Carbon fiber support connecting device of unmanned aerial vehicle
By designing the connecting and positioning components of the UAV carbon fiber bracket connection device, the problem of loose bolt connections was solved, achieving a highly stable and efficient connection effect.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- APEX TOYS SHENZHEN
- Filing Date
- 2025-05-23
- Publication Date
- 2026-06-26
AI Technical Summary
The existing method of bolting the carbon fiber bracket to the drone body is prone to loosening due to vibration, posing a risk of detachment and resulting in poor stability.
The design employs a combination of connecting and positioning components. The double locking effect of the snap-fit block and the beveled top block increases the connection strength between the bracket and the machine body. The positioning component locks the angle of the positive and negative threaded rods to prevent rotation.
It improves the connection stability between the bracket and the body, prevents detachment after long-term use, and has a good locking effect and high disassembly efficiency.
Smart Images
Figure CN224409645U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the technical field of drone brackets, and in particular to a carbon fiber bracket connection device for drones. Background Technology
[0002] A carbon fiber drone bracket is an accessory used on drones. Made of carbon fiber, it minimizes the burden on the drone and provides some protection, making it a common drone accessory.
[0003] Currently, when assembling the carbon fiber bracket for drones with the drone body, bolts are usually used for fixing. Although this connection method is simple and quick, drones will vibrate to a certain extent during operation. Over time, this vibration will cause the bolts to loosen, which may lead to the bracket detaching from the drone body, resulting in poor stability. Utility Model Content
[0004] The purpose of this utility model is to provide a carbon fiber bracket connection device for unmanned aerial vehicles (UAVs) to solve the problem mentioned in the background art that the existing carbon fiber brackets, which are fixed to the body with bolts, are prone to loosening due to vibration of the body, posing a risk of detachment.
[0005] To achieve the above objectives, the present invention provides the following technical solution: a carbon fiber bracket connection device for a drone, comprising a bracket body, a connecting frame fixedly connected to the upper surface of the bracket body, two connecting components slidably connected to the inner bottom wall of the connecting frame, a rectangular groove provided on the right side of the connecting frame, and a positioning component slidably connected to the inner wall of the rectangular groove.
[0006] The connecting component is used to connect and assemble the bracket body and the machine body, and the positioning component is used to limit and prevent the connecting component from detaching.
[0007] Preferably, the connecting assembly includes a strip frame, with transmission blocks fixedly connected to the lower surfaces of both strip frames. Two sliding grooves are provided on the inner bottom wall of the connecting frame. A positive and negative threaded rod is rotatably connected to the right side of the connecting frame. The left end of the positive and negative threaded rod is rotatably connected to the left inner wall of the sliding groove. A circular ring is fixedly connected to the right end of the positive and negative threaded rod. A positioning slot is provided on the right side of the circular ring. The two transmission blocks are threadedly connected to the positive and negative threads on the surface of the positive and negative threaded rod, respectively.
[0008] Preferably, each of the two strip frames is fixedly connected to a snap-fit block on its opposite side. The upper surface of the snap-fit block is provided with a rectangular through hole. The inner wall of the rectangular through hole is provided with two limiting grooves. The inner walls of the two limiting grooves are slidably connected to limiting blocks. The inner walls of the two limiting grooves are fixedly connected to a first spring. The end of the first spring away from the inner wall of the limiting groove is fixedly connected to the limiting block.
[0009] Preferably, the side of the limiting block away from the inner wall of the limiting groove is fixedly connected to a beveled top block, and both beveled top blocks are slidably connected to the inner wall of the rectangular through hole.
[0010] Preferably, the strip frame has an internal movable cavity, the inner wall of the movable cavity is slidably connected to a right-angle pressure plate, the upper surface of the strip frame is threadedly connected to a threaded rod, the bottom end of the threaded rod extends into the interior of the movable cavity and is rotatably connected to the upper surface of the right-angle pressure plate, and the inner wall of the movable cavity has a through hole.
[0011] Preferably, the snap-fit block has an ejector hole on the side near the strip frame corresponding to the through hole. The inner top wall of the ejector hole has a moving groove. A moving block is slidably connected to the inner top wall of the moving groove. A second spring is fixedly connected to the inner wall of the moving groove. The end of the second spring away from the inner wall of the moving groove is fixedly connected to the moving block. A double-sloped top rod is fixedly connected to the lower surface of the moving block. The two ends of the double-sloped top rod correspond to the positions of the right-angle pressure plate and the two sloping top blocks, respectively.
