Method for identifying failure state of rotor vibration signal of aircraft engine
A technology for aircraft engine and signal failure, applied in the testing of mechanical components, testing of machine/structural components, measuring devices, etc.
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[0035] Below in conjunction with accompanying drawing, content of the present invention is described in further detail:
[0036] General faults of aircraft engine rotors include: inner ring faults, outer ring faults, rolling element faults, unbalance faults. The method for identifying the fault state of the aircraft engine rotor vibration signal can identify these fault states, and the general process can be divided into two processes: offline and online: the offline process, that is, the engine rotor vibration data of the known fault category, through the method mentioned in the present invention Processing to obtain a trained classifier; online process, that is, to use the acceleration sensor on the aircraft to collect new vibration data from the engine rotor, and then use the method of vibration signal fault analysis to process the data and substitute it into the trained classifier, and finally Displays fault status results.
[0037] The method for identifying the fault st...
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