Rapid dismounting and mounting structure of functional modules of unmanned aerial vehicle and unmanned aerial vehicle

A functional module, UAV technology, applied in the field of UAV, can solve the problems of complicated disassembly and installation process, time-consuming and so on

Pending Publication Date: 2017-12-26
GUANGZHOU DINGFEI AEROSPACE TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

like figure 1 As shown in the middle part A, the connection between different functional modules and the UAV body is usually locked by screws and nuts. The disassembly and installation process is complicated and time-consuming.

Method used

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  • Rapid dismounting and mounting structure of functional modules of unmanned aerial vehicle and unmanned aerial vehicle
  • Rapid dismounting and mounting structure of functional modules of unmanned aerial vehicle and unmanned aerial vehicle
  • Rapid dismounting and mounting structure of functional modules of unmanned aerial vehicle and unmanned aerial vehicle

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Embodiment Construction

[0031] The present invention provides a quick disassembly and assembly structure for functional modules of an unmanned aerial vehicle, which realizes convenient and quick installation and replacement of functional modules.

[0032] A quick disassembly and assembly structure of the functional module of the drone of the present invention comprises:

[0033] Quick release male head, quick release female head and movable deadbolt assembly;

[0034] The quick release male head includes a sliding part, the quick release female head is provided with a chute, and the movable lock tongue assembly includes a lock tongue;

[0035] The sliding part can slide along the chute, so that the quick release male head can slide relative to the quick release female head;

[0036] There is a notch on the outer peripheral wall where the slider is embedded into the chute, and the lock tongue can be selectively inserted into or disengaged from the notch. When the lock tongue is inserted into the notc...

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Abstract

The invention provides a rapid dismounting and mounting structure of functional modules of an unmanned aerial vehicle, which can be used for conveniently and rapidly mounting and replacing the functional modules. The rapid dismounting and mounting structure of the functional modules of the unmanned aerial vehicle, provided by the invention, comprises a rapid dismounting male head, a rapid dismounting female head and a movable spring bolt assembly, wherein the rapid dismounting female head comprises a sliding groove; the rapid dismounting male head comprises a sliding part; the movable spring bolt assembly comprises a spring bolt; the sliding part slides along the sliding groove; a notch is formed in an outer circumference wall, which is embedded into the sliding groove, of the sliding part; the movable spring bolt can be selectively embedded into or released from the notch.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a quick disassembly structure for functional modules of an unmanned aerial vehicle. The embodiment of the present invention also relates to an unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aerial vehicle operated by radio remote control equipment or its own program control device, which first appeared in the 1940s. [0003] The drone includes a drone body and one or more functional modules. The functional modules include cameras of various specifications, spiral wings of various specifications, battery packs of various specifications, and auxiliary modules of various specifications. Various functional modules. Such as figure 1 As shown in the middle part A, the connection between different functional modules and the UAV body is usually locked by screws and nuts. The disassembly and installation p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/00B64C27/08B64D47/00
CPCB64C1/00B64C27/08B64D47/00B64U10/10
Inventor 汪建伟刘建勋周平和
Owner GUANGZHOU DINGFEI AEROSPACE TECH CO LTD
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