Connector assembly and unmanned aerial vehicle

CN224625977UActive Publication Date: 2026-08-11SHENZHEN HOBBYWING TECH CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-07-01
Publication Date
2026-08-11

AI Technical Summary

Technical Problem

当无人机在飞行的过程中产生高频震动并传递至连接器时,易使连接器震动或晃动,导致连接器与线缆的连接处松动、脱落或断裂等,造成无人机的失控,引发安全隐患

Benefits of technology

[0015]The beneficial effects of this utility model embodiment are as follows: Unlike existing technologies, this utility model embodiment provides a connector assembly, including a base, a snap-fit ​​component, a fastener, and a connector. The base supports the drone body; the snap-fit ​​component has a snap-fit ​​portion; the fastener passes through the snap-fit ​​component and connects to the base, fixing the snap-fit ​​component to the base; the connector snaps into the snap-fit ​​portion, and the connector is used for electrical connection with the drone body. Through the above method, the connector in this utility model embodiment can not only be indirectly fixed to the base through the snap-fit ​​component and fastener, improving the connector's stability and reducing vibration caused by high-frequency vibration during flight, thus reducing the probability of loosening at the connection between the connector and the cable, reducing the probability of drone loss of control, and reducing the probability of safety hazards, but also form a detachable connection through the snap-fit ​​component and fastener, enabling quick assembly and disassembly of the connector, which is helpful for connector maintenance and replacement.

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Abstract

This utility model discloses a connector assembly and a drone. The connector assembly includes a base, a snap-fit ​​component, a fastener, and a connector. The base supports the drone body. The snap-fit ​​component has a snap-fit ​​portion. The fastener passes through the snap-fit ​​component and connects to the base, fixing the snap-fit ​​component to the base. The connector snaps into the snap-fit ​​portion and is used for electrical connection with the drone body. Through this method, the connector in this utility model embodiment can not only be indirectly fixed to the base through the snap-fit ​​component and fastener, improving the connector's stability and reducing vibration caused by high-frequency vibration during flight, thus reducing the probability of loosening at the connection between the connector and the cable, reducing the probability of drone loss of control, and reducing the probability of safety hazards, but also form a detachable connection through the snap-fit ​​component and fastener, enabling quick assembly and disassembly of the connector, which is helpful for connector maintenance and replacement.
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Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a connector assembly and a UAV. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are aircraft that perform flight missions through wireless remote control or autonomous control systems and are widely used in fields such as aerial photography, surveying, logistics, and plant protection.

[0003] Currently, during drone use, the drone's base generally lacks a support structure to support the connector, leaving the connector suspended in mid-air. When the drone generates high-frequency vibrations during flight and these vibrations are transmitted to the connector, the connector is prone to vibration or shaking, leading to loosening, detachment, or breakage of the connection between the connector and the cable. This can cause the drone to lose control and create safety hazards. Utility Model Content

[0004] The present invention aims to provide a connector assembly and a drone that can reduce the probability of connector vibration or shaking.

[0005] To solve the above-mentioned technical problems, one technical solution adopted in this utility model embodiment is: to provide a connector assembly, including a base, a snap-fit ​​component, a fastener, and a connector; the base is used to support the main body of a drone; the snap-fit ​​component is provided with a snap-fit ​​portion; the fastener passes through the snap-fit ​​component and is connected to the base, the fastener fixing the snap-fit ​​component to the base; the connector snaps into the snap-fit ​​portion, and the connector is used for electrical connection with the main body of the drone.

[0006] Optionally, the latching portion includes a first latching portion and a second latching portion, the first latching portion and the second latching portion being set at a preset angle; the connector includes a first connector and a second connector, the first connector being latched with the first latching portion, and the second connector being latched with the second latching portion.

[0007] Optionally, the latching portion is provided with a first latch claw, the first latch claw is arc-shaped, the claw opening of the first latch claw faces the base, the first connector is latched onto the first latch claw, and the first latch claw constitutes the first latching portion.

[0008] Optionally, the latching part is provided with a second latch, the second latch is arc-shaped, the jaw of the second latch is set at a preset angle with the jaw of the first latch, the second connector is latched onto the second latch, and the second latch constitutes the second latching part.

