Unmanned aerial vehicle suspension damping support and unmanned aerial vehicle
By designing a drone suspension shock absorbing bracket containing multiple first shock absorbing balls, the problem of poor shock absorption effect in the prior art is solved, effective shock absorption in the vertical direction is achieved, and external load is protected.
Patent Information
- Application Number
- CN202422126550.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-29
- Publication Date
- 2025-05-27
- Estimated Expiration
- 2034-08-29
AI Technical Summary
The shock absorption effect of existing drone shock absorbers is poor, resulting in the external load still being affected by high-frequency vibration during flight.
A drone suspension shock absorbing bracket is designed, including an upper bracket, a lower bracket and a first shock absorbing assembly. The first shock absorbing assembly is composed of a plurality of first shock absorbing balls, and the central axis of the first shock absorbing ball is perpendicular to the plane where the upper bracket is located, so that the gravity of the external load can stretch the first shock absorbing ball along the central axis.
By stretching the first shock absorbing ball, effective shock filtering in the vertical direction is achieved, the shock absorption effect is improved, and effective shock absorption protection is provided for external loads.
Smart Images
Figure CN222905878U_ABST
Abstract
Description
Technical Field
[0001] This application relates to the technical field of unmanned flight devices, and more particularly, to a shock-absorbing suspension bracket for an unmanned aerial vehicle and an unmanned aerial vehicle. Background Technique
[0002] An unmanned aerial vehicle (UAV) is short for an unpiloted aircraft, which is an aircraft without a pilot using radio remote control equipment and self-contained program control devices. Currently, UAVs have been widely used in fields such as aerial photography, agricultural protection, police security, logistics transportation, and military. As a flight platform, a UAV usually needs to carry external devices to achieve corresponding functions. Since high-frequency vibrations during flight will affect the external devices, shock-absorbing brackets are usually set up to filter high-frequency vibrations. However, the shock-absorbing brackets provided by the current prior art have poor shock-absorbing effects, resulting in the external load still being affected by high-frequency vibrations. Summary of the Utility Model
[0003] The purpose of this application is to provide a shock-absorbing suspension bracket for an unmanned aerial vehicle and an unmanned aerial vehicle, which can effectively filter vibrations in the vertical direction and improve the shock-absorbing ability of the shock-absorbing bracket.
[0004] The embodiments of this application are implemented as follows:
[0005] In a first aspect, an embodiment of this application provides a shock-absorbing suspension bracket for an unmanned aerial vehicle, including an upper bracket, a lower bracket, and a first shock-absorbing component; the plane where the upper bracket is located is parallel to the plane where the lower bracket is located, and the first shock-absorbing component is arranged between the upper bracket and the lower bracket; the first shock-absorbing component includes a plurality of first shock-absorbing balls arranged at intervals in a plane, one side of the first shock-absorbing ball is connected to the upper bracket, and the other side is connected to the lower bracket; the side of the lower bracket facing away from the upper bracket is a mounting surface for mounting an external load; the central axis of the first shock-absorbing ball is perpendicular to the plane where the upper bracket is located, so that the gravity generated by the external load can stretch the first shock-absorbing ball along the central axis.
[0006] As an optional implementation manner, a quick-release connection structure for mounting an external load is arranged on the mounting surface, and the connection point between the quick-release connection structure and the lower bracket is located within the area surrounded by the first shock-absorbing balls.
[0007] As an optional implementation manner, a clamping groove with an extending direction parallel to the plane where the upper bracket is located is arranged on the quick-release connection structure, and the external load has a clamping protrusion that cooperates with the clamping groove for connection.
[0008] As an alternative embodiment, a plurality of first extension arms are provided on the upper bracket, one end of the first extension arm is connected to the upper bracket and the other end extends away from the upper bracket; a second extension arm is provided on the lower bracket, and the second extension arm is parallel to the extension direction of the first extension arm; a second shock absorption assembly is provided between the first extension arm and the second extension arm.
[0009] As an alternative embodiment, the second shock absorption assembly includes a plurality of second shock absorption balls arranged at intervals around the outer periphery of the upper bracket; the central axis of the second shock absorption ball intersects with the central axis of the first shock absorption ball.