[0012] Preferably, the positioning component includes a rectangular rod, a strip groove is formed on the inner top wall of the rectangular groove, a locking rod is fixedly connected to the inner wall of the strip groove, a third spring is sleeved on the surface of the locking rod, a rectangular block is slidably connected to the inner top wall of the strip groove, the lower surface of the rectangular block is fixedly connected to the upper surface of the rectangular rod, and the left end of the third spring overlaps with the right side of the rectangular block, the right end of the third spring overlaps with the right inner wall of the strip groove, and a right-angled locking block is fixedly connected to the back of the rectangular rod, and the right-angled locking block is adapted to the positioning slot.
[0013] Compared with the prior art, the beneficial effects of this utility model are as follows: This carbon fiber bracket connection device for drones, through the cooperation of the connecting component and the positioning component, can increase the connection strength between the bracket body and the aircraft body through the double locking effect of the snap-fit block and the inclined top block during use, thereby ensuring that the bracket body will not detach from the aircraft body after long-term use, resulting in higher stability. In addition, the positioning component can also lock the angle of the positive and negative threaded rods, ensuring that the positive and negative threaded rods will not rotate on their own due to vibration during long-term use, resulting in a better locking effect. Attached Figure Description
[0014] Figure 1 This is a three-dimensional structural diagram of the present invention;
[0015] Figure 2 This is a schematic diagram of the cross-sectional structure of the strip frame of this utility model;
[0016] Figure 3 This utility model Figure 2 Enlarged schematic diagram of the structure at point A in the middle;
[0017] Figure 4 This is a three-dimensional structural diagram of the positioning component of this utility model.
[0018] In the diagram: 1. Bracket body; 2. Connecting frame; 3. Connecting assembly; 4. Positioning assembly; 301. Strip frame; 302. Transmission block; 303. Positive and negative threaded rod; 304. Circular ring; 305. Positioning slot; 306. Snap-fit block; 307. Limiting block; 308. First spring; 309. Inclined top block; 310. Right-angle pressure plate; 311. Threaded rod; 312. Moving block; 313. Second spring; 314. Double-inclined top rod; 401. Rectangular rod; 402. Locking rod; 403. Third spring; 404. Rectangular block; 405. Right-angle snap-fit block. Detailed Implementation
[0019] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and 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 protection scope of the present utility model.
[0020] Please see Figure 1-4 This utility model provides a technical solution: a carbon fiber bracket connection device for a drone, including a bracket body 1, a connecting frame 2 fixedly connected to the upper surface of the bracket body 1, two connecting components 3 slidably connected to the inner bottom wall of the connecting frame 2, a rectangular groove is opened on the right side of the connecting frame 2, and a positioning component 4 is slidably connected to the inner wall of the rectangular groove.
[0021] The connecting component 3 is used to connect and assemble the bracket body 1 with the machine body, and the positioning component 4 is used to limit and prevent the connecting component 3 from detaching.
[0022] Furthermore, the connecting assembly 3 includes a strip frame 301, with transmission blocks 302 fixedly connected to the lower surfaces of both strip frames 301. Two sliding grooves are formed in the inner bottom wall of the connecting frame 2. A positive and negative threaded rod 303 is rotatably connected to the right side of the connecting frame 2. The left end of the positive and negative threaded rod 303 is rotatably connected to the left inner wall of the sliding groove. A circular ring 304 is fixedly connected to the right end of the positive and negative threaded rod 303. A positioning slot 305 is formed on the right side of the circular ring 304. The two transmission blocks 302 are threadedly connected to the positive and negative threads on the surface of the positive and negative threaded rod 303, respectively. A locking block 306 is fixedly connected to the opposite surfaces of both strip frames 301. A rectangular through hole is formed on the upper surface of the locking block 306. Two limiting grooves are formed in the inner wall of the rectangular through hole. The inner walls of the two limiting grooves are... A sliding connection is provided with a limiting block 307. A first spring 308 is fixedly connected to the inner wall of each of the two limiting grooves. The end of the first spring 308 away from the inner wall of the limiting groove is fixedly connected to the limiting block 307. A beveled top block 309 is fixedly connected to the side of the limiting block 307 away from the inner wall of the limiting groove, and both beveled top blocks 309 are slidably connected to the inner wall of the rectangular through hole. A movable cavity is provided inside the strip frame 301. A right-angle pressure plate 310 is slidably connected to the inner wall of the movable cavity. A threaded rod 311 is threadedly connected to the upper surface of the strip frame 301. The bottom end of the threaded rod 311 extends into the interior of the movable cavity and is rotatably connected to the upper surface of the right-angle pressure plate 310. A through hole is provided in the inner wall of the movable cavity. A snap-fit block 306 is located on the side