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Maintenance method based on aircraft structure health monitoring

A technology for health monitoring and aircraft structure, applied in data processing applications, forecasting, calculations, etc., can solve problems such as waste of cost and frequent maintenance

Active Publication Date: 2017-02-22
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The existing technology usually adopts after-the-fact maintenance and regular maintenance. In this way, sometimes it is not possible to repair the aircraft that has failed or cracked in time, and sometimes it may be repaired frequently, which wastes costs.

Method used

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  • Maintenance method based on aircraft structure health monitoring
  • Maintenance method based on aircraft structure health monitoring
  • Maintenance method based on aircraft structure health monitoring

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Embodiment Construction

[0049] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a maintenance method based on aircraft structure health monitoring. The maintenance method based on aircraft structure health monitoring comprises a step 1 of establishing an aircraft database of aircraft condition data; a step 2 of computing, by simulation, the life consumption of an aircraft in the aircraft database and the probability distribution of cracks in a flight process; a step 3 of establishing a maintenance model, classifying the maintenance of an aircraft group according to the operation state of the aircraft group, and classifying the maintenance into first-level maintenance, second-level maintenance and third-level maintenance according to the operation status of the aircraft group; a step 4 of according to the actual operating state of the aircraft group, performing corresponding maintenance in the first-level maintenance, the second-level maintenance and the third-level maintenance on respective aircrafts. The maintenance method based on aircraft structure health monitoring is used for the aircraft group, fully excavate the life potential of the aircraft group in the case of ensuring the normal task of the aircraft group and avoid unnecessary maintenance.

Description

technical field [0001] The invention relates to the technical field of aircraft structure fatigue strength, in particular to a maintenance method based on aircraft structure health monitoring. Background technique [0002] Glossary: [0003] Retention rate: In an aircraft group, at least the aircraft that can perform tasks immediately (or can perform tasks when required) account for the ratio of aircraft in the aircraft group, that is, the aircraft that can fly account for the aircraft that cannot fly (due to Aircraft that are out of flight due to maintenance, failure, damage, etc.). [0004] People pay more and more attention to the safety, reliability, fault diagnosis and prediction, health management and maintenance guarantee of modern aircraft. Fault diagnosis and health monitoring refers to using as few sensors as possible to collect various data information of the system, using various intelligent reasoning algorithms to evaluate the health status of the aircraft, pr...

Claims

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Application Information

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IPC IPC(8): G06Q10/04
CPCG06Q10/04
Inventor 宋恩鹏洪海明周丽君顾宇轩张音旋
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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