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Vibration monitoring system for aircraft engines

  • US 4,488,240 A
  • Filed: 02/01/1982
  • Issued: 12/11/1984
  • Est. Priority Date: 02/01/1982
  • Status: Expired due to Fees
First Claim
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1. Apparatus to monitor rotating machinery for incipient failures signalled by increased vibration at frequencies related to the frequency of rotation, comprising, in combination:

  • (a) sensing means connected to detect and signal vibrations of an element of rotating machinery;

    (b) tachometer means for detecting and signalling frequency of rotation of the rotating element;

    (c) clocking means coupled to receive said tachometer means signals for generating a predetermined number of sampling pulses for each rotation of the element;

    (d) sampling means coupled to said sensing means, and responsive to said sampling pulses for gating sensing means signal samples;

    (e) digital conversion means coupled to said sampling means for producing digital signals corresponding to and representative of samples of sensed element vibrations;

    (f) nonrecursive digital filter means coupled to said digital conversion means and operable in response to each digitized sample to produce digital signals corresponding to and representative of vibrations of the element occurring at the frequency of rotation; and

    (g) signal processing means connected to receive the output of said filter means for converting digital signals to analog signals and for generating a signal representative of a desired descriptor of the quantity represented by the digital filter output signal;

    whereby desired descriptor analog signals corresponding to and representative of periodic machine vibration can be displayed or further processed.

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