Fuselage of unmanned aerial vehicle and unmanned aerial vehicle with fuselage

A technology for unmanned aerial vehicles and airframes, applied in the field of flight, can solve problems such as mutual interference between equipment, limited equipment functions, and inability to cope with various usage requirements, so as to improve assembly efficiency and shorten assembly time.

Pending Publication Date: 2021-01-29
GUANGZHOU XAIRCRAFT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Since the fuselage of the unmanned aerial vehicle contains a variety of equipment and wiring to realize various functions of the unmanned aerial vehicle, the structural design and layout of the unmanned aerial vehicle of the related technology are unreasonable, which leads to the occurrence of various equipment layouts in the fuselage. Mutual interference, or limited functions of some devices, will affect the overall performance of the UAV, affect the functionality and applicability of the UAV, and cannot meet a variety of usage needs

Method used

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  • Fuselage of unmanned aerial vehicle and unmanned aerial vehicle with fuselage
  • Fuselage of unmanned aerial vehicle and unmanned aerial vehicle with fuselage
  • Fuselage of unmanned aerial vehicle and unmanned aerial vehicle with fuselage

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Embodiment Construction

[0042] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0043] A fuselage 10 according to an embodiment of the present invention will be described below with reference to the drawings.

[0044] Such as Figure 1-Figure 10 As shown, the body 10 according to the embodiment of the present invention includes a body frame 111 , a lower cover 16 , a first electronic component 114 , a second electronic component 80 and a third electronic component 90 .

[0045] The fuselage frame 111 includes a first fixed frame 11 and a second fixed frame 12, the first fixed frame 11 is provided with a first stora...

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Abstract

The invention discloses a fuselage of an unmanned aerial vehicle and the unmanned aerial vehicle with the fuselage. The fuselage of the unmanned aerial vehicle comprises a fuselage frame comprising afirst fixing frame and a second fixing frame, a first storage cavity is formed in the first fixing frame, and a second storage cavity is formed in the second fixing frame; the first fixing frame and the second fixing frame are connected in parallel in the length direction of the fuselage; a lower cover is arranged on the bottom wall of the fuselage frame, and a wiring space is defined among the bottom wall of the second fixing frame, the side wall of the first fixing frame and the lower cover; a first electronic element is arranged at the top of the second fixing frame; a second electronic element is arranged in the second storage cavity and is positioned below the first electronic element; and a third electronic element is arranged on the lower cover and is positioned below the second electronic element. When in use, the electronic elements are convenient to install and arrange, the assembly efficiency of the fuselage is improved, and enough operation space and accommodating space areconvenient to reserve for connecting wire terminals among the electronic elements.

Description

technical field [0001] The present invention relates to the field of flight, in particular, to a fuselage of an unmanned aerial vehicle and an unmanned aerial vehicle having the fuselage of the unmanned aerial vehicle. Background technique [0002] Since the fuselage of the unmanned aerial vehicle contains a variety of equipment and wiring to realize various functions of the unmanned aerial vehicle, the structural design and layout of the unmanned aerial vehicle of the related technology are unreasonable, which leads to the occurrence of various equipment layouts in the fuselage. Mutual interference or limited functions of some devices will affect the overall performance of the UAV, affect the functionality and applicability of the UAV, and cannot meet a variety of usage needs. Contents of the invention [0003] The present invention aims to solve at least one of the technical problems existing in the prior art. For this reason, the present invention proposes a fuselage o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64C1/36
CPCB64C1/061B64C1/068B64C1/36
Inventor 梁杰肖锭锋
Owner GUANGZHOU XAIRCRAFT TECH CO LTD
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