Unmanned aerial vehicle carbon tube anti-loose rapid butt joint structure and unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicle structures, and discloses an unmanned aerial vehicle carbon tube anti-loosening rapid butt joint structure and an unmanned aerial vehicle, the unmanned aerial vehicle carbon tube anti-loosening rapid butt joint structure comprises a first butt joint module, a second butt joint module, a spring bolt, a spring bolt base, a locking ring and a pressure spring, the first butt joint module is sleeved with the spring bolt base, the spring bolt base is sleeved with the first butt joint module before the first butt joint module is bonded, the situation that the first butt joint module cannot be sleeved with the first butt joint module after bonding is avoided, and the locking ring is connected to the spring bolt base in a threaded mode and used for locking the two butt joint modules after the first butt joint module and the second butt joint module are in butt joint. After the anti-loosening quick butt joint structure is applied to the unmanned aerial vehicle, quick, simple and convenient butt joint of the unmanned aerial vehicle and the carbon tube can be quickly achieved, it is ensured that the carbon tube can be stably locked in the connected state, and the loosening risk is reduced.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle structures, in particular to an unmanned aerial vehicle carbon tube anti-loosening quick docking structure and an unmanned aerial vehicle. Background Art

[0002] Unmanned aerial vehicles, also known as "drones", are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices, or are operated completely or intermittently autonomously by on-board computers.

[0003] In the field of drones, the design and performance of docking structures are crucial. Traditional docking structures may have problems such as loose connections, complex operations, and time consumption. At present, drone docking structures mainly use metal connections or complex threaded structures, which have problems such as cumbersome operations, loose connections, and susceptibility to environmental influences. In order to improve the flexibility and reliability of drones, a new type of docking structure is needed. Therefore, a drone carbon tube anti-loosening quick docking structure is proposed, which improves docking efficiency, reduces the operating burden, and ensures the firmness and safety of the connection. This innovation is expected to promote the development of the drone field and provide a more reliable connection experience. Utility Model Content

[0004] The utility model aims to provide a carbon tube anti-loosening quick docking structure for a UAV and a UAV, so as to achieve the purpose of solving the above-mentioned problems.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a carbon tube anti-loosening quick docking structure for unmanned aerial vehicles, comprising a first docking module, a second docking module, a locking tongue, a locking tongue base, a locking ring and a compression spring;

[0006] The first docking module is plugged into the interior of the second docking module;

[0007] The locking tongue base is sleeved on the first docking module and is inserted before the first docking module is bonded to avoid being unable to be inserted after bonding;

[0008] The locking ring is threadedly connected to the locking tongue base and is used to lock the two docking modules after the first docking module and the second docking module are docked;

[0009] The lock tongue is inlaid in the inside of the lock tongue base bayonet by rivets, and is used to hook the locking ring after locking to prevent loosening and falling off;

[0010] The compression spring is arranged between the lock tongue base and the lock tongue, and is used to give the lock tongue a downward force to control the compression tongue to lock the locking ring.

[0011] Preferably, a first limiting cylinder is fixedly connected to the outer wall of the lock tongue base, and the lower end of the compression spring is fixedly installed inside the first limiting cylinder. The setting of the first limiting cylinder can limit and fix the lower end of the compression spring, thereby avoiding the problem of position deviation of the lower end of the compression spring.

[0012] Preferably, the bottom of the locking tongue is fixedly connected to a second limiting cylinder, and the upper end of the compression spring is fixedly installed inside the second limiting cylinder. The setting of the second limiting cylinder can limit and fix the upper end of the compression spring, thereby avoiding the problem of position displacement of the upper end of the compression spring.

[0013] Preferably, a limiting groove is provided on the outer wall of the first docking module, and a convex strip is provided inside the second docking module, and the convex strip is inserted into the limiting groove. The setting of the limiting groove and the convex strip can play a limiting role for the first docking module.

[0014] Preferably, a fixing plate is fixedly mounted on the lock tongue, and a rubber sheet is bonded to the fixing plate. The arrangement of the fixing plate and the rubber sheet can increase the contact friction between the lock tongue and the locking ring, thereby improving the locking effect.

[0015] A drone comprises the drone carbon tube anti-loosening quick docking structure.

[0016] The utility model provides a carbon tube anti-loosening quick docking structure for unmanned aerial vehicles and the unmanned aerial vehicle, which has the following beneficial effects:

[0017] The utility model applies the anti-loosening quick docking structure to the UAV, which can not only quickly realize the quick and easy docking of the UAV and the carbon tube, but also ensure that the carbon tube can be firmly locked in the connected state, reducing the risk of loosening. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The accompanying drawings are used to provide a further understanding of the present invention and constitute a part of the specification. Together with the embodiments of the present invention, they are used to explain the present invention and do not constitute a limitation of the present invention. In the accompanying drawings:

[0019] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0020] Figure 2 This is a schematic diagram of the structure of the first docking module of the utility model;

[0021] Figure 3 This is a schematic diagram of the structure of the second docking module of the utility model;

[0022] Figure 4 for Figure 1 A schematic diagram of the enlarged structure in the middle.