[0009] Optionally, the connector assembly further includes a first anti-slip member disposed between the first latching portion and the first connector, the first anti-slip member being sleeved on the first connector, and the first anti-slip member being latched on the first latching portion; and / or, the connector assembly further includes a second anti-slip member disposed between the second latching portion and the second connector, the second anti-slip member being sleeved on the second connector, and the second anti-slip member being latched on the second latching portion.

[0010] Optionally, the connector assembly further includes a third anti-slip element that at least partially covers the surfaces of the first and second latching portions, and both the first and second connectors are at least partially in contact with the third anti-slip element.

[0011] Optionally, the base is provided with an extension, and the fastener passes through the snap-fit ​​member and is connected to the extension, thereby fixing the snap-fit ​​member to the extension.

[0012] Optionally, along a first direction, the projection of the extension overlaps with the projection of the first snap-fit ​​portion, and the projection of the extension is offset from the projection of the second snap-fit ​​portion, wherein the first direction is the height direction of the base.

[0013] Optionally, the base has a screw hole in the extension; the snap-fit ​​member has a connecting portion and a through hole in the connecting portion, the through hole being aligned with the screw hole; the fastener has a screwed portion and a tightening portion, the screwed portion passing through the through hole and screwed into the screw hole, and the tightening portion abutting against the side of the snap-fit ​​member opposite to the base.

[0014] To solve the above-mentioned technical problems, another technical solution adopted in this utility model embodiment is: to provide a drone, including a drone body and the above-mentioned connector assembly, wherein the drone body is connected to the base of the connector assembly, and the drone body is electrically connected to the connector of the connector assembly.

[0015] The beneficial effects of this utility model embodiment are as follows: Unlike existing technologies, this utility model embodiment provides a connector assembly, including a base, a snap-fit ​​component, a fastener, and a connector. The base supports the drone body; the snap-fit ​​component has a snap-fit ​​portion; the fastener passes through the snap-fit ​​component and connects to the base, fixing the snap-fit ​​component to the base; the connector snaps into the snap-fit ​​portion, and the connector is used for electrical connection with the drone body. Through the above method, the connector in this utility model embodiment can not only be indirectly fixed to the base through the snap-fit ​​component and fastener, improving the connector's stability and reducing vibration caused by high-frequency vibration during flight, thus reducing the probability of loosening at the connection between the connector and the cable, reducing the probability of drone loss of control, and reducing the probability of safety hazards, but also form a detachable connection through the snap-fit ​​component and fastener, enabling quick assembly and disassembly of the connector, which is helpful for connector maintenance and replacement. Attached Figure Description

[0016] To more clearly illustrate the technical solutions in the specific embodiments of this utility model or the prior art, the drawings used in the description of the specific embodiments or the prior art will be briefly introduced below. In all the drawings, similar elements or parts are generally identified by similar reference numerals. In the drawings, the elements or parts are not necessarily drawn to actual scale.

[0017] Figure 1 This is a schematic diagram of the overall structure of the connector assembly provided in this embodiment of the utility model;

[0018] Figure 2 This is an exploded view of the overall structure of the connector assembly provided in this embodiment of the utility model;

[0019] Figure 3 This is a schematic diagram of the structure of the base of the connector assembly provided in this embodiment of the present invention;

[0020] Figure 4 This is a schematic diagram of the snap-fit ​​component of the connector assembly provided in this embodiment of the utility model. Figure 1 ;

[0021] Figure 5 This is a schematic diagram of the snap-fit ​​component of the connector assembly provided in this embodiment of the utility model. Figure 2 ;

[0022] Figure 6 This is a schematic diagram of the structure of the first and second anti-slip components of the connector assembly provided in this embodiment of the utility model. Figure 1 ;

[0023] Figure 7 This is a schematic diagram of the structure of the first and second anti-slip components of the connector assembly provided in this embodiment of the utility model. Figure 2 ;

[0024] Figure 8 This is a schematic diagram of the structure of the third anti-slip component of the connector assembly provided in this embodiment of the utility model. Figure 1 ;

[0025] Figure 9 This is a schematic diagram of the structure of the third anti-slip component of the connector assembly provided in this embodiment of the utility model. Figure 2 .

