Locking structure and unmanned aerial vehicle

Abstract

The embodiment of the invention provides a locking structure and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The locking structure is used for fixedly locking and connecting a first part and a second part which are hinged to each other in the unmanned aerial vehicle. The locking structure comprises a hook assembly and a lock pin assembly, the hook assembly comprises a lock catch, and the lock pin assembly comprises a bayonet lock. The hook assembly is used for being installed on the first part, and the lock pin assembly is used for being installed on the second part. And one part of the bayonet lock is positioned between the first part and the second part and is clamped with or separated from the lock catch. When the lock catch is clamped with the bayonet lock, the first part can be fixed relative to the second part, and when the lock catch is separated from the bayonet lock, the first part can move relative to the second part. When the locking structure is used for connecting a winglet and a wing, the locking or unlocking of the winglet and the wing on the unmanned aerial vehicle can be realized through the clamping or separation ofthe lock catch and the bayonet lock, so that the locking difficulty of the winglet is greatly reduced, the operation time of unfolding and folding the winglet relative to the wing is shortened, and the maneuverability of whole machine assembly is improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular, to a locking structure and an unmanned aerial vehicle. Background technique [0002] At present, the winglets of fixed-wing or compound-wing UAVs are hinged to the wings by means of hinges. So that the winglet can rotate relative to the wing, so as to be in an unfolded state or a folded state. [0003] When the winglet is in the unfolded state relative to the wing, it is currently locked and fixed by screws so that the winglet is in the unfolded locked state. However, when the screws are actually locked and assembled, they are prone to problems of misalignment or oblique locking, resulting in difficulties in disassembly and assembly. Contents of the invention [0004] The purpose of the present invention includes, for example, to provide a locking structure and a drone. The locking structure can avoid the problem of difficult disassembly and assembly of screws ...

AI Technical Summary

Problems solved by technology

However, when the screws are actually locked and assembled, they are prone to problems of misalignment or oblique locking, which makes disassembly and assembly difficult

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