of the strip frame 301 corresponding to the through hole. An ejector hole is provided at the position, and a movable groove is provided on the inner top wall of the ejector hole. A movable block 312 is slidably connected to the inner top wall of the movable groove. A second spring 313 is fixedly connected to the inner wall of the movable groove. The end of the second spring 313 away from the inner wall of the movable groove is fixedly connected to the movable block 312. A double-beveled push rod 314 is fixedly connected to the lower surface of the movable block 312. The two ends of the double-beveled push rod 314 correspond to the positions of the right-angle pressure plate 310 and the two beveled push blocks 309, respectively. After rotating the positive and negative threaded rods 303, the two strip frames 301 can be driven to move closer to each other through the two transmission blocks 302 until the two locking blocks 306 are inserted into the slots on both sides of the machine body. The inner top wall and inner bottom wall of the slots on both sides of the machine body are provided with locking grooves. At this time, rotating the two threaded rods 311 The threaded rod 311 drives the right-angle pressure plate 310 to descend within the movable cavity. The right-angle pressure plate 310 can press the double-sloped top rod 314, causing the two double-sloped top rods 314 to move closer to each other. During the movement of the two double-sloped top rods 314, they can press the second spring 313 through the moving block 312. At the same time, the two double-sloped top rods 314 can press the two sets of sloping top blocks 309, causing the sloping top blocks 309 to press the first spring 308 through the limiting block 307. This allows the two sets of sloping top blocks 309 to protrude through the upper and lower surfaces of the snap-fit block 306, thereby inserting into the locking groove. The snap-fit block 306 and the sloping top blocks 309 can achieve a double locking effect, thereby increasing the connection stability between the bracket body 1 and the machine body, preventing easy detachment.
[0023] Furthermore, the positioning component 4 includes a rectangular rod 401, a strip groove is formed on the inner top wall of the rectangular groove, a locking rod 402 is fixedly connected to the inner wall of the strip groove, a third spring 403 is sleeved on the surface of the locking rod 402, a rectangular block 404 is slidably connected to the inner top wall of the strip groove, the lower surface of the rectangular block 404 is fixedly connected to the upper surface of the rectangular rod 401, and the left end of the third spring 403 overlaps with the right side of the rectangular block 404, and the right end of the third spring 403 overlaps with the right inner wall of the strip groove. A right-angled locking block 405 is fixedly connected to the back of the rectangular rod 401, and the right-angled locking block 405 and the positioning slot 305 are connected. In accordance with the action of the third spring 403, the rectangular block 404 will drive the rectangular rod 401 to exert pressure to the left, and the right-angle locking block 405 will be tightly locked in the positioning slot 305 on the right side of the circular ring 304. This locks the angle of the circular ring 304 and the positive and negative threaded rod 303, ensuring that the positions of the two strip frames 301 will not shift. After the two locking blocks 306 are inserted into the machine body, the circular ring 304 will drive the positioning slot 305 to correspond exactly with the right-angle locking block 405. Therefore, there will be no problem that the right-angle locking block 405 cannot be locked into the positioning slot 305.
[0024] Working principle: First, the machine body is secured within the connecting frame 2. Pulling the right-angle locking block 405 forward disengages it from the positioning slot 305. At this point, the threaded rods 303 and the circular ring 304 are no longer restricted. Rotating the threaded rods 303 brings the two transmission blocks 302 closer together. The two transmission blocks 302 drive the two strip frames 301 closer together until the two locking blocks 306 are engaged in the slots on both sides of the machine body. Then, rotating the two threaded rods 311 lowers the right-angle pressure plate 310 within the movable cavity. The right-angle pressure plate 310 presses against the double-beveled push rods 314, causing them to move towards the center. During this movement, the moving block 312 presses against the second spring 313. The double-beveled push rods 314 press against the two beveled push blocks 309, thereby driving the two... The beveled top block 309 moves out from the upper and lower surfaces of the snap-fit block 306 and snaps into the locking groove in the slot. At this time, the right-angle snap-fit block 405 is released. The reaction force generated by the third spring 403 can drive the rectangular block 404 and the rectangular rod 401 to move to the left, thereby driving the right-angle snap-fit block 405 to re-insert into the positioning slot 305 on the right side of the circular ring 304. This locks the circular ring 304 and the positive and negative threaded rod 303. Through the double limiting effect of the snap-fit block 306 and the beveled top block 309, the connection stability between the bracket body 1 and the machine body can be ensured, and the bracket body 1 will not be dislodged due to shaking. In addition, the right-angle snap-fit block 405 plays a certain safety role, which can prevent the positive and negative threaded rod 303 from rotating. The locking effect is better and the efficiency is higher when disassembling.