[0010] As an alternative embodiment, the first extension arm and the second extension arm are bent toward the side close to the external load, and a preset angle is formed between the extension direction of the first extension arm and the plane where the upper bracket is located; the central axis of the second shock absorption ball is perpendicular to the first extension arm.
[0011] As an alternative embodiment, the upper bracket and the lower bracket are rectangular frames with a weight reduction opening in the middle; the first extension arm and the second extension arm are respectively arranged at the four corners of the rectangular frame and extend away from the rectangular frame.
[0012] As an alternative embodiment, it further includes an adjustment knob and a traction member provided on the upper bracket; both ends of the traction member are respectively connected to the adjustment knob and the middle of the traction member is connected to the lower bracket, and the traction member can generate a force that makes the upper bracket and the lower bracket approach each other.
[0013] As an alternative embodiment, the traction member is a traction hanging rope, and the adjustment knob can adjust the extension length of the hanging rope between the upper bracket and the lower bracket by rotation.
[0014] In a second aspect, an embodiment of the present application provides a drone, including a drone body and a drone suspension shock absorption bracket provided below the drone body; an external load is installed on the lower bracket of the drone suspension shock absorption bracket.
[0015] The beneficial effects of the embodiments of the present application include:
[0016] An embodiment of the present application provides a drone suspension shock-absorbing bracket, which includes an upper bracket, a lower bracket, and a first shock-absorbing component; the plane where the upper bracket is located is parallel to the plane where the lower bracket is located, and the first shock-absorbing component is arranged between the upper bracket and the lower bracket; the first shock-absorbing component of the embodiment of the present application includes a plurality of first shock-absorbing balls arranged at intervals in a plane, one side of the first shock-absorbing ball is connected to the upper bracket, and the other side is connected to the lower bracket; the side of the lower bracket facing away from the upper bracket is a mounting surface for mounting an external load; the central axis of the first shock-absorbing ball of the embodiment of the present application is perpendicular to the plane where the upper bracket is located, so that the gravity generated by the external load can stretch the first shock-absorbing ball along the central axis. Therefore, the vibration energy generated during the flight of the drone needs to pass through the stretched first shock-absorbing ball and then be transmitted to the external load on the mounting surface. Since the first shock-absorbing ball can be stretched along the central axis, the first shock-absorbing ball can obtain a longer shock-absorbing stroke in the vertical direction, thus achieving an effective shock-absorbing effect and realizing an effective shock-absorbing protection function for the external load.
[0017] An embodiment of the present application provides a drone, which includes a drone body and a drone suspension shock-absorbing bracket arranged below the drone body; an external load is installed on the lower bracket of the drone suspension shock-absorbing bracket. The drone provided by the embodiment of the present application adopts the above-mentioned drone suspension shock-absorbing bracket and has good shock-absorbing performance. In addition, the drone suspension shock-absorbing bracket provided by the embodiment of the present application is light and simple, which is convenient for realizing the precise control of the drone. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings required in the embodiments. It should be understood that the following drawings only show some embodiments of the present application, and therefore should not be regarded as limiting the scope. For those of ordinary skill in the art, without creative efforts, other related drawings can also be obtained based on these drawings.
[0019] Figure 1 It is one of the structural schematic diagrams of the drone suspension shock-absorbing bracket according to the embodiment of the present application;
[0020] Figure 2 It is another structural schematic diagram of the drone suspension shock-absorbing bracket according to the embodiment of the present application;
[0021] Figure 3 It is the third structural schematic diagram of the drone suspension shock-absorbing bracket according to the embodiment of the present application.
[0022] ICON:
[0023] 100 - Upper support bracket; 101 - Lower support bracket; 102 - First shock absorption component; 103 - First shock absorption ball; 104 - Mounting surface; 105 - Quick-release connection structure; 106 - Clamping groove; 107 - First extension arm; 108 - Second extension arm; 109 - Second shock absorption component; 110 - Second shock absorption ball; 111 - Adjusting knob; 112 - Traction member. Detailed implementation manners
[0024] To make the objectives, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are some, but not all, of the embodiments of the present application. The components of the embodiments of the present application described and illustrated herein generally may be arranged and designed in a variety of different configurations.
