The invention discloses a vibration component
decomposition and
resonance area identification method based on blade tip timing
original data, and relates to the field of blade vibration state monitoring. In order to solve the defects that an existing blade tip timing test method cannot realize
online analysis and cannot automatically identify a
resonance area, the method comprises the following steps: acquiring blade tip
timing data by adopting a blade tip timing probe; the vibration displacement of the
tip position of the rotating blade is obtained by subtracting the actual
arrival time of the rotating blade from the theoretical time and combining the rotating speed of the tip of the rotating blade: constructing a blade tip vibration
signal model, selecting a blade tip timing
signal of the blade to carry out sparse auxiliary
decomposition, setting optimization parameters and the maximum number of iterations, and calculating the vibration displacement of the
tip position of the rotating blade. Obtaining
decomposition results of the synchronous vibration
signal component and the asynchronous vibration signal component; and carrying out automatic identification on a
resonance region, and respectively obtaining region identification results of synchronous resonance and asynchronous resonance. The method is mainly used for
online analysis of blade tip timing
original data and automatic resonance area identification.