[0026] Explanation of reference numerals in the attached figures:

[0027] 1. Base, 11. Main body, 12. Pipe clamp, 121. First pipe clamp, 122. Second pipe clamp, 13. Extension, 14. Mounting hole, 15. Through hole, 16. First opening, 17. Second opening, 18. Screw hole;

[0028] 2. Snap-fit ​​component, 21. Snap-fit ​​part, 211. First snap-fit ​​part, 212. Second snap-fit ​​part, 213. First claw, 214. Second claw, 22. Connecting part, 23. Through hole;

[0029] 3 Fasteners, 31 Screw connections, 32 Tightening connections;

[0030] 4 connectors, 41 first connector, 42 second connector;

[0031] 5. First anti-slip component;

[0032] 6. Second anti-slip component;

[0033] 7. Third anti-slip component;

[0034] 100 connector assembly. Detailed Implementation

[0035] To facilitate understanding of this utility model, a more detailed description is provided below with reference to the accompanying drawings and specific embodiments. It should be noted that when an element is described as "fixed to" another element, it can be directly on the other element, or one or more intermediate elements may exist between them. When an element is described as "connected" to another element, it can be directly connected to the other element, or one or more intermediate elements may exist between them. The terms "upper," "lower," "inner," "outer," "vertical," "horizontal," etc., used in this specification indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are used only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. Furthermore, the terms "first," "second," etc., are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0036] Unless otherwise defined, all technical and scientific terms used in this specification have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains. The terminology used in this specification is for the purpose of describing particular embodiments only and is not intended to limit the scope of the invention. The term "and / or" as used in this specification includes any and all combinations of one or more of the associated listed items.

[0037] Unmanned aerial vehicles (UAVs) are aircraft that perform flight missions through wireless remote control or autonomous control systems and are widely used in fields such as aerial photography, surveying, logistics, and plant protection.

[0038] Currently, during drone use, the drone's base generally lacks a support structure to support the connector, leaving the connector suspended in mid-air. When the drone generates high-frequency vibrations during flight and these vibrations are transmitted to the connector, the connector is prone to vibration or shaking, leading to loosening, detachment, or breakage of the connection between the connector and the cable. This can cause the drone to lose control and create safety hazards.

[0039] In view of this, the present invention provides an embodiment of connector 4 assembly 100, which can not only support the main body of the drone, but also reduce the probability of loosening at the connection between connector 4 and cable.

[0040] To facilitate the reader's understanding of the concept of this utility model embodiment, the specific structure of the connector 4 component 100 is described below:

[0041] Please see Figures 1 to 3 The connector 4 assembly 100 includes a base 1, a snap-fit ​​2, a fastener 3, and a connector 4; the base 1 is used to support the main body of the drone; the snap-fit ​​2 is provided with a snap-fit ​​part 21; the fastener 3 passes through the snap-fit ​​2 and is connected to the base 1, and the fastener 3 fixes the snap-fit ​​2 to the base 1; the connector 4 snaps into the snap-fit ​​part 21, and the connector 4 is used for electrical connection with the main body of the drone.

[0042] In the above manner, the snap-fit ​​2 and fastener 3 in this embodiment of the present invention form a support structure for supporting the connector 4, so that the connector 4 can not only be indirectly fixed to the base 1 through the snap-fit ​​2 and fastener 3, thereby improving the stability of the connector 4, reducing the shaking of the connector 4 due to high-frequency vibration during flight, reducing the probability of loosening at the connection between the connector 4 and the cable, reducing the probability of the drone going out of control, and reducing the probability of causing safety hazards, but also form a detachable connection through the snap-fit ​​2 and fastener 3, enabling quick assembly and disassembly of the connector 4, which is helpful for the maintenance and replacement of the connector 4.

[0043] Regarding the base 1 described above, please refer to some embodiments. Figures 1 to 3The base 1 is a pipe clamp seat. The base 1 is provided with a main body 11, a pipe clamp 12 and an extension 13. The main body 11, the pipe clamp 12 and the extension 13 are integrally formed. The pipe clamp 12 is located below the main body 11 and the extension 13 is located on the side of the main body 11. The main body 11 is used to support the main body of the UAV. The pipe clamp 12 is used to clamp the components of the UAV (e.g., arms, frames, sensor brackets, plant protection spray pipes or plant protection nozzles, etc.). The extension 13 is used for connecting the card connector 2 and the fastener 3.

