Small UAV canopy
A small unmanned aerial vehicle and umbrella canopy technology, applied in the field of umbrella canopy, can solve problems such as affecting the appearance of the aircraft, increasing flight resistance, etc., and achieve the effect of reducing weight
Active Publication Date: 2012-07-25
CHENGDU AIRCRAFT INDUSTRY GROUP
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Problems solved by technology
The protrusion itself affects the appearance of the aircraft and increases flight resistance.
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Abstract
The invention discloses an umbrella hatch cover of a small unmanned aerial vehicle parachute recovery system. The umbrella canopy is composed of a front cover of the umbrella canopy and a rear cover of the umbrella canopy. The open double umbrella canopy makes the front and rear umbrella hanger joints all placed inside the fuselage, and the rear cover of the umbrella canopy uses a limit cloth to limit the opening angle and reduce the flight resistance. The split double umbrella canopy reduces the rigidity requirements for the umbrella canopy. The umbrella canopy is made of carbon fiber composite material with a honeycomb sandwich structure, which can reduce the weight by 60% compared with the aluminum alloy canopy canopy.
Description
Small unmanned aerial vehicle canopy canopy technical field The present invention relates to the canopy cover of a kind of small unmanned aerial vehicle parachute recovery system. Especially when it comes to parachuting small drones Split double umbrella hatch for recovery system. Background technique Parachute recovery is the commonly used recovery mode of small unmanned aerial vehicles. The recovery umbrella generally passes through the three umbrella belts and the three belts on the fuselage. There are two umbrella hanging joints, including two front hanging points and one rear hanging point. In order to ensure stability, the three hanging points are separated by a relatively large distance. An umbrella cabin is arranged between the front and rear hanging points, and an umbrella bag is placed in the umbrella cabin. The canopy is single open, its rear edge is hinged to the fuselage, and the front The end is locked by the locking and releasing mechanism of the can...
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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/14B64D17/80
Inventor 李景虎朱丹田刚
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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