Clamping assembly, clamping mechanism, unmanned aerial vehicle cabin and vehicle

Abstract

The utility model relates to a clamping assembly, a clamping mechanism, an unmanned aerial vehicle cabin, a vehicle and a clamping piece. The abutting piece is movably mounted on the clamping piece and can move relative to the clamping piece when being stressed; the clamping piece is suitable for abutting against the unmanned aerial vehicle in the moving direction of the abutting piece through the abutting piece. According to the technical scheme, the possibility that the clamping assembly damages the structure of the unmanned aerial vehicle is reduced.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of clamping assemblies, in particular to a clamping assembly, a clamping mechanism, a UAV nacelle and a vehicle. BACKGROUND

[0002] At present, the unmanned aerial vehicle industry develops rapidly, and the vehicle-mounted unmanned aerial vehicle is an inevitable product of technological development, which has more and more extensive application market. However, the existing unmanned aerial vehicle is clamped and fixed by a clamping device after landing on the unmanned aerial vehicle platform, but due to the large force of the clamping device, the structure of the unmanned aerial vehicle may be damaged, thereby reducing the service life of the unmanned aerial vehicle. CONTENT OF THE INVENTION

[0003] The embodiment of the present application provides a clamping assembly, which reduces the possibility of damage to the structure of the unmanned aerial vehicle by the clamping assembly, so as to at least partially solve the above technical problems.

[0004] In order to achieve the above purpose, according to the first aspect of the present application, a clamping assembly is provided, comprising: a clamping piece; an abutting piece movably installed on the clamping piece and movable relative to the clamping piece under stress; wherein the clamping piece is adapted to abut the unmanned aerial vehicle along the movement direction of the abutting piece through the abutting piece.

[0005] Optionally, the clamping piece has a first accommodating cavity, and at least a part of the abutting piece is movably installed in the first accommodating cavity.

[0006] Optionally, the clamping assembly further comprises an elastic piece, and the elastic piece is adapted to elastically connect the abutting piece and the cavity wall of the first accommodating cavity.

[0007] Optionally, the clamping assembly further comprises a first buffer piece, and the first buffer piece is arranged on the abutting piece, and the abutting piece is adapted to abut the unmanned aerial vehicle through the first buffer piece.

[0008] Optionally, the clamping assembly further comprises a first limiting structure, and the first limiting structure is located between the abutting piece and the first buffer piece to limit the movement position of the abutting piece.

[0009] Optionally, one end of the abutting piece close to the first buffer piece is provided with a first step structure, one end of the first buffer piece close to the abutting piece is provided with a second step structure, and the first step structure and the second step structure cooperate to form the first limiting structure.

[0010] Optionally, the clamping assembly further comprises a limiting piece, and the limiting piece is arranged on the abutting piece, and the limiting piece is used for abutting the clamping piece to limit the position of the abutting piece.

[0011] Optionally, the clamping assembly further comprises a positioning piece, and the positioning piece is arranged on the clamping piece, and the positioning piece is used for abutting the unmanned aerial vehicle to position the position of the unmanned aerial vehicle.

[0012] Optionally, the clamping assembly further comprises a second buffer configured to abut against the outer component to limit the position of the clamping member.

[0013] Optionally, the clamping assembly further comprises a drone charging port and a wire harness, the wire harness being adapted to connect the drone charging port.

[0014] Optionally, the wire harness comprises a protective shell and a connecting wire arranged in the protective shell, the protective shell being configured to limit the displacement of the connecting wire.

[0015] Optionally, the protective shell comprises a first section, a plurality of second sections, and a third section, an end of the third section away from the first section being connected to the clamping member, an end of the first section away from the third section being adapted to be connected to the rim of the base, wherein two adjacent second sections are rotatably connected, the other end of the first section is rotatably connected to the second section close to the first section, and the other end of the third section is rotatably connected to the second section close to the third section.

[0016] Optionally, the length of the third section is greater than the length of each second section.

[0017] Optionally, the clamping assembly further comprises a bushing arranged on the clamping member, the clamping member being adapted to be movably arranged on the guide rail, and the bushing being adapted to be arranged between the guide rail and the clamping member.

[0018] According to a second aspect of the present application, a clamping mechanism is provided, comprising a clamping assembly.

[0019] Optionally, the clamping mechanism further comprises a driving member and a transmission assembly, the driving member driving the clamping member of the clamping assembly to move through the transmission assembly.

