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Performance parameter based civil aircraft engine starting system health monitoring method

A technology for engine starting and engine application in the direction of engine testing, machine/structural component testing, measuring devices, etc. It can solve the problems of not extracting valuable information, not using data mining, singleness, etc., to achieve easy access, Optimize the repair plan and spare parts management, and reduce the effect of sudden failure

Inactive Publication Date: 2019-12-13
SHANGHAI AIRCRAFT CUSTOMER SERVICE +1
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  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

However, airlines currently adopt a single visualization method without using relevant technologies of data mining, and cannot extract valuable information from massive operational data.
[0005] In summary, there is a lack of a non-parametric modeling method in the prior art to evaluate the performance of the engine starting system, which can perform real-time quantitative evaluation of the performance of the engine starting system without the need for a physical model of the system or the use of system failure or failure data , effectively reduce the sudden failure of the engine starting system, and prevent the occurrence of super-economical maintenance

Method used

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  • Performance parameter based civil aircraft engine starting system health monitoring method
  • Performance parameter based civil aircraft engine starting system health monitoring method
  • Performance parameter based civil aircraft engine starting system health monitoring method

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Embodiment Construction

[0036] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with specific embodiments.

[0037] Since the actual aircraft engine starting system adopts an after-the-fact maintenance strategy, troubleshooting and maintenance are performed only when engine 1 and engine 2 fail. Therefore, the method provided by this embodiment can be used for early warning of starting system failure, and at the same time combined with the concept of fleet management, the maintenance and troubleshooting of the engine starting system can be reasonably arranged.

[0038] The embodiment of the present invention provides a method for health monitoring of civil aircraft engine starting system based on performance parameters, the flow chart is as follows figure 1 shown, including:

[0039] S1. Extract feature values ​​according to the actual operating environment ...

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Abstract

The invention discloses a performance parameter based civil aircraft engine starting system health monitoring method and relates to the technical field of equipment state monitoring. On the basis of aircraft QAR data, a performance parameter baseline model of important parameters in a civil aircraft engine starting system is established with a data mining technology; then, a covariance matrix of test samples is calculated; finally, the similarity and the mahalanobis distance between the test samples and the baseline model are obtained with a mahalanobis distance technology, the health state ofthe system is represented with the distance, and the purpose of health monitoring is achieved. The method is applied to the civil aircraft engine starting system, the problem of insufficiency of performance evaluation means of the aircraft engine starting system is solved, the performance state of the engine starting system can be accurately evaluated, early warning is timely given at the early stage of failure of the engine starting system, and unplanned accidents are reduced; and besides, performance evaluation data come from existing civil aircraft QAR data and have higher practicability and operability.

Description

technical field [0001] The invention relates to the technical field of equipment state monitoring, in particular to a method for monitoring the health of a civil aircraft engine starting system based on performance parameters. Background technique [0002] Health monitoring is the basis for automatic fault diagnosis and condition-based maintenance of the aircraft engine starting system. It can not only greatly reduce unplanned maintenance, improve the economy and timeliness of aircraft maintenance; on-wing time. In view of the relevance and coupling of the accessory systems of the engine, the health monitoring of the starting system can also ensure the safe operation of the engine body and avoid the phenomenon of engine over-rotation and engine starting suspension due to the failure of the starting system. Systematic implementation of health monitoring has great practical significance. [0003] At present, on the route, due to the complexity and marginality of the starting...

Claims

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Application Information

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IPC IPC(8): G01M15/00
CPCG01M15/00
Inventor 黄加阳刘翠高鑫磊孙见忠晏震乾陈金
Owner SHANGHAI AIRCRAFT CUSTOMER SERVICE
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