A kind of quick disassembly and assembly structure and UAV with the structure

A fast and component-based technology, applied in the field of unmanned aerial vehicles, can solve the problems of reduced flight efficiency and stability, inability to realize quick disassembly, inconvenient disassembly, etc., to achieve improved flight efficiency and stability, rapid disassembly and assembly, stable structure, and simple operation convenient effect
CN108891579BActive Publication Date: 2021-09-21GOERTEK ROBTICS CO LTD
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Patent Information

Authority / Receiving Office
CN ยท China
Patent Type
Patents(China)
Current Assignee / Owner
GOERTEK ROBTICS CO LTD
Publication Date
2021-09-21

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Abstract

The invention relates to a quick disassembly structure and an unmanned aerial vehicle with the structure. The quick disassembly structure includes a first component and a second component, wherein the first component is provided with at least two circumferentially distributed and movable A clamping piece, an elastic piece is provided between the clamping piece and the first member; the second member is provided with matching pieces not less than the number of the clamping piece; the above-mentioned quick disassembly structure is simple and convenient to operate, and can realize the connection between the first member and the second member. For the quick disassembly and assembly of the two components, in addition, at least two clamping parts are provided and distributed along the circumferential direction to realize clamping and locking with the matching parts from different directions, which can make the quick disassembly and assembly structure more stable.
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Description

technical field

[0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a quick disassembly structure and an unmanned aerial vehicle with the structure. Background technique

[0002] UAVs are getting deeper and deeper into the current social production due to their high efficiency, high mobility and safety. However, the current installation structure of the UAV foot bracket is relatively traditional. For example, the foot bracket and the fuselage are connected by fasteners such as screws or screws. The foot bracket and the fuselage are connected by a quick-release structure, but some structures that rely on springs in one direction will cause the vibration of the motor or the spring rebound caused by the unstable flight to cause the position of the foot bracket to appear during the operation of the whole machine. Vibration, when serious, will bring the whole machine to resonance, which will easily cause a great reduction in flight e...

Claims

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