A Method for Evaluating the Validity of Vibration Monitoring Data of Helicopter Moving Parts
A technology for data validity and vibration monitoring, applied in the field of data processing, to achieve the effect of improving validity and versatility
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[0039] The method for evaluating the validity of vibration monitoring data of helicopter moving parts described in this embodiment, the specific steps are as follows:
[0040] S1, read the data of the vibration acceleration signal of a measuring point collected by the monitoring equipment, extract the time domain and frequency domain characteristic values in the vibration acceleration data of the measuring point through signal processing; detect the steady state of the engine The speed effective value Eng_CI_Vrms of the gas generator and the power turbine and the frequency division characteristic values Eng_CI_1st_AMP and Eng_CI_2st_AMP;
[0041] The speed effective value Eng_CI_Vrms is the root mean square value of the vibration speed signal, the Eng_CI_1st_AMP is the first-order frequency amplitude with the same frequency as the engine shaft, and the Eng_CI_2st_AMP is the second-order frequency amplitude with the same frequency as the engine shaft.
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