Wavelet Extraction of Impact Vibration Frequency Component and Fault Analysis for a Twine Spool Aero-Engine

Noise and weak symptom give rise difficulties to aero-engine vibration monitoring and faults diagnosis.The conventional methods in time or spectrum domain are not so effective for it is hard to detect some kinds of fault symptoms.After measuring the data in an aero-engine on the ground,its time-frequency characteristics under different working conditions were analyzed.First,the signals were analyzed using Morlet wavelet and then the frequency component could be extracted from their time-frequency plane.Some impact components were obvious in the time frequency plane which indicated that some faults might occur in the rotor system.They were located in the band of bearing characteristic frequencies.Second,the signal was decomposed using harmonic wavelet whose resolving capability is high in both time and frequency domain in the bearing characteristic frequencies.Then the components of different frequencies were obtained by harmonic wavelet.Energy of the signal was concentrated in some frequency band.From these results of the harmonic wavelet analysis in the bearing characteristic frequencies,the kind of fault can be determined easily.