[0025] Therefore, the following detailed description of the embodiments of the present application provided in the drawings is not intended to limit the scope of the claimed present application, but merely represents selected embodiments of the present application. All other embodiments obtained by those of ordinary skill in the art based on the embodiments in the present application without creative efforts shall fall within the scope of protection of the present application.
[0026] It should be noted that like reference numerals and letters denote like items in the following drawings. Therefore, once an item is defined in one drawing, it does not need to be further defined and explained in subsequent drawings. In addition, the terms "first", "second", "third", etc. are only used for descriptive distinction and cannot be construed as indicating or implying relative importance.
[0027] In the description of the present application, it should also be noted that unless otherwise clearly defined and limited, the terms "set", "installed", "connected", "connected" should be understood in a broad sense. For example, it may be a fixed connection, a detachable connection, or an integral connection; it may be a mechanical connection or an electrical connection; it may be directly connected or indirectly connected through an intermediate medium, and it may be the communication inside two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present application can be understood according to specific circumstances.
[0028] UAV is the abbreviation of unmanned aircraft, which is an unmanned aircraft that uses radio remote control equipment and self-contained program control devices. At present, UAVs have been widely used in aerial photography, agricultural value protection, police security, logistics and transportation, and military fields. As a flying platform, UAVs usually need to carry external devices to realize corresponding functions. Since high-frequency vibrations during flight will affect external devices, shock-absorbing brackets are usually set to filter high-frequency vibrations. The shock-absorbing brackets provided by the existing technology have poor shock-absorbing effect, resulting in the external load still being affected by high-frequency vibrations.
[0029] In order to solve the above technical problems, an embodiment of the present application provides a drone suspension shock absorbing bracket and a drone.
[0030] Reference Figure 1 , Figure 3 As shown, an embodiment of the present application provides a suspension shock-absorbing bracket for an unmanned aerial vehicle, comprising an upper bracket 100, a lower bracket 101 and a first shock-absorbing assembly 102; the plane where the upper bracket 100 is located is parallel to the plane where the lower bracket 101 is located, and the first shock-absorbing assembly 102 is arranged between the upper bracket 100 and the lower bracket 101; the first shock-absorbing assembly 102 includes a plurality of first shock-absorbing balls 103 arranged in a plane at intervals, one side of the first shock-absorbing ball 103 is connected to the upper bracket 100, and the other side is connected to the lower bracket 101; the side of the lower bracket 101 facing away from the upper bracket 100 is a mounting surface 104 for mounting an external load; the central axis of the first shock-absorbing ball 103 is perpendicular to the plane where the upper bracket 100 is located, so that the gravity generated by the external load can stretch the first shock-absorbing ball 103 along the central axis.
[0031] It should be noted that the upper bracket 100 and the lower bracket 101 provided in the embodiment of the present application both have a hollow structure, which can effectively reduce the weight of the upper bracket 100 and the lower bracket 101. This is conducive to realizing the lightweight design of the suspension shock-absorbing bracket of the drone and facilitating the precise control of the drone.
[0032] The upper bracket 100 and the lower bracket 101 of the embodiment of the present application are arranged in parallel, so that the first shock absorbing assembly 102 can be sandwiched between the upper bracket 100 and the lower bracket 101. The first shock absorbing assembly 102 of the present application can form a first shock absorbing surface which is parallel to the upper bracket 100 and the lower bracket 101.
[0033] It should be noted that the number of the first shock-absorbing balls 103 in the embodiment of the present application can be designed by those skilled in the art as required, and is not particularly limited thereto.
[0034] Reference Figure 1 , Figure 3As shown, preferably, the upper bracket 100 and the lower bracket 101 of the embodiment of the present application are rectangular frames, and first shock-absorbing balls 103 are respectively arranged at the four corners of the upper bracket 100 and the lower bracket 101. The middle part of the rectangular frame is hollowed out and has a relatively light weight. The arrangement of the four first shock-absorbing balls 103 can not only achieve a good shock-absorbing effect, but also avoid adding extra weight, so that the entire UAV suspension shock-absorbing bracket has a relatively light weight as a whole.
