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Quick disassembling device for mission loads of unmanned aerial vehicle

A technology for drones and missions, which is applied to unmanned aircraft, motor vehicles, aircraft parts, etc., can solve the problems of inconvenient disassembly of mission loads and potential safety hazards, and achieve convenient installation of load equipment, reduction of flight weight, and Easy and fast operation

Pending Publication Date: 2017-05-10
TIANXUN INNOVATION BEIJING TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The present invention is aimed at the problem of inconvenient disassembly of task loads and potential safety hazards, and researches and designs a quick dismountable, safe and reliable quick release device for unmanned aerial vehicle task loads

Method used

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  • Quick disassembling device for mission loads of unmanned aerial vehicle
  • Quick disassembling device for mission loads of unmanned aerial vehicle

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Embodiment Construction

[0019] The present invention is described in further detail now in conjunction with accompanying drawing. These drawings are all simplified schematic diagrams, which only illustrate the basic structure of the present invention in a schematic manner, so they only show the configurations related to the present invention.

[0020] Such as figure 1 and figure 2 The quick-release device for the mission load of the UAV shown in the figure is hung under the UAV through three hanging points. The front of the UAV has two symmetrically arranged hanging points, and one hanging point is set at the rear. The so-called hanging point is a bolt threaded on the lower part of the drone, and the nut of the bolt and a part of the stud protrude from the bottom of the drone.

[0021] The quick release device of the present embodiment comprises the load plate 1 that is used for fixing task load equipment, and task load is fixed on the lower surface of load plate 1, and a plurality of threaded hol...

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Abstract

The invention discloses a quick disassembling device for mission loads of an unmanned aerial vehicle. The quick disassembling device is hung under the unmanned aerial vehicle by three hanging points and comprises a loading plate for fixing the mission loads, wherein two front U-shaped hanging grooves with backward openings are arranged at the front part of the loading plate, and a rear U-shaped hanging groove with a backward opening is arranged at the rear part of the loading plate; a locking hook for locking the loading plate and the hanging points is arranged under the rear U-shaped hanging groove; the front end of the locking hook is in pin joint at the lower bottom surface of the loading plate, and the rear end of the locking hook is provided with a bending hook for blocking the hanging points from sliding out of the rear U-shaped hanging groove; one end of a locking spring is fixed on the loading plate and the other end of the locking spring is fixed on the locking hook; the locking hook is poked by a force in the tension direction of the locking spring, the hanging points are inserted into the three U-shaped hanging grooves, then the locking hook is loosened, the locking spring is reset to drive the locking hook to return, and the hanging point at the rear part is locked in the rear U-shaped hanging groove by the bending hook. The quick disassembling device disclosed by the invention has the advantages that the mission loads can be quickly disassembled according to the needs, and the fixing is firm, so that the risk of falling of the mission loads when in flying of the unmanned aerial vehicle is reduced.

Description

technical field [0001] The invention belongs to the technical field of aircraft design, and in particular relates to a quick release device for a mission load of an unmanned aerial vehicle. Background technique [0002] With the rapid development of UAV technology, more and more UAVs are applied to various industries to perform tasks, and the mounting equipment is also an indispensable tool for UAVs to perform tasks. The traditional drone’s mission load is fixed directly with the drone by screws. It is troublesome to disassemble when the load equipment needs to be replaced, and it may damage the equipment. Since the load equipment may be replaced at any time, it is generally not screwed to strengthen the fixation. , During the flight, the vibration of the aircraft may cause the screws to loosen and cause danger, causing unnecessary economic losses and even endangering personal safety. Contents of the invention [0003] The present invention is aimed at the problem of inco...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00
CPCB64D47/00B64U10/00
Inventor 王川王朔杨威
Owner TIANXUN INNOVATION BEIJING TECH CO LTD
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