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
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[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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