[0035] The embodiment of the present application provides a UAV suspension shock-absorbing bracket, which includes an upper bracket 100, a lower bracket 101 and a first shock-absorbing component 102; the plane where the upper bracket 100 is located is parallel to the plane where the lower bracket 101 is located, and the first shock-absorbing component 102 is arranged between the upper bracket 100 and the lower bracket 101; the first shock-absorbing component 102 of the embodiment of the present application includes a plurality of first shock-absorbing balls 103 arranged at intervals in a plane, one side of the first shock-absorbing ball 103 is connected to the upper bracket 100, and the other side is connected to the lower bracket 101; the side of the lower bracket 101 facing away from the upper bracket 100 is a mounting surface 104 for mounting an external load.
[0036] The central axis of the first shock-absorbing ball 103 of the embodiment of the present application is perpendicular to the plane where the upper bracket 100 is located, so that the gravity generated by the external load can stretch the first shock-absorbing ball 103 along the central axis. Therefore, the vibration energy generated by the UAV during flight needs to pass through the stretched first shock-absorbing ball 103 and then be transmitted to the external load on the mounting surface 104. Since the first shock-absorbing ball 103 can be stretched along the central axis, the first shock-absorbing ball 103 can obtain a longer shock-absorbing stroke in the vertical direction, so as to achieve an effective shock-absorbing effect and an effective shock-absorbing protection function for the external load.
[0037] Refer to Figure 1 As shown, as an optional implementation manner, a quick-release connection structure 105 for mounting an external load is arranged on the mounting surface 104, and the connection point of the quick-release connection structure 105 and the lower bracket 101 is located within the area surrounded by the first shock-absorbing balls 103.
[0038] Furthermore, in the embodiment of the present application, the mounting surface 104 is formed on the lower side surface of the lower bracket 101, and a plurality of connection points distributed at intervals are arranged on the mounting surface 104, and the quick-release connection structure 105 is fixedly connected to these connection points. Exemplarily, the quick-release connection structure 105 and the lower bracket 101 can be connected by bolts.
[0039] It should be noted that the connection points of the embodiment of the present application are all located inside the area surrounded by the first shock-absorbing balls 103, that is to say, the first shock-absorbing balls 103 are arranged at intervals in the circumferential direction around the quick-release connection structure 105. Through the above settings, edge shock absorption of the upper bracket 100 and the lower bracket 101 can be realized, which is beneficial to improving the shock-absorbing effect.
[0040] Refer to Figure 1 、Figure 2 As shown, as an alternative embodiment, the quick-release connection structure 105 is provided with a clamping groove 106 whose extending direction is parallel to the plane where the upper bracket 100 is located, and the external load has a clamping protrusion that cooperates with the clamping groove 106 for connection.
[0041] Furthermore, the external load of the embodiment of the present application is connected to the quick-release connection structure 105 through the clamping structure formed by the clamping groove 106 and the clamping protrusion, which is convenient for installation, disassembly and maintenance.
[0042] Refer to Figure 1 、 Figure 2 As shown, as an alternative embodiment, the upper bracket 100 is provided with a plurality of first extension arms 107. One end of the first extension arm 107 is connected to the upper bracket 100 and the other end extends away from the upper bracket 100; the lower bracket 101 is provided with a second extension arm 108, and the extending direction of the second extension arm 108 is parallel to that of the first extension arm 107; a second damping component 109 is provided between the first extension arm 107 and the second extension arm 108.
[0043] In the embodiment of the present application, the upper bracket 100 is provided with a plurality of first extension arms 107, and the lower bracket 101 is provided with a second extension arm 108. A second damping component 109 is clamped between the first extension arm 107 and the second extension arm 108.
[0044] Wherein, the second damping component 109 includes a plurality of second damping balls 110 arranged at intervals around the outer periphery of the upper bracket 100; the central axis of the second damping ball 110 intersects with the central axis of the first damping ball 103.
[0045] It should be noted that the first extension arm 107 and the second extension arm 108 are bent on the side close to the external load, and the extending direction of the first extension arm 107 has a preset angle with the plane where the upper bracket 100 is located; the central axis of the second damping ball 110 is perpendicular to the first extension arm 107.
[0046] Refer to Figure 3 As shown, exemplarily, the preset angle between the first extension arm 107 and the plane where the upper bracket 100 is located is 20°, or it can also be set to 30-40°. In this regard, those skilled in the art can set it according to needs.