[0020] Optionally, the transmission assembly comprises a first transmission member and a second transmission member, the driving member being connected to the clamping member through the first transmission member and the second transmission member, wherein the driving member is configured to drive the first transmission member to rotate, and the second transmission member is configured to drive the clamping member to move under the driving of the rotation of the first transmission member.

[0021] Optionally, the first transmission member is threadedly connected to the second transmission member.

[0022] Optionally, the first transmission member is one of a screw rod and a nut, and the second transmission member is the other one of the screw rod and the nut.

[0023] Optionally, the first transmission member has a double-end screw thread.

[0024] Optionally, the clamping mechanism comprises two clamping assemblies, the two clamping assemblies being configured to clamp a drone.

[0025] Optionally, the first transmission member comprises two first transmission portions, the second transmission member comprises two second transmission portions, and the driving member is connected to the corresponding clamping member through the corresponding first transmission portion and the corresponding second transmission portion; wherein the driving member is configured to drive the first transmission portion to rotate, and the second transmission portion is adapted to move the clamping member under the driving of the rotation of the first transmission portion.

[0026] Optionally, the two first transmission portions are fixedly connected.

[0027] Optionally, the two first transmission portions are fixedly connected.

[0028] Optionally, the two first transmission portions are fixedly connected.

[0029] Optionally, the clamping mechanism further comprises a base, and the base is provided with a fixing seat, the fixing seat comprises a through hole portion, and the through hole portion is provided with a through hole; wherein the first transmission member is rotatably installed in the through hole.

[0030] Optionally, the first transmission member is in interference fit with the through hole.

[0031] Optionally, the outer peripheral wall of the through hole portion is provided with a reinforcing structure.

[0032] Optionally, the inner side wall of the through hole portion is provided with a protruding portion, and the protruding portion is configured to abut against the outer peripheral wall of the transmission member.

[0033] Optionally, the fixing seat is provided with at least one hollow portion, and the at least one hollow portion surrounds the through hole portion.

[0034] Optionally, the fixing seat comprises at least a first fixing seat and a second fixing seat; the first fixing seat is arranged at the fixed connection position of the two first transmission portions, and the shaft sleeve is rotatably installed in the through hole of the first fixing seat; and the second fixing seat is arranged at the end portion of the two first transmission portions.

[0035] Optionally, the clamping mechanism further comprises a guide rail, and the clamping member is movably arranged on the guide rail; the driving member drives the clamping member to move along the guide rail through the first transmission member and the second transmission member; and the first fixing seat is further provided with a guide rail mounting hole, and the guide rail passes through the guide rail mounting hole.

[0036] Optionally, the clamping mechanism further comprises a damping pad, and the damping pad is arranged around the outer periphery of the second transmission member and is in interference fit with the second transmission member.

[0037] According to a third aspect of the present application, a UAV nacelle is also provided, comprising the clamping assembly or the clamping mechanism as above.

[0038] According to a fourth aspect of the present application, a vehicle is also provided, comprising the clamping assembly, the clamping mechanism, or the UAV nacelle.

[0039] The clamping assembly of the embodiment of the present application comprises a clamping piece, and an abutting piece movably mounted on the clamping piece; wherein the clamping piece is adapted to abut against the unmanned aerial vehicle through the abutting piece along the moving direction of the abutting piece. Through the above technical solution, the movable abutting piece is arranged on the clamping piece, and in the process of clamping the unmanned aerial vehicle by the clamping piece, the abutting piece can be used to buffer the contact force between the clamping piece and the unmanned aerial vehicle, so as to avoid damaging the structure of the unmanned aerial vehicle when the clamping piece moves to the limit position, thereby improving the service life of the unmanned aerial vehicle.

[0040] Other features and advantages of the present application will be described in detail in the following specific embodiments. BRIEF DESCRIPTION OF DRAWINGS

[0041] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiment description. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can also be obtained by those skilled in the art without creative labor on the basis of these drawings.

[0042] In order to more completely understand the present application and its beneficial effects, the following will be described in conjunction with the drawings, wherein the same reference numerals in the following description represent the same parts.