[0044] Furthermore, in some embodiments, please refer to Figure 3 The base 1 has a plurality of mounting holes 14 on the main body 11. The mounting holes 14 are arranged in an array and extend from the top to the bottom of the main body 11. The mounting holes 14 are all stepped. The mounting holes 14 are used for screws to pass through and screw into the drone body so that the drone body is fixed to the main body 11. The cross-section of the clamp part 12 is arc-shaped. The cross-section here refers to the cross-section of the clamp part 12 along the length direction. The base 1 has a plurality of through holes 15 on the clamp part 12. The through holes 15 are used to release the air pressure between the clamp part 12 and the drone's rod when the clamp part 12 clamps the drone's rod. The through holes 15 are used to allow the drone's rod to be exposed to air for heat dissipation when the clamp part 12 clamps the drone's rod. The through holes 15 are also used to reduce the weight of the base 1 to achieve the purpose of weight reduction.

[0045] Furthermore, in some embodiments, please refer to Figure 3 The clamping part 12 includes a first clamp 121 and a second clamp 122, which are arranged opposite to each other. A gap is formed between the first clamp 121 and the second clamp 122 on the side away from the main body 11. The clamping part 12 has a through first opening 16 in the first clamp 121 and a through second opening 17 in the second clamp 122. Both the first opening 16 and the second opening 17 are stepped and aligned. The first opening 16 is used for a screw to pass through and extend to the second opening 17. The second opening 17 is used to receive a nut so that the nut and the screw are screwed together and fixed, thereby eliminating the gap between the first clamp 121 and the second clamp 122 and realizing clamping.

[0046] In some embodiments, the snap-fit ​​component 2 is made of plastic, metal, or alloy. For example, in some embodiments, the snap-fit ​​component 2 is made of aluminum alloy, copper alloy, or nickel alloy, etc.

[0047] Regarding the aforementioned card connector 2, in some embodiments, please refer to... Figure 1 and Figure 2The latching portion 21 includes a first latching portion 211 and a second latching portion 212, which are arranged at a preset angle. The connector 4 includes a first connector 41 and a second connector 42, with the first connector 41 latching with the first latching portion 211 and the second connector 42 latching with the second latching portion 212. In this manner, the first latching portion 211 and the second latching portion 212 can expand the latching function of the latching portion 21, allowing it to adapt to latching connectors 4 with different shapes and structures. Furthermore, by arranging the first latching portion 211 and the second latching portion 212 at a preset angle, the first latching portion 211 and the second latching portion 212 can be oriented in different positions, reducing the probability of interference between the first connector 41 and the second connector 42.

[0048] It should be noted that, please refer to [link / reference needed]. Figure 1 and Figure 2 The included angle between the first latching portion 211 and the second latching portion 212 is greater than or equal to zero degrees and less than or equal to 180 degrees. It should also be noted that, as a more preferred option, the included angle between the first latching portion 211 and the second latching portion 212 is greater than or equal to ninety degrees and less than or equal to 180 degrees. For example, in some embodiments, please refer to... Figure 4 The preset included angle between the first latching portion and the second latching portion is zero degrees, meaning the first latching portion and the second latching portion are arranged in parallel; or, in other embodiments, please refer to... Figure 5 The preset included angle between the first snap-fit ​​part and the second snap-fit ​​part is 90 degrees, that is, the first snap-fit ​​part and the second snap-fit ​​part are perpendicular.

[0049] Furthermore, in some embodiments, please refer to Figure 5 The snap-fit ​​part 21 is provided with a first snap-fit ​​claw 213. The first snap-fit ​​claw 213 is arc-shaped and the claw opening of the first snap-fit ​​claw 213 faces the base 1. The first connector 41 snaps into the first snap-fit ​​claw 213, and the first snap-fit ​​claw 213 constitutes the first snap-fit ​​part 211.

[0050] Furthermore, in some embodiments, please refer to Figure 5 The latching part 21 is provided with a second latch 214. The second latch 214 is arc-shaped. The jaw of the second latch 214 is set at a preset angle with the jaw of the first latch 213. The second connector 42 is latched onto the second latch 214. The second latch 214 constitutes the second latching part 212.

