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An aircraft fairing with impact resistance

A technology for impact resistance and aircraft, applied in the field of aircraft, can solve problems such as poor impact resistance, achieve the effects of good impact resistance, ensure safety, and increase resistance

Inactive Publication Date: 2020-02-04
JILIN INST OF CHEM TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to make up for the deficiencies of the prior art, and to provide an aircraft fairing with impact resistance, which has the advantage of good impact resistance and solves the problem of poor impact resistance of existing aircraft

Method used

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  • An aircraft fairing with impact resistance
  • An aircraft fairing with impact resistance
  • An aircraft fairing with impact resistance

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Embodiment Construction

[0034] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0035] see Figure 1-5, the present invention provides a technical solution: an aircraft fairing with impact resistance, comprising a cowl head 4, the right side of the cowl head 4 is fixedly connected with two symmetrical cowl bodies 11, between the two cowl bodies 11 The aircraft body 9 is placed between them, the right side of the aircraft body 9 is placed with a cover tail 7, the right side of each cover body 11 is fixedly connected with the left side of t...

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Abstract

The invention discloses an aircraft fairing with good impact resistance and a manufacturing method thereof, and relates to the technical field of aircrafts. The aircraft fairing comprises a cover head, wherein two symmetrical cover bodies are fixedly connected to the right side face of the cover head, an aircraft body is placed between the two cover bodies, and a cover tail is placed on the rightside of the aircraft body. The aircraft fairing with good impact resistance and the manufacturing method thereof have the functions of reducing the friction between the whole and the airflow, have theadvantages of good impact resistance, improve the overall buffer performance, further ensure the safety of the aircraft body, have the function of reducing the friction between the whole and the airflow, further improve the overall impact resistance, ensure the safety and integrity of the aircraft body, have the function of protecting the aircraft body, and have the advantage of ensuring the safety of the integrity of the aircraft body; and a foreign object is prevented from colliding with the aircraft body through a first port.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft fairing with impact resistance. Background technique [0002] The aerospace industry usually includes production enterprises and repair enterprises, as well as independent or affiliated research departments, design departments, sales departments, test and flight test bases and management departments. Most aerospace industry enterprises rely on their own technology and production conditions to produce some non-aerospace products. [0003] The fairing used to protect the aircraft in the aerospace industry, during the flight of the aircraft, the fairing will rub against the surrounding airflow, which is easy to cause damage, thus losing the protective effect on the aircraft and having poor impact resistance. Contents of the invention [0004] The object of the present invention is to make up for the deficiencies in the prior art, and to provide an aircraft fairing wi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C7/00B23P15/00
CPCB23P15/00B64C7/00
Inventor 刘东帅肖尧
Owner JILIN INST OF CHEM TECH
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