[0023] In the figure: 1. first docking module; 2. second docking module; 3. locking tongue; 4. locking tongue base; 5. locking ring; 6. first limiting cylinder; 7. compression spring; 8. second limiting cylinder; 9. limiting groove; 10. convex strip; 11. fixing plate; 12. rubber sheet. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0025] like Figure 1-4 As shown, the utility model provides a technical solution: a carbon tube anti-loosening quick docking structure for unmanned aerial vehicles, comprising a first docking module 1, a second docking module 2, a locking tongue 3, a locking tongue base 4, a locking ring 5 and a compression spring 7;

[0026] The first docking module 1 is plugged into the interior of the second docking module 2;

[0027] The lock tongue base 4 is sleeved on the first docking module 1 and is inserted before bonding the first docking module 1 to avoid being unable to be inserted after bonding;

[0028] The locking ring 5 is threadedly connected to the locking tongue base 4, and is used to lock the two docking modules after the first docking module 1 and the second docking module 2 are docked;

[0029] The lock tongue 3 is inlaid in the inside of the lock tongue base 4 by rivets, and is used to hook the locking ring 5 after locking to prevent loosening and falling off;

[0030] The compression spring 7 is arranged between the lock tongue base 4 and the lock tongue 3 , and is used to give the lock tongue 3 a downward force to control the compression spring to lock the locking ring 5 .

[0031] A first limiting cylinder 6 is fixedly connected to the outer wall of the lock tongue base 4, and the lower end of the compression spring 7 is fixedly installed inside the first limiting cylinder 6. The setting of the first limiting cylinder 6 can limit and fix the lower end of the compression spring 7, thereby avoiding the problem of position deviation of the lower end of the compression spring 7.

[0032] The bottom of the lock tongue 3 is fixedly connected to a second limiting cylinder 8, and the upper end of the compression spring 7 is fixedly installed inside the second limiting cylinder 8. The setting of the second limiting cylinder 8 can limit and fix the upper end of the compression spring 7, thereby avoiding the problem of position deviation of the upper end of the compression spring 7.

[0033] A limiting groove 9 is provided on the outer wall of the first docking module 1 , and a convex strip 10 is provided inside the second docking module 2 . The convex strip 10 is inserted into the limiting groove 9 . The setting of the limiting groove 9 and the convex strip 10 can limit the first docking module 1 .

[0034] A fixing plate 11 is fixedly mounted on the lock tongue 3, and a rubber sheet 12 is bonded to the fixing plate 11. The setting of the fixing plate 11 and the rubber sheet 12 can increase the contact friction between the lock tongue 3 and the locking ring 5, thereby improving the locking effect.

[0035] A UAV comprises a carbon tube anti-loosening quick docking structure for the UAV.

[0036] When in use, when bonding the first docking module 1 and the second docking module 2, use a cleaning tool to ensure that the surface of the docking point between the carbon tube and the docking module is clean, free of dust or foreign matter, carefully check the carbon tube and the docking point to ensure that there is no visible damage or defect, and in the process of docking the first docking module 1 and the second docking module 2, pay attention to the notch cooperation between the two modules, otherwise the plugging will not be successful. When the docking is successful, push the locking ring 5 in the opposite direction to tighten it, and after tightening, push the lock tongue base 4 forward until it is aligned with the docking module, press the lock tongue 3 during the pushing process, so that it is lifted up to avoid collision with the docking module, so as to avoid unnecessary structural damage, and when the lock tongue base 4 is aligned with the docking module, put down the lock tongue 3 so that it hooks the end face of the docking module on the other side. If it is not hooked, there is a gap between the carbon tube docking, and it is not docked firmly. By applying this anti-loosening quick docking structure to the drone, not only can the drone and the carbon tube be quickly docked quickly and easily, but also ensure that the carbon tube can be firmly locked in the connected state to reduce the risk of loosening.

Claims

1. A carbon tube anti-loosening quick docking structure for drones, characterized in that: It comprises a first docking module (1), a second docking module (2), a locking tongue (3), a locking tongue base (4), a locking ring (5) and a compression spring (7); The first docking module (1) is plugged into the interior of the second docking module (2); The locking tongue base (4) is sleeved on the first docking module (1); The locking ring (5) is threadedly connected to the locking tongue base (4) and is used to lock the two docking modules after the first docking module (1) and the second docking module (2) are docked. The lock tongue (3) is embedded in the inside of the lock tongue base (4) by means of rivets, and is used to hook the locking ring (5) after locking; The compression spring (7) is arranged between the lock tongue base (4) and the lock tongue (3) and is used to give the lock tongue (3) a downward force to control the compression tongue to lock the locking ring (5).

2. The carbon tube anti-loosening quick docking structure for unmanned aerial vehicles according to claim 1, characterized in that: A first limiting cylinder (6) is fixedly connected to the outer wall of the locking tongue base (4), and the lower end of the compression spring (7) is fixedly installed inside the first limiting cylinder (6).

3. The carbon tube anti-loosening quick docking structure for unmanned aerial vehicles according to claim 1, characterized in that: The bottom of the locking tongue (3) is fixedly connected to a second limiting cylinder (8), and the upper end of the compression spring (7) is fixedly mounted inside the second limiting cylinder (8).

4. The carbon tube anti-loosening quick docking structure for unmanned aerial vehicles according to claim 1, characterized in that: A limiting groove (9) is provided on the outer wall of the first docking module (1), and a convex strip (10) is provided inside the second docking module (2), and the convex strip (10) is inserted into the limiting groove (9).

5. The carbon tube anti-loosening quick docking structure for unmanned aerial vehicles according to claim 1, characterized in that: A fixing plate (11) is fixedly mounted on the locking tongue (3), and a rubber sheet (12) is bonded to the fixing plate (11).

6. A drone, characterized in that: It includes the carbon tube anti-loosening quick docking structure for unmanned aerial vehicles as described in claim 1 or 5.

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