[0025] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A carbon fiber support connection device for a drone, comprising a support body (1), characterized in that: The upper surface of the bracket body (1) is fixedly connected to a connecting frame (2), and two connecting components (3) are slidably connected to the inner bottom wall of the connecting frame (2). A rectangular groove is opened on the right side of the connecting frame (2), and a positioning component (4) is slidably connected to the inner wall of the rectangular groove. The connecting component (3) is used to connect and assemble the bracket body (1) with the machine body, and the positioning component (4) is used to limit the connecting component (3) to prevent it from falling off.
2. The carbon fiber bracket connection device for a drone according to claim 1, characterized in that: The connecting component (3) includes a strip frame (301), and a transmission block (302) is fixedly connected to the lower surface of each of the two strip frames (301). Two sliding grooves are opened in the inner bottom wall of the connecting frame (2). A positive and negative threaded rod (303) is rotatably connected to the right side of the connecting frame (2). The left end of the positive and negative threaded rod (303) is rotatably connected to the left inner wall of the sliding groove. A circular ring (304) is fixedly connected to the right end of the positive and negative threaded rod (303). A positioning slot (305) is opened on the right side of the circular ring (304). The two transmission blocks (302) are respectively threaded to the positive and negative threads on the surface of the positive and negative threaded rod (303).
3. The carbon fiber bracket connection device for a drone according to claim 2, characterized in that: Each of the two strip frames (301) has a snap-fit block (306) fixedly connected to its opposite face. The upper surface of the snap-fit block (306) has a rectangular through hole. The inner wall of the rectangular through hole has two limiting grooves. The inner walls of the two limiting grooves are slidably connected to limiting blocks (307). The inner walls of the two limiting grooves are fixedly connected to a first spring (308). The end of the first spring (308) away from the inner wall of the limiting groove is fixedly connected to the limiting block (307).
4. The carbon fiber bracket connection device for a drone according to claim 3, characterized in that: The limiting block (307) is fixedly connected to a beveled top block (309) on the side away from the inner wall of the limiting groove, and both beveled top blocks (309) are slidably connected to the inner wall of the rectangular through hole.
5. The carbon fiber bracket connection device for a drone according to claim 2, characterized in that: The strip frame (301) has an internal movable cavity. A right-angle pressure plate (310) is slidably connected to the inner wall of the movable cavity. A threaded rod (311) is threadedly connected to the upper surface of the strip frame (301). The bottom end of the threaded rod (311) extends into the interior of the movable cavity and is rotatably connected to the upper surface of the right-angle pressure plate (310). A through hole is provided in the inner wall of the movable cavity.
6. The carbon fiber bracket connection device for a drone according to claim 3, characterized in that: The snap-fit block (306) has an ejector hole on the side of the strip frame (301) corresponding to the through hole. The inner top wall of the ejector hole has a moving groove. The inner top wall of the moving groove is slidably connected to a moving block (312). The inner wall of the moving groove is fixedly connected to a second spring (313). The end of the second spring (313) away from the inner wall of the moving groove is fixedly connected to the moving block (312). The lower surface of the moving block (312) is fixedly connected to a double-sloped top rod (314). The two ends of the double-sloped top rod (314) correspond to the positions of the right-angle pressure plate (310) and the two sloped top blocks (309), respectively.
7. The carbon fiber bracket connection device for a drone according to claim 1, characterized in that: The positioning component (4) includes a rectangular rod (401), a strip groove is provided on the inner top wall of the rectangular groove, a locking rod (402) is fixedly connected to the inner wall of the strip groove, a third spring (403) is sleeved on the surface of the locking rod (402), a rectangular block (404) is slidably connected to the inner top wall of the strip groove, the lower surface of the rectangular block (404) is fixedly connected to the upper surface of the rectangular rod (401), and the left end of the third spring (403) overlaps with the right side of the rectangular block (404), the right end of the third spring (403) overlaps with the right inner wall of the strip groove, and a right-angled locking block (405) is fixedly connected to the back of the rectangular rod (401), and the right-angled locking block (405) is adapted to the positioning slot (305).