Unmanned aerial vehicle and fuselage assembly thereof

A component and fuselage technology, applied in the field of aircraft, can solve the problems of complex shell structure and heavy weight, and achieve the effects of simple internal and external structure, light weight and reduced manufacturing cost

Pending Publication Date: 2018-10-02
SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the embodiments of the present invention is to provide an unmanned aerial vehicle and its fuselage assembly, so as to solve the technical problems of complex structure and heavy weight of the fuselage assembly shell of the unmanned aerial vehicle in the prior art

Method used

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  • Unmanned aerial vehicle and fuselage assembly thereof
  • Unmanned aerial vehicle and fuselage assembly thereof
  • Unmanned aerial vehicle and fuselage assembly thereof

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Embodiment Construction

[0046] In order to facilitate the understanding of the present invention, the present invention will be described in more detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted that when an element is said to be "fixed" to another element, it may be directly on the other element, or there may be one or more intervening elements therebetween. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or one or more intervening elements may be present therebetween. The terms "vertical", "horizontal", "left", "right", "inner", "outer" and similar expressions are used in this specification for the purpose of description only.

[0047] Unless otherwise defined, all technical and scientific terms used in this specification have the same meaning as commonly understood by one of ordinary skill in the technical field of the invention. Terms used in the description of the pre...

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Abstract

The invention provides an unmanned aerial vehicle and a fuselage assembly thereof. The fuselage assembly comprises a shell, a bracket and an internal assembly piece. The shell is provided with an accommodating cavity. The bracket is accommodated in the accommodating cavity and connected with the shell. The internal assembly piece is mounted on the bracket. In the fuselage assembly, the shell doesnot need a fixing structure used for mounting the internal assembly piece, so that the internal and external structures of the shell are concise, low in weight, easy to machine and low in machining defect rate; and the high-quality appearance can also be obtained under the low-cost condition, so that the overall manufacturing cost of the fuselage assembly is reduced.

Description

【Technical field】 [0001] The invention relates to the field of aircraft, in particular to an unmanned aircraft and a fuselage assembly. 【Background technique】 [0002] Unmanned aerial vehicle, referred to as unmanned aerial vehicle (UAV), is a new concept equipment in rapid development, which has the advantages of flexible maneuvering, quick response, unmanned driving, and low operation requirements. The unmanned aerial vehicle is equipped with various types of sensors or camera devices through the gimbal, which can realize real-time image transmission and detection of high-risk areas. It is a powerful supplement to satellite remote sensing and traditional aerial remote sensing. [0003] Generally, the fuselage assembly of an unmanned aerial vehicle includes a first shell and a second shell, and internal assemblies in the fuselage assembly, such as printed circuit boards, etc., are fixed to the first shell and the second shell , the second shell is fastened to the first she...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06
CPCB64C1/061B64C1/069
Inventor 梁智颖
Owner SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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