[0043] Figure 1 is the overall structure schematic diagram of the clamping mechanism provided in the exemplary embodiment of the present disclosure;

[0044] Figure 2 is the bottom view schematic diagram of the clamping mechanism provided in the exemplary embodiment of the present disclosure;

[0045] Figure 3 is the structure schematic diagram of the clamping assembly provided in the exemplary embodiment of the present disclosure;

[0046] Figure 4 is the structure schematic diagram of the clamping assembly provided in the exemplary embodiment of the present disclosure;

[0047] Figure 5 is the partial structure cross-sectional schematic diagram of the clamping assembly provided in the exemplary embodiment of the present disclosure;

[0048] Figure 6 is the partial structure schematic diagram of the clamping assembly provided in the exemplary embodiment of the present disclosure;

[0049] Figure 7 is the structure schematic diagram of the bushing provided in the exemplary embodiment of the present disclosure;

[0050] Figure 8 is the structure schematic diagram of the wire harness provided in the exemplary embodiment of the present disclosure;

[0051] Figure 9 is a structural schematic view of a wire harness provided in the exemplary embodiment of the present disclosure;

[0052] Figure 10 is a structural schematic view of a first fixing seat provided in the exemplary embodiment of the present disclosure;

[0053] Figure 11 is a structural schematic view of a first fixing seat provided in the exemplary embodiment of the present disclosure.

[0054] Legend of reference signs:

[0055] Clamping assembly 1, clamping piece 10, first accommodating cavity 11, first stepped structure 12, abutting piece 20, elastic piece 30, first buffer piece 40, second stepped structure 41, first limiting structure 13, limiting piece 50, positioning piece 60, second buffer piece 70, wire harness 80, protective shell 81, first section 811, second section 812, third section 813, connecting wire 82, bushing 90, clamping mechanism 100, driving piece 110, transmission assembly 120, first transmission piece 130, second transmission piece 140, base 150, first fixing seat 160, first through hole part 170, first reinforcing structure 180, first protruding part 190, first hollowed-out part 200, second fixing seat 210, second through hole part 220, second reinforcing structure 230, second protruding part 240, second hollowed-out part 250, damping pad 260, guide rail mounting hole 270, guide rail 280. DETAILED DESCRIPTION

[0056] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor are within the protection scope of the present application.

[0057] As Figures 1 to 11 shown, in order to achieve the above-mentioned purpose, according to the first aspect of the present application, a clamping assembly 1 is provided, comprising:

[0058] The clamping piece 10; the abutting piece 20 is movably installed on the clamping piece 10 and can move relative to the clamping piece 10 under stress; wherein the clamping piece 10 is adapted to abut the unmanned aerial vehicle through the abutting piece 20 along the movement direction of the abutting piece 20.

[0059] By the above technical scheme, the movable abutting piece 20 is arranged on the clamping piece 10, and the abutting piece 20 is used to buffer the contact force between the clamping piece 10 and the unmanned aerial vehicle during the clamping of the unmanned aerial vehicle by the clamping piece 10, so that the structure of the unmanned aerial vehicle is prevented from being damaged when the clamping piece 10 moves to the limit position, and the service life of the unmanned aerial vehicle is improved.

[0060] Optionally, the clamping piece 10 has a first accommodating cavity 11, and at least a part of the abutting piece 20 is movably arranged in the first accommodating cavity 11. By the above arrangement, the movement of the abutting piece 20 can be guided, so that the movement accuracy of the abutting piece 20 is improved, and the movement efficiency of the abutting piece 20 is also improved.

[0061] Optionally, the clamping assembly 1 further comprises an elastic piece 30, and the elastic piece 30 is adapted to elastically connect the abutting piece 20 and the cavity wall of the first accommodating cavity 11. In the present application, the elastic piece 30 comprises a spring, so that the abutting piece 20 can be in close contact with the unmanned aerial vehicle by the elastic force of the spring, so as to prevent the unmanned aerial vehicle from being displaced.

[0062] Optionally, the clamping assembly 1 further comprises a first buffer piece 40, and the first buffer piece 40 is arranged on the abutting piece 20, and the abutting piece 20 is adapted to abut against the unmanned aerial vehicle through the first buffer piece 40. When the unmanned aerial vehicle is clamped, the first buffer piece 40 directly contacts the unmanned aerial vehicle and can be contracted within a certain range, so as to avoid damaging the unmanned aerial vehicle.

[0063] Optionally, the clamping assembly 1 further comprises a first limiting structure 13, and the first limiting structure 13 is located between the abutting piece 20 and the first buffer piece 40 to limit the movement position of the abutting piece 20. In this way, the abutting piece 20 is prevented from being excessively displaced to cause clamping failure, so as to improve the use stability of the clamping assembly 1.

