Unmanned aerial vehicle connecting buckle

Abstract

The utility model discloses an unmanned aerial vehicle connecting buckle, and relates to the technical field of hasps. The connecting buckle mechanisms are arranged on the unmanned aerial vehicle body and used for assembling and connecting the unmanned aerial vehicle body, each connecting buckle mechanism comprises a first fixing plate, a second fixing plate, a clamping rod and a position adjusting component, the first fixing plate is fixedly connected to the unmanned aerial vehicle body through a bolt, and the second fixing plate is fixedly connected to the clamping rod through a bolt. One end of the first fixing plate is fixedly connected with two hook plates, and the second fixing plate is fixedly connected to an unmanned aerial vehicle body through bolts. According to the unmanned aerial vehicle connecting buckle, through the use of the connecting buckle mechanism, the fastening degree can be adjusted according to the required distance, the anti-loosening effect can be achieved, the fixing hole positions of the buckle are scientifically distributed, the stress of the buckle is more uniform in the use process of the buckle, and the buckle is suitable for all the positions needing to be quickly disassembled on a small unmanned aerial vehicle; and the hasp has a loosening function, and the service life of the hasp is longer.

Description

Technical Field

[0001] This utility model relates to the field of buckle technology, specifically a drone connection buckle. Background Technology

[0002] To enable rapid assembly of various components, drones require a quick-connect structure. Currently, most drones use latches and spring clips as connection structures. Using spring clips as connectors requires high positioning accuracy for each component, while using latches as connectors is preferable.

[0003] The authorized publication number "CN209112422U" describes "a composite vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV) that is easy to disassemble and pack, comprising: a fuselage, the lower part of which is connected to the landing gear; an engine mounted at the rear of the fuselage, with a propeller connected to the engine; a middle wing connected to the upper part of the fuselage; the middle wing being spliced ​​with a left wing and a right wing; the rear end of the left wing being a left aileron; a left arm and a left tail boom mounted on the left side of the middle wing; the right side having the same structure as the left side; and the left and right tail booms being connected to the tail fin." This utility model enables rapid disassembly of the various components of the UAV, greatly reducing the storage volume of the UAV and saving transportation costs. Furthermore, the UAV can be manufactured in sections, reducing manufacturing and processing costs and facilitating mass production.

[0004] The aforementioned patent enables rapid disassembly of various components of the drone, greatly reducing the drone's storage volume and saving transportation costs. At the same time, the drone can be manufactured in sections, reducing the manufacturing and processing costs of the drone and facilitating mass production. However, the large latches currently on the market cannot be used on small drones because they are too large, and the small latches do not have an anti-loosening function, which will loosen after long-term use. Utility Model Content

[0005] This utility model provides a drone connection buckle. By using the connection buckle mechanism, the tightness can be adjusted according to the required distance and a loosening effect can be achieved. The fixed holes of the buckle are scientifically distributed, and the force on the buckle is more even during use. The buckle is suitable for various quick-release positions on small drones and has a loosening function, resulting in a longer service life.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a drone connection buckle, comprising:

[0007] The fuselage of the drone;

[0008] The connecting buckle mechanism comprises multiple sets, all of which are mounted on the drone body for assembling and connecting the drone body. Each set of the connecting buckle mechanism includes a first fixing plate, a second fixing plate, a locking rod, and an adjusting component. The first fixing plate is fixedly connected to the drone body by bolts, and one end of the first fixing plate is fixedly connected to two hook plates. The second fixing plate is fixedly connected to the drone body by bolts, and one end of the second fixing plate is rotatably connected to a rotating plate. The adjusting component is located on the rotating plate, and the locking rod is located on the adjusting component, with both ends of the locking rod respectively engaged in the two hook plates.

[0009] Furthermore, the positioning component includes two slides and a linkage assembly. The two slides are respectively opened on both sides of the rotating plate, and the linkage assembly is located inside the two rotating plates.

[0010] Furthermore, the linkage component includes a sliding rod and two connecting plates. The two ends of the sliding rod are slidably connected to two sliding grooves, and the two connecting plates are rotatably connected to the two ends of the sliding rod, with one end of each connecting plate rotatably connected to the upper part of the locking rod.

[0011] Furthermore, it also includes a pushing mechanism, which is set on the second fixed plate and is used to control the position of the sliding rod. The pushing mechanism includes two sets of limiting components, a pushing arc plate and two top springs. A positioning plate is fixedly connected to one side of the top of the second fixed plate, and one end of each of the two top springs is fixedly connected to the positioning plate. The pushing arc plate is fixedly connected to one end of each of the two top springs.

