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Fixed wing unmanned aerial vehicle with rapidly mountable and demountable wings

A fixed-wing and unmanned aerial vehicle technology, applied in the field of aircraft, can solve the problems of complex wing disassembly and assembly, and achieve the effect of convenient operation, simple structure and accurate positioning

Pending Publication Date: 2018-08-24
南京航天猎鹰飞行器技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem solved by the present invention is to provide a fixed-wing unmanned aerial vehicle that can quickly disassemble and assemble the wings, so as to solve the complicated problem of disassembling and assembling the wings of the current fixed-wing aircraft

Method used

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  • Fixed wing unmanned aerial vehicle with rapidly mountable and demountable wings
  • Fixed wing unmanned aerial vehicle with rapidly mountable and demountable wings
  • Fixed wing unmanned aerial vehicle with rapidly mountable and demountable wings

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Embodiment Construction

[0017] In order to illustrate the technical scheme and technical purpose of the present invention, the present invention will be further introduced below in conjunction with the accompanying drawings and specific embodiments.

[0018] combine figure 1 , figure 2 , a fixed-wing UAV that can quickly disassemble the wings of the present invention includes a fuselage 10, two symmetrical fuselages 10 arrange wings 9, and a disassembly mechanism 100; The connecting end is provided with a wing 91; the fuselage 10 is provided with a deck 11 and a box 8; the box 8 is a U-shaped plate structure, and the box 8 and the deck 11 are connected to form an insert between the two. Wing 91 is plugged into the slot; the cover box 8 is provided with a first installation groove 81, and the insertion wing 91 is provided with a second installation groove 92; after the insertion wing 91 is inserted into the slot, the first installation groove 81 and The second installation groove 92 overlaps;

[0...

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Abstract

The invention discloses a fixed wing unmanned aerial vehicle with rapidly mountable and demountable wings. The fixed wing unmanned aerial vehicle includes a fuselage, two wings symmetric about the fuselage, and disassembly and assembly structures. The wings' ends connected to the fuselage are equipped with plug wings. The fuselage is internally equipped with a cabin plate and a casing box. The casing box is a U-shaped plate structure, the casing box and the cabin plate are connected, and slots for plugging of the plug wings are formed between the casing box and the cabin plate. The casing boxis equipped with first mounting grooves, and the plug wings are equipped with second mounting grooves. After the plug wings are plugged into the slots, the first mounting grooves overlap with the second mounting grooves, and the disassembly and assembly structures are utilized to fix the plug wings and the casing box. The unmanned aerial vehicle provided by the invention is convenient to mount anddemount, can complete disassembly and assembly of the wings without additional tools, has a simple structure, is easy to operate, and can realize quick disassembly and assembly.

Description

technical field [0001] The invention belongs to the technical field of aircraft, in particular to a fixed-wing unmanned aerial vehicle whose wings can be quickly disassembled. Background technique [0002] Due to its small size, high cost performance, and strong combat survivability, UAVs will play an important role in future air combat. With the widespread use of fixed-wing UAVs, the disadvantages of traditional disassembly methods relying on tools and cumbersome assembly make the pre-flight preparation and subsequent maintenance work extremely complicated. In order to facilitate users to replace and repair by themselves, many manufacturers have introduced the tool-free quick disassembly design into the design of the aircraft platform. However, in the prior art, the realization of the quick-release structure is complicated. In order to realize the quick-release requirement, the connection strength between components is often sacrificed, and a high-strength connection canno...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/26
CPCB64C1/26
Inventor 缪炎王雨卿
Owner 南京航天猎鹰飞行器技术有限公司
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