are respectively matched between the two third matching holes and the two third pull rods.

20. The lifting fixture according to claim 16, characterized in that: The two first vibration dampers are columnar vibration dampers, and the geometric center axes of the two first vibration dampers are perpendicular to the rotation axis of the tilting bracket. The first vibration dampers are used to absorb the vibration of the propeller in its radial direction.

21. The warping fixture according to claim 20, characterized in that: The connecting assembly also includes an adapter block, one end of which is connected to the first end portion, and the other end of the adapter block is provided with two mounting holes. The tilting bracket is provided with two mounting columns, and the two mounting columns are spaced apart along the rotation axis of the tilting bracket. The two mounting columns are respectively engaged in the two mounting holes, and the first vibration damping member is engaged between the mounting holes and the mounting columns.

22. The warping fixture according to claim 21, characterized in that: The tilting bracket is provided with a mounting groove, the two mounting posts are protruding from the bottom surface of the mounting groove, and the adapter block is installed in the mounting groove.

23. The warping fixture according to claim 22, characterized in that: A buffer pad is also provided between the adapter block and the bottom surface of the installation groove.

24. The warping fixture according to claim 15, characterized in that: The tilting bracket is provided with a rotation hole, the length direction of the rotation hole is perpendicular to the rotation axis of the tilting bracket, the connecting rod is fitted in the rotation hole, and the second vibration damping member is fitted between the second end of the connecting rod and the rotation hole.

25. The warping fixture according to claim 2, characterized in that: The connecting assembly further comprises a steering shaft, which is connected to the first end portion and is used for rotationally cooperating with a steering actuator of the host machine.

26. The warping fixture according to claim 25, characterized in that: The lifting fixture also includes a bearing and a seal. The bearing is used to be fixed to the main machine, and the steering shaft is assembled in the bearing. The seal is sleeved on the steering shaft and abuts against one end of the bearing facing the connecting rod.

27. The warping fixture according to claim 25, characterized in that: The main engine is provided with a steering shaft hole close to the underwater part, and the second end portion is fitted in the steering shaft hole. The lifting fixture also includes a supporting bushing which is sleeved on the second end portion and fits in the steering shaft hole, and the supporting bushing is used to support the connecting rod.

28. The warping fixture according to claim 1, characterized in that: The tilting bracket includes a rotating section and a connecting section, the rotating section is rotatably connected to the fixed bracket, the connecting section is bent and connected to the rotating section, the length direction of the connecting section is perpendicular to the rotating axis of the rotating section, and the connecting assembly is connected to the connecting section through the vibration damping structure.

29. The warping fixture according to claim 2, characterized in that: The first vibration damper is a columnar vibration damper, the geometric center axis of the first vibration damper is perpendicular to the rotation axis of the tilting bracket, and the first vibration damper is used to absorb the vibration of the propeller in its radial direction; the second vibration damper is a columnar vibration damper, the geometric center axis of the second vibration damper is parallel to the rotation axis of the tilting bracket, and the second vibration damper is used to absorb the vibration of the propeller in its radial direction.

30. The warping fixture according to claim 29, characterized in that: The tilting bracket is provided with a protruding mounting rod, the length direction of the mounting rod is perpendicular to the rotation axis of the tilting bracket, the connecting assembly also includes a fourth connecting block arranged at the first end, the fourth connecting block is provided with a straight hole, the mounting rod is fitted in the straight hole, and the first vibration damping member is fitted between the mounting rod and the straight hole.

31. The warping fixture according to claim 29, characterized in that: The connecting assembly also includes a fourth pull rod, which is arranged at the second end, the lifting bracket has a fourth matching hole, the fourth pull rod is matched with the fourth matching hole, and the second vibration damping member is matched between the fourth pull rod and the fourth matching hole.

32. The warping fixture according to claim 1, characterized in that: The lifting fixture further includes a lifting driving member, which is connected between the fixed bracket and the lifting bracket and is used for driving the lifting bracket to rotate relative to the fixed bracket.

33. The warping fixture according to claim 32, characterized in that: One end of the tilting driving member is rotatably connected to the fixed bracket, and the other end is rotatably connected to the tilting bracket, and its rotation axis is parallel and spaced from the rotation axis of the tilting bracket relative to the fixed bracket, and the tilting driving member is retractable.

34. A propeller, characterized in that: include: Host; According to the lifting clamp as described in any one of claims 1 to 33, the host is connected to the connecting component of the lifting clamp.

35. The propeller according to claim 34, characterized in that: The main machine also includes a frame, a steering actuator and a power part. The frame is connected to the connecting component. The steering actuator is arranged on the frame and cooperates with the connecting component to drive the frame to rotate relative to the lifting fixture. The power part is arranged on the frame to output propulsion power.

36. The propeller according to claim 35, characterized in that: The power part includes a propulsion motor and a propeller. The propulsion motor is transmission-connected to the propeller to drive the propeller to rotate and generate propulsion force.

37. A movable device in water area, characterized in that: include: Water carrier; The thruster according to any one of claims 34 to 36, wherein the fixed bracket is connected to the water body carrier.

Citation Information

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