[0012] Furthermore, each of the limiting components includes a limiting rod and a limiting sleeve. The limiting sleeve is fixedly connected to the positioning plate, and the limiting rod is fixedly connected to the push-position arc plate. The limiting rod is movably inserted into the limiting sleeve.

[0013] Furthermore, a fixing post is fixedly connected to the center of one bottom end of the rotating plate, and a strong magnetic base is fixedly connected to the center of one top end of the second fixing plate, with the fixing post installed inside the strong magnetic base.

[0014] This utility model provides a drone connection clip. It has the following beneficial effects:

[0015] (1) The drone connection buckle, through the use of the connection buckle mechanism, can adjust the tightness according to the required distance and achieve the anti-loosening effect. The fixed hole of the buckle is scientifically distributed, and the force of the buckle is more even during the use of the buckle. The buckle is suitable for various quick-release positions on small drones and has a loosening function, and the service life of the buckle is longer. Attached Figure Description

[0016] Figure 1This is a perspective view of the present utility model;

[0017] Figure 2 This is an exploded cross-sectional view of the connecting buckle mechanism of this utility model;

[0018] Figure 3 This is an exploded view of the connecting buckle mechanism of this utility model;

[0019] Figure 4 This is a partial sectional view of the connecting buckle mechanism of this utility model;

[0020] Figure 5 This is a perspective view of the connecting buckle mechanism of this utility model.

[0021] In the diagram: 1. UAV fuselage; 2. Connecting buckle mechanism; 201. First fixing plate; 202. Clamping rod; 203. Rotating plate; 204. Fixing column; 205. Pushing arc plate; 206. Top spring; 207. Limiting rod; 208. Sliding rod; 209. Second fixing plate; 210. Positioning plate; 211. Limiting sleeve; 212. Strong magnetic base; 213. Slide groove; 214. Hook plate; 215. Connecting plate. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present utility model, not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the scope of protection of the present utility model.

[0023] Please see Figure 1-5 This utility model provides a technical solution: a drone connection buckle, comprising:

[0024] Unmanned aerial vehicle fuselage 1;

[0025] The connecting buckle mechanism 2 is provided in multiple sets, all of which are located on the drone body 1 for the assembly and connection of the drone body 1. Each set of connecting buckle mechanisms 2 includes a first fixing plate 201, a second fixing plate 209, a locking rod 202, and an adjusting component. The first fixing plate 201 is fixedly connected to the drone body 1 by bolts, and one end of the first fixing plate 201 is fixedly connected to two hook plates 214. The second fixing plate 209 is fixedly connected to the drone body 1 by bolts, and one end of the second fixing plate 209 is rotatably connected to a rotating plate 203. The adjusting component is located on the rotating plate 203, and the locking rod 202 is located on the adjusting component. Both ends of the locking rod 202 are respectively locked into the two hook plates 214.

[0026] In this implementation scheme: the drone body 1 is based on existing technology. The connecting buckle mechanism 2 is used at different positions on the drone body 1 to connect the drone body 1 as a whole, ensuring quick assembly and disassembly. The first fixing plate 201 and the second fixing plate 209 are changed from steel plates to metal processing parts. The tension hook plate can withstand stronger loads and will not deform after long-term use. The clamping rod 202 is connected to the two hook plates 214 to ensure the effect of use.

[0027] Specifically, the adjustment component includes two slides 213 and a linkage assembly. The two slides 213 are respectively opened on both sides of the rotating plate 203, and the linkage assembly is located inside the two rotating plates 203.

[0028] In this embodiment, the two slides 213 adjust the position of the lever 202 through the linkage component to ensure the effect of use.

[0029] Specifically, the linkage component includes a sliding rod 208 and two connecting plates 215. The two ends of the sliding rod 208 are slidably connected to the two sliding grooves 213 respectively, and the two connecting plates 215 are rotatably connected to the two ends of the sliding rod 208 respectively, and one end of each of the two connecting plates 215 is rotatably connected to the upper part of the locking rod 202.

[0030] In this embodiment, the sliding rod 208 and the two connecting plates 215 work together to complete the overall use, and the overall rotational connection does not affect the rotational use during use.

[0031] Specifically, it also includes a pushing mechanism, which is set on the second fixed plate 209 and used to control the position of the sliding rod 208. The pushing mechanism includes two sets of limiting components, a pushing arc plate 205 and two top springs 206. A positioning plate 210 is fixedly connected to one side of the top of the second fixed plate 209. One end of each of the two top springs 206 is fixedly connected to the positioning plate 210. The pushing arc plate 205 is fixedly connected to one end of each of the two top springs 206.

[0032] In this embodiment, two top springs 206 control the position of the push-position arc plate 205 and the position of the sliding rod 208, while preventing foreign objects from affecting the compression distance of the springs during use.

