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Aircraft

A technology of aircraft and installation space, applied in the field of aircraft, can solve problems such as insufficient carrying capacity, unreasonable aircraft structure design, and unstable operation of aircraft

Active Publication Date: 2021-04-20
GUANGZHOU XAIRCRAFT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In related technologies, the structural design of the aircraft is unreasonable, and there are problems of unstable operation of the aircraft and insufficient carrying capacity

Method used

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  • Aircraft
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Embodiment Construction

[0045] 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.

[0046] In describing the present invention, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "top", "bottom", "inner", "outer", " The orientation or positional relationship indicated by "left", "right", etc. is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, are constructed...

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Abstract

The invention discloses an aircraft. The aircraft comprises a rack, a first mounting frame and a functional module. The rack comprises a top plate and a bottom plate, the top plate is provided with a first through hole and a second through hole, and the bottom plate is provided with a third through hole and a fourth through hole. The first mounting frame is clamped between the top plate and the bottom plate, a first mounting space and a second mounting space are formed in the first mounting frame, the first mounting space and the second mounting space are arranged in a spaced mode in the front-back direction, and the first mounting space is opposite to the first through hole and the third through hole; and the second mounting space is opposite to the second through hole and the fourth through hole. Part of the function module is accommodated in the first mounting space. According to the aircraft, the rack is constructed by arranging the bottom plate and the top plate which are distributed at intervals, and the second mounting frame and the first mounting frame are arranged between the bottom plate and the top plate, so that the stability and the balance of the aircraft can be improved, the rigidity and the supporting capacity of the rack can be improved, and the reliability of the aircraft is further improved.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft. Background technique [0002] With the development of aircraft, because of its advantages of flexible maneuverability, quick response, unmanned flight, and low operation requirements, it has attracted a lot of attention and has been applied in many fields such as agriculture and exploration. [0003] Due to the limitation of space layout, various parts of the aircraft are arranged in different positions of the aircraft. In related technologies, the structural design of the aircraft is unreasonable, and there are problems of unstable operation of the aircraft and insufficient carrying capacity. Contents of the invention [0004] The present application proposes an aircraft, which has the advantages of high stability, good balance, and strong bearing capacity. [0005] According to an aircraft according to an embodiment of the present invention, the aircraft inclu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/00B64C1/06
CPCY02T50/40
Inventor 徐智芹肖锭锋
Owner GUANGZHOU XAIRCRAFT TECH CO LTD