The invention discloses an acoustic monitoring method,
system, medium and equipment for the near stall condition of an aircraft compressor, and the method comprises the steps: carrying out the synchronous collection of
sound pressure time domain signals of multiple channels of an
aviation compression system; adding a rectangular window to the multi-channel
sound pressure time-domain
signal, and constructing an acoustic time-domain
signal segment to monitor the current operation state of the
aviation compression system; performing
fast Fourier transform on the multichannel acoustic
time domain signal segment in the
current time domain window to form a plurality of
sound pressure frequency spectrums, judging whether a plurality of single-tone characteristic frequencies which are non-integer multiples of the current rotation frequency exist in the sound pressure frequency spectrums or not, and constructing an orthogonal Fourier
transfer matrix based on the installation position and the highest circumferential
modal order, and judging whether the order difference of the characteristic acoustic mode under each characteristic frequency is the rotation frequency multiple difference of the corresponding characteristic frequency, calculating the acoustic mode amplitude corresponding to each
broadband frequency component, drawing an acoustic mode
spectrogram, and judging whether a mode bright band exists at the
cut-off frequency boundary in the acoustic mode
spectrogram.