[0051] For the fastener 3 described above, please refer to some embodiments. Figures 1 to 3 The fastener 3 passes through the snap-fit ​​2 and is connected to the extension 13, thus fixing the snap-fit ​​2 to the extension 13.

[0052] Furthermore, in some embodiments, please refer to Figures 1 to 3Along the first direction, the projection of the extension 13 overlaps with the projection of the first latching portion 211, meaning the first latching portion 211 is located directly below the extension 13. The projection of the extension 13 is offset from the projection of the second latching portion 212, meaning the second latching portion 212 is located obliquely below the extension 13 away from the base 1. The first direction is the height direction of the base 1. This optimizes the positions of the first latching portion 211 and the second latching portion 212, reducing the probability of interference between the first connector 41 and the second connector 42. Furthermore, by having the projection of the extension 13 overlap with the projection of the first latching portion 211 and the projection of the extension 13 offset from the projection of the second latching portion 212, the latching member 2 can at least partially overlap with the base 1 along the first direction, improving the structural compactness of the connector 4 assembly 100 and helping to reduce the overall volume of the connector 4 assembly 100.

[0053] Furthermore, in some embodiments, please refer to Figures 1 to 3 The base 1 has a screw hole 18 in the extension 13; the snap-fit ​​part 2 has a connecting part 22, and a through hole 23 in the connecting part 22, which is aligned with the screw hole 18; the fastener 3 has a screwing part 31 and a tightening part 32, the screwing part 31 passes through the through hole 23 and is screwed into the screw hole 18, and the tightening part 32 abuts against the side of the snap-fit ​​part 2 away from the base 1. In this way, the snap-fit ​​part 2 is detachably connected to the base 1 by the fastener 3, which facilitates the maintenance and replacement of the snap-fit ​​part 2.

[0054] Regarding the connector 4 component 100 described above, in some embodiments, please refer to... Figure 6 and Figure 7 The connector 4 assembly 100 further includes a first anti-slip member 5, which is disposed between the first latching portion 211 and the first connector 41. The first anti-slip member 5 is annularly arranged and sleeved on the first connector 41, and latched onto the first latching portion 211. And / or, the connector 4 assembly 100 further includes a second anti-slip member 3, which is disposed between the second latching portion 212 and the second connector 42. The second anti-slip member 3 is annularly arranged and sleeved on the second connector 42, and latched onto the second latching portion 212. Through the above methods, the sliding friction between the first latching portion 211 and the first connector 41, and / or the sliding friction between the second latching portion 212 and the second connector 42, can be increased, thereby reducing the probability of slippage of the first connector 41 and / or the second connector 42, and thus improving the latching stability of the first connector 41 and / or the second connector 42.

[0055] For the connector 4-component 100 described above, please refer to other embodiments. Figure 8 and Figure 9The connector 4 assembly 100 also includes a third anti-slip element 7, which at least partially covers the surfaces of the first latching portion 211 and the second latching portion 212. Both the first connector 41 and the second connector 42 are at least partially in contact with the third anti-slip element 7. In this manner, the third anti-slip element 7 covers the first latching portion 211 and the second latching portion 212, which not only increases the sliding friction between the first latching portion 211 and the first connector 41, and also increases the sliding friction between the second latching portion 212 and the second connector 42, but also reduces the intrusion of dust or debris between the first latching portion 211 and the first connector 41, and between the second latching portion 212 and the second connector 42, thereby improving the reliability of the anti-slip mechanism.

[0056] Furthermore, in some embodiments, the first anti-slip component 5, the second anti-slip component 6, and the third anti-slip component 7 are all made of silicone.