[0064] Optionally, an end of the abutting piece 20 close to the first buffer piece 40 is provided with a first step structure 12, an end of the first buffer piece 40 close to the abutting piece 20 is provided with a second step structure 41, and the first step structure 12 and the second step structure 41 cooperate to form the first limiting structure 13. The first limiting structure 13 is formed by the first buffer piece 40 and the structure of the abutting piece 20 itself, which can reduce the production cost of the first limiting structure 13, thereby facilitating the batch production of the assembly.

[0065] Optionally, the clamping assembly 1 further comprises a limiting piece 50, and the limiting piece 50 is arranged on the abutting piece 20 and is used to abut against the clamping piece 10 to limit the position of the abutting piece 20. In this way, the abutting piece 20 is prevented from being excessively displaced to cause clamping failure, so as to improve the use stability of the clamping assembly 1.

[0066] Optionally, the clamping assembly 1 further comprises a positioning member 60, which is arranged on the clamping member 10 and used to abut against the UAV to position the UAV. By arranging the above structure, the clamping precision of the clamping assembly 1 can be improved, and the clamping efficiency of the clamping assembly 1 is ensured.

[0067] Optionally, the clamping assembly 1 further comprises a second buffer member 70, which is configured to abut against an external component to limit the position of the clamping member 10. In this way, the second buffer member 70 plays a buffering and protecting role when clamping the UAV, thereby prolonging the service life of the clamping member 10.

[0068] In the present application, the second buffer member 70 is a rubber sleeve, and the external component is another second buffer member 70 on another clamping assembly 1. When clamping the UAV, the left and right second buffer members 70 are pressed against each other, thereby playing a buffering and protecting role for the clamping member 10.

[0069] Optionally, the clamping assembly 1 further comprises a UAV charging port and a wire harness 80, which is adapted to be connected to the UAV port. In this way, the clamping member 10 can charge the UAV at the same time when clamping and fixing the UAV, thereby avoiding the problem of manually charging or replacing the battery of the UAV. At the same time, the charging port also has a data transmission function, and the data of the UAV can be displayed on the display in the vehicle when the clamping block clamps and fixes the UAV.

[0070] Optionally, the wire harness 80 comprises a protective shell 81 and a connecting wire 82 arranged in the protective shell 81, and the protective shell 81 is used to limit the displacement of the connecting wire 82. In this way, the wire harness 80 can be prevented from moving randomly during movement, the wire harness 80 is ensured to be within a specified range, and the stability of the device during use is improved.

[0071] Optionally, the protective shell 81 comprises a first section 811, a plurality of second sections 812, and a third section 813. The end of the third section 813 away from the first section 811 is connected to the clamping member 10, the end of the first section 811 away from the third section 813 is adapted to be connected to the edge of the base 150, and the other end of the first section 811 is rotatably connected to the second section 812 close to the first section 811, and the other end of the third section 813 is rotatably connected to the second section 812 close to the third section 813.

[0072] In the present application, the first section 811, the second section 812, and the third section 813 are all made of plastic material, which reduces the production cost of the device and is conducive to the batch production of the device.

[0073] Optionally, the length of the third section 813 is greater than the length of each second section 812. This can avoid the wire harness 80 near the charging head side from being bent and deformed, thereby improving the safety during charging.

[0074] Optionally, the clamping assembly 1 further comprises a bushing 90, which is arranged between the clamping member 10 and the guide rail 280. By arranging the bushing 90, the product manufacturing error can be accommodated, and the problem of abnormal noise during movement caused by direct metal-to-metal contact can be avoided.

[0075] According to a second aspect of the present application, a clamping mechanism 100 is provided, comprising the clamping assembly 1.

[0076] Optionally, the clamping mechanism 100 further comprises a driving member 110 and a transmission assembly 120, the driving member 110 drives the clamping member 10 of the clamping assembly 1 to move through the transmission assembly 120. In this way, the automation of the clamping mechanism 100 is realized, thereby improving the clamping efficiency.

[0077] Optionally, the transmission assembly 120 comprises a first transmission member 130 and a second transmission member 140, the driving member 110 is connected to the clamping member 10 through the first transmission member 130 and the second transmission member 140, and the driving member 110 is configured to drive the first transmission member 130 to rotate, and the second transmission member 140 is configured to drive the clamping member 10 to move under the driving of the rotation of the first transmission member 130. By arranging the above structure, the space occupation problem caused by direct connection is avoided, and the overall structure is more compact. Due to the compact structure, this assembly can realize the required function in a limited space, improving the space utilization.