[0047] It should be noted that the included angle between the central axis of the second shock-absorbing ball 110 and the central axis of the first shock-absorbing ball 103 is the same as the above-mentioned preset included angle. The first shock-absorbing ball 103 can achieve vertical shock-absorbing protection. The second shock-absorbing balls 110 are arranged at intervals around the outer periphery of the first shock-absorbing assembly 102 and are inclined, which is used to strengthen the lateral shock-absorbing function. Therefore, the second shock-absorbing balls 110 can achieve shock-absorbing protection in the circumferential direction, which is beneficial to preventing large lateral movement of the lower bracket 101 and external loads. In addition, it should be noted that the planes where the first shock-absorbing assembly 102 and the second shock-absorbing assembly 109 are located are parallel to each other and have a preset distance. Therefore, the support protection of the two shock-absorbing planes can be realized, and efficient shock filtering can be achieved.
[0048] Exemplarily, the upper bracket 100 and the lower bracket 101 are rectangular frames with weight-reducing openings in the middle; the first extension arm 107 and the second extension arm 108 are respectively arranged at the four corners of the rectangular frame and extend away from the rectangular frame.
[0049] Referring to Figure 2 As shown, as an optional implementation manner, it further includes an adjustment knob 111 and a traction member 112 provided on the upper bracket 100; both ends of the traction member 112 are respectively connected to the adjustment knob 111, and the middle of the traction member 112 is connected to the lower bracket 101. The traction member 112 can generate a force that makes the upper bracket 100 and the lower bracket 101 approach each other.
[0050] Among them, the traction member 112 is a traction hanging rope, and the adjustment knob 111 can adjust the extension length of the hanging rope between the upper bracket 100 and the lower bracket 101 by rotation.
[0051] In the embodiment of the present application, through the arrangement of the traction member 112, it is possible to prevent failures such as changes in the distance between the upper and lower brackets 101 or separation caused by the loosening or even falling off of the shock-absorbing balls. Among them, the safety and reliability of the drone suspension shock-absorbing bracket can be improved through the traction member 112, which is convenient for the reliable loading of external loads.
[0052] The embodiment of the present application provides a drone, including a drone body and a drone suspension shock-absorbing bracket arranged below the drone body; an external load is installed on the lower bracket 101 of the drone suspension shock-absorbing bracket.
[0053] The drone provided by the embodiment of the present application adopts the above-mentioned drone suspension shock-absorbing bracket and has good shock-absorbing performance. In addition, the drone suspension shock-absorbing bracket provided by the embodiment of the present application is light and simple, which is convenient for realizing the precise control of the drone.
[0054] Preferably, the drone suspension shock-absorbing bracket provided by the embodiment of the present application includes an upper bracket 100, a lower bracket 101, and a first shock-absorbing component 102; the plane where the upper bracket 100 is located is parallel to the plane where the lower bracket 101 is located, and the first shock-absorbing component 102 is arranged between the upper bracket 100 and the lower bracket 101; the first shock-absorbing component 102 includes a plurality of first shock-absorbing balls 103 arranged at intervals in a plane, one side of the first shock-absorbing ball 103 is connected to the upper bracket 100, and the other side is connected to the lower bracket 101; the side of the lower bracket 101 facing away from the upper bracket 100 is a mounting surface 104 for mounting an external load; the central axis of the first shock-absorbing ball 103 is perpendicular to the plane where the upper bracket 100 is located, so that the gravity generated by the external load can stretch the first shock-absorbing ball 103 along the central axis.
[0055] Among them, a plurality of first extension arms 107 are provided on the upper bracket 100, one end of the first extension arm 107 is connected to the upper bracket 100, and the other end extends away from the upper bracket 100; a second extension arm 108 is provided on the lower bracket 101, and the second extension arm 108 extends in a direction parallel to the extension direction of the first extension arm 107; a second shock-absorbing component 109 is provided between the first extension arm 107 and the second extension arm 108. The second shock-absorbing component 109 includes a plurality of second shock-absorbing balls 110 arranged at intervals around the outer periphery of the upper bracket 100; the central axis of the second shock-absorbing ball 110 intersects with the central axis of the first shock-absorbing ball 103. Among them, the centers of the plurality of first shock-absorbing balls 103 are connected to form a first shock-absorbing surface, and the centers of the plurality of second shock-absorbing balls 110 are connected to form a second shock-absorbing surface, and the first shock-absorbing surface and the second shock-absorbing surface are parallel and spaced apart. Therefore, the embodiment of the present application can form a double-layer shock-absorbing effect.