[0057] This utility model embodiment provides a connector 4 assembly 100, including a base 1, a snap-fit ​​component 2, a fastener 3, and a connector 4. The base 1 supports the main body of a drone. The snap-fit ​​component 2 is provided with a snap-fit ​​portion 21. The fastener 3 passes through the snap-fit ​​component 2 and is connected to the base 1, fixing the snap-fit ​​component 2 to the base 1. The connector 4 snaps into the snap-fit ​​portion 21 and is used for electrical connection with the main body of the drone. Through the above method, the connector 4 in this utility model embodiment can not only be indirectly fixed to the base 1 through the snap-fit ​​component 2 and the fastener 3, improving the stability of the connector 4, reducing the shaking of the connector 4 due to high-frequency vibration during flight, reducing the probability of loosening at the connection between the connector 4 and the cable, reducing the probability of drone loss of control, and reducing the probability of causing safety hazards, but also form a detachable connection through the snap-fit ​​component 2 and the fastener 3, enabling quick assembly and disassembly of the connector 4, which is helpful for the maintenance and replacement of the connector 4.

[0058] This utility model also provides an embodiment of a drone, which includes a drone body and the aforementioned connector 4 assembly 100. The drone body is connected to the base 1 of the connector 4 assembly 100, and the drone body is electrically connected to the connector 4 of the connector 4 assembly 100. The specific structure and function of the connector 4 assembly 100 can be found in the above embodiments, and will not be repeated here.

[0059] The above description is merely an embodiment of this utility model and does not limit the patent scope of this utility model. Any equivalent structural or procedural transformations made based on the description and drawings of this utility model, or direct or indirect applications in other related technical fields, are similarly included within the patent protection scope of this utility model.

Claims

1. A connector assembly, characterized in that, include: The base is used to support the main body of the drone; A snap-fit ​​connector, wherein the snap-fit ​​connector is provided with a snap-fit ​​portion; A fastener, which passes through the snap-fit ​​member and is connected to the base, thereby fixing the snap-fit ​​member to the base; A connector that engages with the snap-fit ​​part, the connector being used for electrical connection with the main body of the drone.

2. The connector assembly according to claim 1, characterized in that, The latching part includes a first latching part and a second latching part, and the first latching part and the second latching part are arranged at a preset angle. The connector includes a first connector and a second connector, wherein the first connector engages with the first snap-fit ​​portion, and the second connector engages with the second snap-fit ​​portion.

3. The connector assembly according to claim 2, characterized in that, The latching part is provided with a first latch claw, which is arc-shaped and has its claw opening facing the base. The first connector is latched onto the first latch claw, and the first latch claw constitutes the first latching part.

4. The connector assembly according to claim 3, characterized in that, The latching part is provided with a second latch, which is arc-shaped. The opening of the second latch is at a preset angle to the opening of the first latch. The second connector is latched onto the second latch, and the second latch constitutes the second latching part.

5. The connector assembly according to claim 2, characterized in that, The connector assembly further includes a first anti-slip member, which is disposed between the first snap-fit ​​portion and the first connector. The first anti-slip member is sleeved on the first connector and snap-fitted onto the first snap-fit ​​portion. And / or, The connector assembly further includes a second anti-slip member, which is disposed between the second snap-fit ​​portion and the second connector. The second anti-slip member is sleeved on the second connector and snap-fitted onto the second snap-fit ​​portion.

6. The connector assembly according to claim 2, characterized in that, The connector assembly further includes a third anti-slip element, which at least partially covers the surfaces of the first and second latching portions, and both the first and second connectors are at least partially in contact with the third anti-slip element.

7. The connector assembly according to claim 6, characterized in that, The base is provided with an extension, and the fastener passes through the snap-fit ​​member and is connected to the extension, thereby fixing the snap-fit ​​member to the extension.

8. The connector assembly according to claim 7, characterized in that, Along the first direction, the projection of the extension overlaps with the projection of the first snap-fit ​​portion, and the projection of the extension is offset from the projection of the second snap-fit ​​portion. The first direction is the height direction of the base.

9. The connector assembly according to claim 7, characterized in that, The base is provided with a screw hole in the extension portion; The snap-fit ​​component is provided with a connecting portion, and the snap-fit ​​component is provided with a through hole in the connecting portion, and the through hole is aligned with the screw hole; The fastener is provided with a threaded part and a screwing part. The threaded part passes through the through hole and is threaded into the threaded hole. The screwing part abuts against the side of the snap-fit ​​member away from the base.

10. A drone, characterized in that, It includes a drone body and a connector assembly as described in any one of claims 1-9, wherein the drone body is connected to the base of the connector assembly and the drone body is electrically connected to the connector of the connector assembly.