[0078] The design of the first transmission member 130 and the second transmission member 140 can effectively transmit the power of the driving member 110, reduce energy loss, and improve transmission efficiency. By accurately designing the transmission ratio and transmission mode, the precise control of the moving distance of the clamping member 10 can be realized, meeting the needs of different application scenarios.

[0079] Optionally, the first transmission member 130 is threadedly connected to the second transmission member 140. The connection is realized by the mutual engagement between the threads, which can ensure the precision and stability during transmission, thereby improving the performance of the entire transmission system.

[0080] Optionally, the first transmission member 130 is one of a screw rod and a nut, and the second transmission member 140 is the other one of the screw rod and the nut. The above setting structure is simple and easy to process, thereby reducing the production cost of the device.

[0081] Optionally, the first transmission member 130 has a double-end screw thread. In this way, the movement speed of the clamping member 10 can be increased, thereby improving the clamping efficiency of the device.

[0082] Optionally, the clamping mechanism 100 comprises two clamping assemblies 1, the two clamping assemblies 1 are opposite in movement direction, and the two clamping assemblies 1 are configured to clamp the unmanned aerial vehicle. In this way, the clamping effect on the unmanned aerial vehicle can be improved to ensure the clamping effect in the clamping assembly 1.

[0083] Optionally, the first transmission member 130 comprises two first transmission parts, the second transmission member 140 comprises two second transmission parts, and the driving member 110 is connected to the corresponding clamping member 10 through the corresponding first transmission part and the corresponding second transmission part; wherein the driving member 110 is used to drive the first transmission part to rotate, and the second transmission part is adapted to drive the clamping member 10 to move under the driving of the rotation of the first transmission part. In this way, the clamping effect on the unmanned aerial vehicle can be improved to ensure the clamping effect in the clamping assembly 1.

[0084] Optionally, the thread directions of the two first transmission parts are opposite. In this way, the two opposite clamping assemblies 1 can move towards or reverse each other to meet the use requirements of the device.

[0085] Optionally, the two first transmission parts are fixedly connected. In this way, the two first transmission parts can move synchronously, thereby improving the movement efficiency of the two first transmission parts.

[0086] Optionally, the two first transmission parts are fixedly connected through a shaft sleeve. The above-mentioned setting has a simple structure and is easy to process, thereby reducing the production cost of the device.

[0087] Optionally, the clamping mechanism 100 further comprises a base 150, the base 150 is provided with a fixing seat, the fixing seat comprises a through hole part, and the through hole part is provided with a through hole; wherein the first transmission member 130 is rotatably installed in the through hole.

[0088] Optionally, the first transmission member 130 is in interference fit with the through hole. In this way, the stability of the whole during operation can be ensured.

[0089] Optionally, the outer peripheral wall of the through hole part is provided with a reinforcing structure. In this way, the first transmission member 130 can be prevented from shaking in the first through hole, thereby ensuring the stability of the first transmission member 130 during operation.

[0090] Optionally, the inner side wall of the through hole part is provided with a protruding part, and the protruding part is configured to abut against the outer peripheral wall of the transmission member. In this way, the excessive holding force can be avoided, which can cause the first transmission member 130 to be stuck at low temperature, thereby improving the stability of the first transmission member 130 during operation.

[0091] Optionally, the fixing seat is provided with at least one hollowed part, and the at least one hollowed part surrounds the through hole part. Through the above structure, the through hole part can be deformed under the premise of ensuring the interference amount, so that the first transmission member 130 cannot be locked.

[0092] Optionally, the fixing seat at least includes a first fixing seat 160 and a second fixing seat 210; the first fixing seat 160 is arranged at the fixed connection position of the two first transmission parts, and the shaft sleeve is rotatably arranged in the through hole of the first fixing seat 160; the second fixing seat 210 is arranged at the end of the two first transmission parts. In this way, the stable operation of the first transmission can be ensured.

[0093] Optionally, the clamping mechanism 100 further includes a guide rail 280, the clamping member 10 is movably arranged on the guide rail 280; the driving member 110 drives the clamping member 10 to move along the guide rail 280 through the first transmission member 130 and the second transmission member 140; the first fixing seat 160 is further provided with a guide rail mounting hole 270, and the guide rail 280 passes through the guide rail mounting hole 270. In this way, the stability of the clamping mechanism 100 during movement can be improved, so as to ensure the normal operation of the device.

