Aluminum alloy material design verification method for airworthiness certification

An aluminum alloy material, design verification technology, applied in the field of aluminum alloy material design verification

Pending Publication Date: 2020-05-12
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0010] In view of this, in order to solve at least one technical problem in the prior art, the present invention provides an aluminum alloy material design verification method for airworthiness certification

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  • Aluminum alloy material design verification method for airworthiness certification
  • Aluminum alloy material design verification method for airworthiness certification

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Embodiment Construction

[0025] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Apparently, the described embodiments are some, but 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.

[0026] Features and exemplary embodiments of various aspects of the invention are described in detail below. In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be apparent, however, to one skilled in the art that the present invention may be practice...

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Abstract

The invention provides an aluminum alloy material design verification method for airworthiness certification, which comprises the following steps: matching airworthiness verification parameters of analuminum alloy material with a verification database Q1: when the airworthiness verification parameters of the aluminum alloy material are successfully matched with the verification database Q1, determining that the aluminum alloy material passes verification; when the airworthiness verification parameters of the aluminum alloy material are not successfully matched with the verification database Q1, matching the airworthiness verification parameters of the aluminum alloy material with the general standard database Q2, and when the airworthiness verification parameters of the aluminum alloy material are successfully matched with the general standard database Q2, determining that the aluminum alloy material passes verification; and when the airworthiness verification parameters of the aluminum alloy material are not successfully matched with the general standard database Q2, and when the airworthiness verification parameters of the aluminum alloy material are successfully matched with the basic global database Q3, determining that the aluminum alloy material passes verification. According to the embodiment of the invention, the airworthiness verification efficiency of the aluminum alloy material can be greatly improved, the reliability is high, the reliability can be improved, and the examination efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of civil aircraft airworthiness, in particular to an aluminum alloy material design verification method for airworthiness certification. Background technique [0002] The metal materials used on aircraft mainly include aluminum alloy, steel, titanium alloy and copper alloy. Among them, aluminum alloys mainly include 2024, 2124, 7075, 7050, 7475 and other commonly used aluminum alloy grades with excellent performance, etc., and high-performance aluminum alloys mainly include 7150, 7055, 2524, 2026 and 2024HDT. [0003] After research, the applicant knows that the materials selected for civil aircraft must comply with the relevant provisions of the Airworthiness Regulations. The selection of materials should consider the requirements of airworthiness, the materials have passed the necessary tests, have certain experience in use, and meet the requirements of the corresponding material specifications. In terms...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F16/2455G06F16/21
CPCG06F16/2455G06F16/211
Inventor 李晨
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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