[0033] Specifically, each set of limiting components includes a limiting rod 207 and a limiting sleeve 211. The limiting sleeve 211 is fixedly connected to the positioning plate 210, and the limiting rod 207 is fixedly connected to the push-position arc plate 205. The limiting rod 207 is movably inserted into the limiting sleeve 211.

[0034] In this embodiment, the limiting rod 207 and the limiting sleeve 211 are used together to limit the extension and retraction of the top spring 206 and avoid the influence of bending.

[0035] Specifically, a fixing post 204 is fixedly connected to the center of the bottom end of the rotating plate 203, and a strong magnetic base 212 is fixedly connected to the center of the top end of the second fixing plate 209. The fixing post 204 is installed inside the strong magnetic base 212.

[0036] In this embodiment, the powerful magnetic base 212 and the fixed column 204 cooperate with each other to keep the position of the rotating plate 203 stable and prevent it from opening.

[0037] In use, the connecting buckle mechanism 2 is used at different positions on the drone body 1 to connect the drone body 1 as a whole, ensuring quick assembly and disassembly. During assembly, the first fixing plate 201 is fixed to the component, and the second fixing plate 209 is fixed to the body. The strong magnetic seat 212 and the fixing column 204 cooperate with each other to keep the position of the rotating plate 203 stable and prevent it from opening. Pull the locking rod 202 to lock it in the hook plate 214 to ensure connection. After locking, the top spring 206 controls the position of the pushing arc plate 205, so that the pushing arc plate 205 pushes the position of the sliding rod 208 to ensure the connection effect between the locking rod 202 and the hook plate 214 and ensure the use effect.

[0038] The control method of this utility model is to control the device by manually starting and stopping the switch. The wiring diagram of the power element and the supply of power are common knowledge in the field. Since this utility model is mainly used to protect mechanical devices, the control method and wiring layout will not be explained in detail.

[0039] The above is only a preferred specific implementation method of the present invention, but the protection scope of the present invention is not limited to this. Any technician familiar with the technical field within the technical scope disclosed by the present invention can make equivalent replacements or changes based on the technical solution and utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A drone connection clip, characterized in that, include: Unmanned aerial vehicle fuselage (1); The connecting buckle mechanism (2) is provided in multiple sets. All sets of the connecting buckle mechanism (2) are provided on the drone body (1) for the assembly and connection of the drone body (1). Each set of the connecting buckle mechanism (2) includes a first fixing plate (201), a second fixing plate (209), a locking rod (202) and an adjusting component. The first fixing plate (201) is fixedly connected to the drone body (1) by bolts, and one end of the first fixing plate (201) is fixedly connected to two hook plates (214). The second fixing plate (209) is fixedly connected to the drone body (1) by bolts, and one end of the second fixing plate (209) is rotatably connected to a rotating plate (203). The adjusting component is provided on the rotating plate (203), and the locking rod (202) is provided on the adjusting component. Both ends of the locking rod (202) are respectively locked in the two hook plates (214).

2. The drone connection clip according to claim 1, characterized in that, The adjustment component includes two slides (213) and a linkage assembly. The two slides (213) are respectively opened on both sides of the rotating plate (203), and the linkage assembly is located in the two rotating plates (203).

3. The drone connection clip according to claim 2, characterized in that, The linkage component includes a sliding rod (208) and two connecting plates (215). The two ends of the sliding rod (208) are slidably connected to two sliding grooves (213), and the two connecting plates (215) are rotatably connected to the two ends of the sliding rod (208), and one end of each connecting plate (215) is rotatably connected to the upper part of the locking rod (202).

4. A drone connection clip according to claim 3, characterized in that, It also includes a pushing mechanism, which is located on the second fixed plate (209) and is used to control the position of the sliding rod (208). The pushing mechanism includes two sets of limiting components, a pushing arc plate (205) and two top springs (206). A positioning plate (210) is fixedly connected to one side of the top of the second fixed plate (209). One end of each of the two top springs (206) is fixedly connected to the positioning plate (210). The pushing arc plate (205) is fixedly connected to one end of each of the two top springs (206).

5. A drone connection clip according to claim 4, characterized in that, Each of the limiting components includes a limiting rod (207) and a limiting sleeve (211). The limiting sleeve (211) is fixedly connected to the positioning plate (210), and the limiting rod (207) is fixedly connected to the push-position arc plate (205). The limiting rod (207) is movably inserted into the limiting sleeve (211).

6. A drone connection clip according to claim 5, characterized in that, A fixing post (204) is fixedly connected to the center of the bottom end of the rotating plate (203), and a strong magnetic base (212) is fixedly connected to the center of the top end of the second fixing plate (209). The fixing post (204) is installed inside the strong magnetic base (212).

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