[0094] The through hole part includes a first through hole part 170 and a second through hole part 220, the reinforcing structure includes a first reinforcing structure 180 and a second reinforcing structure 230, the protruding part includes a first protruding part 190 and a second protruding part 240, and the hollowed part includes a first hollowed part 200 and a second hollowed part 250.

[0095] The first fixing seat 160 includes a first through hole part 170, and the first through hole part 170 is provided with a first through hole; wherein the shaft sleeve is rotatably arranged in the first through hole. In this way, the stability of the whole during operation can be ensured.

[0096] Optionally, the first transmission member 130 is in interference fit with the first through hole. In this way, the first transmission member 130 can be prevented from shaking in the first through hole, so as to ensure the stability of the first transmission member 130 during operation.

[0097] Optionally, the outer peripheral wall of the first through hole part 170 is provided with the first reinforcing structure 180. In this way, the strength of the first through hole can be ensured, and the product can be prevented from shaking during operation, so as to generate abnormal noise.

[0098] Optionally, the inner side wall of the first through hole part 170 is provided with the first protruding part 190, and the first protruding part 190 is configured to abut against the outer peripheral wall of the first transmission member 130. In this way, the excessive holding force can be avoided, so as to prevent the first transmission member 130 from being stuck at low temperature, and the stability of the first transmission member 130 during operation can be improved.

[0099] Optionally, the first fixed seat 160 is provided with at least one first hollowed part 200, and the at least one first hollowed part 200 surrounds the first through hole part 170. Through the above structure, the first through hole part 170 can be deformed under the premise of ensuring the interference amount, so that the first transmission member 130 cannot be locked.

[0100] Optionally, the base 150 is further provided with a second fixed seat 210, and the second fixed seat 210 comprises a second through hole part 220 provided with a second through hole; wherein the end of the first transmission member 130 is rotatably installed in the second through hole. In this way, the stability of the whole during operation can be ensured.

[0101] Optionally, the end of the first transmission member 130 is in interference fit with the second through hole. In this way, the first transmission member 130 can be prevented from shaking in the second through hole, so as to ensure the stability of the first transmission member 130 during operation.

[0102] Optionally, the outer side wall of the second through hole is provided with a second reinforcing structure 230 in the circumferential direction. In this way, the strength of the second through hole can be ensured, and the product can be prevented from shaking during operation, so as to produce abnormal noise.

[0103] Optionally, the inner side wall of the second through hole part 220 is provided with a second protruding part 240 configured to abut against the outer peripheral wall of the first transmission member 130. In this way, excessive holding force can be avoided, and the first transmission member 130 can be prevented from being stuck at low temperature, so as to improve the stability of the first transmission member 130 during operation.

[0104] Optionally, the second fixed seat 210 is provided with at least one second hollowed part 250, and the at least one second hollowed part 250 surrounds the second through hole part 220. Through the above structure, the second through hole part 220 can be deformed under the premise of ensuring the interference amount, so that the first transmission member 130 cannot be locked.

[0105] Optionally, the clamping mechanism 100 further comprises a damping pad 260, and the damping pad is arranged around the outer periphery of the second transmission member 140 and is in interference fit with the second transmission member 140. Through the above structure, the vibration during movement can be isolated, so as to reduce the possibility of abnormal noise generated during operation of the device.

[0106] According to a third aspect of the present application, a UAV nacelle is also provided, comprising the clamping assembly 1 or the clamping mechanism 100 as above.

[0107] According to a fourth aspect of the present application, a vehicle is also provided, comprising the clamping assembly 1, the clamping mechanism 100, or the UAV nacelle.

[0108] The clamping assembly 1 provided by the embodiment of the present application comprises a clamping piece 10, and an abutting piece 20 movably installed on the clamping piece 10, wherein the clamping piece 10 is adapted to abut against the unmanned aerial vehicle through the abutting piece 20 along the moving direction of the abutting piece 20. Through the above technical solution, the movable abutting piece 20 is arranged on the clamping piece 10, and the abutting piece 20 can be used to buffer the contact force between the clamping piece 10 and the unmanned aerial vehicle in the process that the clamping piece 10 clamps the unmanned aerial vehicle, so that the structure of the unmanned aerial vehicle is prevented from being damaged when the clamping piece 10 moves to the limit position, and the service life of the unmanned aerial vehicle is improved.

