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Detachable fixed wing unmanned aerial vehicle

A technology for dismantling and fixing UAVs, which is applied to rotorcraft, unmanned aircraft, fuselages, etc., can solve the problems of low efficiency, inconvenient disassembly, complex structure of fixed-wing UAVs, etc., and reduce the burden , Simple structure, good convenience effect

Pending Publication Date: 2022-02-08
SHANGHAI FUKUN AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the fixed-wing UAV is disassembled, and the fixed-wing UAV is transported after disassembly, but the structure of the fixed-wing UAV is relatively complicated, and the disassembly efficiency is low, which is very inconvenient

Method used

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  • Detachable fixed wing unmanned aerial vehicle
  • Detachable fixed wing unmanned aerial vehicle
  • Detachable fixed wing unmanned aerial vehicle

Examples

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Embodiment

[0055] figure 1 A schematic structural view of a fixed-wing unmanned aerial vehicle according to an embodiment of the present invention is shown, the unmanned aerial vehicle includes a fuselage, a tail cone 20, a first wing 31 and a second wing 32, wherein: one side of the fuselage Connected to the first wing 31, the other side of the fuselage is connected to the second wing 32, the section of the tail cone 20 and the fuselage is provided with a fixed frame 21, the fixed frame 21 is connected with described tail vertebra 20 and fuselage. Here, the UAV is disassembled into several parts, and several parts are designed to be detachable. The UAV can be transported by packing, which is very convenient. The specific detachable structure is as follows:

[0056] figure 2 Shows the structural representation of the tail vertebra of the embodiment of the present invention, image 3 shows a structural schematic diagram of a fuselage section of an embodiment of the present invention,...

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Abstract

The invention discloses a detachable fixed wing unmanned aerial vehicle, which comprises a fuselage, a tail cone, a first wing and a second wing, wherein one side of the fuselage is connected with the first wing, the other side of the fuselage is connected with the second wing, a fixed frame is arranged at the cross section of the tail cone and the fuselage, and the tail cone and the fuselage are connected into a whole through the fixed frame; more than one bayonet and a third spring button are arranged on the section of the machine body; the fixed frame comprises a plurality of cross rods and more than one third bolt, the plurality of cross rods form a cross section frame, and the more than one third bolt is fixed on the cross section frame; one third bolt in the more than one third bolt is clamped on one bayonet in the more than one bayonet, and the inner wall of a cross rod of the fixed frame is buckled on the third spring button. According to the invention, the unmanned aerial vehicle is designed to be detachable, wherein the wings and the fuselage are rapidly detached, so that boxing and transportation are facilitated, and good convenience is achieved.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a detachable fixed-wing unmanned aerial vehicle. Background technique [0002] Fixed-wing UAVs have the characteristics of long battery life and high-altitude flight, and have been widely used in surveying and mapping, geology, petroleum, agriculture, forestry and other industries; It takes up a lot of space and is troublesome to transport. [0003] At present, the fixed-wing UAV is disassembled, and the fixed-wing UAV is transported after disassembly, but the structure of the fixed-wing UAV is relatively complicated, and the disassembly efficiency is low, which is very inconvenient. Contents of the invention [0004] The purpose of the present invention is to overcome the deficiencies of the prior art. The present invention provides a detachable fixed-wing unmanned aerial vehicle. The unmanned aerial vehicle is designed to be detachable, and the wings and fuselage can ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/26B64C1/30B64C1/06B64C27/26B64C39/02
CPCB64C1/26B64C1/30B64C1/0685B64C27/26B64C39/02B64U10/25B64U30/10B64U30/20B64U50/19
Inventor 刘十一谢陵胡汇
Owner SHANGHAI FUKUN AVIATION TECH CO LTD
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