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Fixed wing unmanned aerial vehicle

A drone and fixed-wing technology, applied in the field of drones, can solve the problems of low landing precision of drones, difficulty in separating the wings from the fuselage, etc., and achieve high landing precision and little wind influence

Pending Publication Date: 2017-05-10
深圳市易飞方达科技有限公司
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

The relative position of the wing and the fuselage is generally fixed. When the stall is disassembled, the wing and the fuselage are difficult to separate, resulting in low landing accuracy of the UAV.

Method used

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  • Fixed wing unmanned aerial vehicle
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Embodiment Construction

[0021] In order to make the purpose, technical solution and advantages of the present invention clearer, the UAV according to the embodiment of the present invention will be further described below in conjunction with the accompanying drawings.

[0022] see figure 1 , The UAV according to the embodiment of the present invention includes a fuselage 10 , an electric propulsion mechanism 20 , a wing 30 , a vertical tail 40 , a flat tail 50 and a buffer package 60 . The electric propulsion 20 is arranged at the head of the fuselage 10 , the wings 30 are arranged at both sides of the fuselage 10 , the vertical tail 40 and the horizontal tail 50 are arranged at the tail of the fuselage 10 , and the buffer bag 60 is arranged at the bottom of the fuselage 10 . It can be understood that the UAV also includes other functional components, such as rudders, hatch covers, etc. To save space, these other functional modules are not described in detail below.

[0023] The fuselage 10 is forme...

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Abstract

A fixed wing unmanned aerial vehicle comprises a vehicle body, an electric propulsion mechanism arranged on the head of the vehicle body, wings arranged on the two sides of the vehicle body, and a horizontal tail arranged at the tail of the vehicle body. The wings are arranged on the vehicle body in a tool-free fast disassembly and assembly mode. During large-stall vertical landing, the wings can be taken off forwards along a chute of the vehicle body, energy of landing of the whole unmanned aerial vehicle is absorbed, so that according to stall decomposition technology of the fixed wing unmanned aerial vehicle provided by the invention, the influence of wind is small, and the landing precision is high.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle, in particular to a hand-throwing fixed-wing unmanned aerial vehicle. Background technique [0002] With the miniaturization and high integration of electronic loads, small electric drones, especially hand-thrown electric drones, are developing rapidly, and have applications in both military and civilian applications. The relative position of the wing and the fuselage is generally fixed. When the stall is disassembled, it is difficult to separate the wing and the fuselage, resulting in low landing accuracy of the UAV. Contents of the invention [0003] In view of this, the embodiments of the present invention provide a fixed-wing UAV with high landing accuracy. [0004] A fixed-wing unmanned aerial vehicle, which comprises a fuselage, an electric propulsion mechanism arranged at the head of the fuselage, wings arranged on both sides of the fuselage and a flat tail arranged at the tail of the fusela...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/38B64D45/06
CPCB64C3/38B64D45/06
Inventor 张会军
Owner 深圳市易飞方达科技有限公司
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