[0109] It should be noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments in accordance with the present application. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms "comprises" and / or "comprising," when used in this specification, specify the presence of stated features, steps, operations, elements, components, and / or groups thereof, but do not preclude the presence or addition of one or more other features, steps, operations, elements, components, and / or groups thereof.

[0110] The relative arrangement of parts and steps, numerical expressions, and numerical values set forth in the examples are not intended to limit the scope of the present application, unless otherwise specifically indicated. At the same time, it should be understood that the sizes of the various parts shown in the drawings are not drawn in accordance with the actual proportional relationship. The techniques, methods and devices known to those skilled in the relevant art can not be discussed in detail, but should be considered as part of the authorized description, if appropriate. In all examples shown and discussed herein, any specific value should be interpreted as merely exemplary, and not as a limitation. Therefore, other examples of exemplary embodiments can have different values. It should be noted that similar reference numbers and letters represent similar items in the following drawings, so further discussion is not needed in subsequent drawings once an item is defined in one drawing.

[0111] In the description of the present application, it should be understood that the orientation words such as "front, back, up, down, left, right", "transverse, vertical, perpendicular, horizontal" and "top, bottom" and the like indicate the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present application and simplifying the description, and does not indicate and imply that the indicated device or element must have a particular orientation or be constructed and operated in a particular orientation, unless otherwise stated, and therefore cannot be understood as a limitation on the scope of protection of the present application; the orientation words "inner, outer" refer to the inner and outer of the contour of the parts themselves.

[0112] For purposes of the description hereinafter, the terms "upper", "lower", "right", "left", "rear", "front", "vertical", "horizontal", and derivatives thereof shall relate to the application as oriented in the drawing figures. However, it is to be understood that the application can assume various alternative orientations and, accordingly, such terms are not to be taken as limitations of the present application.

[0113] In addition, it should be noted that the use of "first", "second", etc. words to describe various components is only intended to distinguish a certain one to another, and the words have no special meaning, and therefore cannot be understood as a limitation on the scope of protection of the present application.

[0114] The above only describes the preferred embodiments of the present application and is not intended to limit the present application. Those skilled in the art can make various modifications and changes to the present application. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the scope of protection of the present application.

Claims

1. A clamping assembly, characterized in that, The clamping assembly comprises: a clamping member; an abutting member mounted on the clamping member and movable relative to the clamping member under force; wherein the clamping member is adapted to abut the UAV through the abutting member along the movement direction of the abutting member.

2. The clamp assembly of claim 1, wherein, The clamping member has a first accommodating cavity, and at least a part of the abutting member is movably mounted in the first accommodating cavity.

3. The clamp assembly of claim 2, wherein, The clamping assembly further comprises an elastic member adapted to elastically connect the abutting member and the cavity wall of the first accommodating cavity.

4. The clamp assembly of claim 1, wherein, The clamping assembly further comprises a first buffer member arranged on the abutting member, and the abutting member is adapted to abut the UAV through the first buffer member.

5. The clamp assembly of claim 4, wherein, The clamping assembly further comprises a first limiting structure between the clamping member and the first buffer member to limit the movement position of the abutting member.

6. The clamp assembly of claim 5, wherein, The end of the clamping member close to the first buffer member is provided with a first step structure, the end of the first buffer member close to the abutting member is provided with a second step structure, and the first step structure and the second step structure cooperate to form the first limiting structure.

7. The clamp assembly of claim 1, wherein, The clamping assembly further comprises a limiting member arranged on the abutting member, and the limiting member is used to abut the clamping member to limit the position of the abutting member.

8. The clamp assembly of claim 1, wherein, The clamping assembly further comprises a positioning member arranged on the clamping member, and the positioning member is used to abut the UAV to position the position of the UAV.

9. The clamp assembly of claim 1, wherein, The clamping assembly further comprises a second buffer member configured to abut an external component to limit the position of the clamping member.

10. The clamp assembly of claim 1, wherein, The clamping assembly further comprises a UAV charging port and a wire harness, and the wire harness is adapted to connect the UAV charging port.

11. The clamp assembly of claim 10, wherein, The wire harness comprises: a protective shell; a connecting wire arranged in the protective shell, and the protective shell is used to limit the displacement of the connecting wire.

12. The clamp assembly of claim 11, wherein, The protective shell comprises sequentially connected: a first section; a plurality of second sections; a third section, the end of the third section away from the first section is connected with the clamping member, and the end of the first section away from the third section is adapted to be connected with the edge of the base; wherein, adjacent two second sections are relatively rotatable connected, the other end of the first section is rotatably connected with the second section close to the first section, and the other end of the third section is rotatably connected with the second section close to the third section.