[0056] The foregoing is only a preferred embodiment of the present application and is not intended to limit the present application. For those skilled in the art, the present application can have various changes and modifications. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included within the protection scope of the present application.
Claims
1. A suspension shock-absorbing bracket for an unmanned aerial vehicle, characterized in that: The invention comprises an upper bracket (100), a lower bracket (101) and a first shock absorbing assembly (102); the plane where the upper bracket (100) is located is parallel to the plane where the lower bracket (101) is located, and the first shock absorbing assembly (102) is arranged between the upper bracket (100) and the lower bracket (101); the first shock absorbing assembly (102) comprises a plurality of first shock absorbing balls (103) arranged in a plane at intervals, one side of the first shock absorbing ball (103) is connected to the upper bracket (100), and the other side is connected to the lower bracket (101); the side of the lower bracket (101) facing away from the upper bracket (100) is a mounting surface (104) for mounting an external load; the central axis of the first shock absorbing ball (103) is perpendicular to the plane where the upper bracket (100) is located, so that the gravity generated by the external load can stretch the first shock absorbing ball (103) along the central axis.
2. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 1, characterized in that: The mounting surface (104) is provided with a quick-release connection structure (105) for mounting an external load, and the connection point between the quick-release connection structure (105) and the lower bracket (101) is located within the area enclosed by the first shock-absorbing ball (103).
3. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 2, characterized in that: The quick-release connection structure (105) is provided with a clamping groove (106) extending in a direction parallel to the plane where the upper bracket (100) is located, and the external load is provided with a clamping protrusion that cooperates with the clamping groove (106).
4. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 1, characterized in that: The upper bracket (100) is provided with a plurality of first extension arms (107), one end of the first extension arm (107) is connected to the upper bracket (100) and the other end thereof extends in a direction away from the upper bracket (100); the lower bracket (101) is provided with a second extension arm (108), the second extension arm (108) is parallel to the extension direction of the first extension arm (107); and a second shock absorbing assembly (109) is provided between the first extension arm (107) and the second extension arm (108).
5. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 4, characterized in that: The second shock absorbing assembly (109) comprises a plurality of second shock absorbing balls (110) arranged at intervals around the outer circumference of the upper bracket (100); the central axis of the second shock absorbing ball (110) intersects with the central axis of the first shock absorbing ball (103).
6. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 5, characterized in that: The first extension arm (107) and the second extension arm (108) are bent close to the external load, and the extension direction of the first extension arm (107) forms a preset angle with the plane where the upper bracket (100) is located; the central axis of the second shock-absorbing ball (110) is perpendicular to the first extension arm (107).
7. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 4, characterized in that: The upper bracket (100) and the lower bracket (101) are rectangular frames with a weight-reducing opening in the middle; the first extension arm (107) and the second extension arm (108) are respectively arranged at the four corners of the rectangular frame and extend in a direction away from the rectangular frame.
8. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 1, characterized in that: It also comprises an adjusting knob (111) and a pulling member (112) arranged on the upper bracket (100); the two ends of the pulling member (112) are respectively connected to the adjusting knob (111) and the middle part of the pulling member (112) is connected to the lower bracket (101); the pulling member (112) can generate a force that causes the upper bracket (100) and the lower bracket (101) to approach each other.
9. The suspension shock-absorbing bracket for unmanned aerial vehicle according to claim 8, characterized in that: The traction member (112) is a traction hanging rope, and the adjustment knob (111) can adjust the extension length of the hanging rope between the upper bracket (100) and the lower bracket (101) by rotating.
10. A drone, characterized in that: It comprises a drone body and the drone suspension shock-absorbing bracket according to any one of claims 1 to 9, wherein the drone suspension shock-absorbing bracket is arranged below the drone body; an external load is installed on the lower bracket (101) of the drone suspension shock-absorbing bracket.