13. The clamp assembly of claim 12, wherein, The length of the third section is greater than the length of each second section.

14. The clamp assembly of claim 1, wherein, The clamping assembly further comprises: a guide rail, and the clamping member is movably arranged on the guide rail; a bushing arranged on the clamping member, and the clamping member is adapted to be movably arranged on the guide rail, and the bushing is adapted to be arranged between the guide rail and the clamping member.

15. A clamping mechanism, characterized by The clamping assembly comprises any one of claims 1-14.

16. The clamping mechanism of claim 15, wherein, The clamping mechanism further comprises: a driving member; a transmission assembly, and the driving member drives the clamping member of the clamping assembly to move through the transmission assembly.

17. The clamping mechanism of claim 16, wherein, The transmission assembly comprises: a first transmission member; A second transmission member, the driving member being connected to the clamping member through the first transmission member and the second transmission member; wherein the driving member is configured to drive the first transmission member to rotate, and the second transmission member is configured to drive the clamping member to move under the driving of the rotation of the first transmission member.

18. The clamping mechanism of claim 17, wherein, The first transmission member is threadedly connected to the second transmission member.

19. The clamping mechanism of claim 18, wherein, The first transmission member is one of a screw rod and a nut, and the second transmission member is the other of the screw rod and the nut.

20. The clamping mechanism of claim 18, wherein, The first transmission member has a double-end screw thread.

21. The clamping mechanism of claim 17, wherein, The clamping mechanism includes two clamping assemblies, the two clamping assemblies are opposite in movement direction, and the two clamping assemblies are configured to clamp a UAV.

22. The clamping mechanism of claim 21, wherein, The first transmission member includes two first transmission parts, the second transmission member includes two second transmission parts, and the driving member is connected to the corresponding clamping member through the corresponding first transmission part and the corresponding second transmission part; wherein the driving member is configured to drive the first transmission part to rotate, and the second transmission part is adapted to drive the clamping member to move under the driving of the rotation of the first transmission part.

23. The clamping mechanism of claim 22, wherein, The two first transmission parts are opposite in thread direction.

24. The clamping mechanism of claim 22, wherein, The two first transmission parts are fixedly connected.

25. The clamping mechanism of claim 22, wherein, The two first transmission parts are fixedly connected through a shaft sleeve.

26. The clamping mechanism of claim 25, wherein, The clamping mechanism further includes a base, the base is provided with a fixing seat, the fixing seat includes a through-hole part, and the through-hole part is provided with a through hole; wherein the first transmission member is rotatably installed in the through hole.

27. The clamping mechanism of claim 26, wherein, The first transmission member is in interference fit with the through hole.

28. The clamping mechanism of claim 26, wherein, The outer peripheral wall of the through-hole part is provided with a reinforcing structure.

29. The clamping mechanism of claim 27, wherein, The inner side wall of the through-hole part is provided with a protruding part, and the protruding part is configured to abut against the outer peripheral wall of the first transmission member.

30. The clamping mechanism of claim 27, wherein, The fixing seat is provided with at least one hollow part, and the at least one hollow part surrounds the through-hole part.

31. The clamping mechanism of claim 26, wherein, The fixing seat includes at least a first fixing seat and a second fixing seat; the first fixing seat is arranged at the fixed connection position of the two first transmission parts, and the shaft sleeve is rotatably installed in the through hole of the first fixing seat; and the second fixing seat is arranged at the end part of the two first transmission parts away from the fixed connection position.

32. The clamping mechanism of claim 31, wherein, The clamping mechanism further includes: A guide rail, the clamping member is arranged on the guide rail, and the driving member drives the clamping member to move along the guide rail through the first transmission member and the second transmission member; The first fixing seat is further provided with a guide rail mounting hole, and the guide rail passes through the guide rail mounting hole.

33. The clamping mechanism of claim 17, wherein, The clamping mechanism further includes a damping pad, the damping pad is arranged around the outer periphery of the second transmission member and is in interference fit with the second transmission member.

34. A drone nacelle, characterized in that The clamping assembly as claimed in any one of claims 1-14, or the clamping mechanism as claimed in any one of claims 15-33.

35. A vehicle characterized by The UAV cabin as claimed in claim 34.

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