Structural monitoring system for helicopter rotor components
First Claim
1. A system for determining a structural condition of a portion of a helicopter rotor assembly, comprising:
- a piezoelectric sensor that is adapted to be supported on a portion of the rotor assembly and that provides a sensor signal indicative of stress waves in the portion of the rotor assembly;
a signal processor that processes the sensor signal and provides an output signal having at least one characteristic that is indicative of the content of the sensor signal, the signal processor including a demodulator portion that demodulates the sensor signal to thereby generate an envelope representation of the sensor signal; and
a signal analyzer that receives the envelope representation output signal and determines the structural condition based upon the output signal characteristic.
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Accused Products
Abstract
A system for monitoring the structural condition of a helicopter rotor assembly component includes a piezoelectric sensor. Acoustic emission signal techniques allow for recognizing the relatively high frequency stress waves associated with the propagation of cracks or defects in a rotor assembly component. A signal conditioner processes the sensor signal and provides an output signal that includes at least one characteristic that is indicative of the content of the sensor signal and, therefore, the structural condition of the item of interest. A signal analyzer utilizes the output signal from the signal processor to determine the structural condition of the component.
66 Citations
14 Claims
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1. A system for determining a structural condition of a portion of a helicopter rotor assembly, comprising:
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a piezoelectric sensor that is adapted to be supported on a portion of the rotor assembly and that provides a sensor signal indicative of stress waves in the portion of the rotor assembly;
a signal processor that processes the sensor signal and provides an output signal having at least one characteristic that is indicative of the content of the sensor signal, the signal processor including a demodulator portion that demodulates the sensor signal to thereby generate an envelope representation of the sensor signal; and
a signal analyzer that receives the envelope representation output signal and determines the structural condition based upon the output signal characteristic. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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10. A method of determining a structural condition of a portion of a helicopter rotor assembly, comprising the steps of:
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(A) attaching a piezoelectric sensor to a portion of the rotor assembly;
(B) detecting stress waves in the portion using the sensor;
(C) generating a stress signal indicative of the detected stress waves;
(D) demodulating the stress signal to generate an output signal that is an envelope representation of the stress signal and has at least one characteristic indicative of the content of the stress signal;
(E) determining the structural condition of the portion based upon the output signal characteristic. - View Dependent Claims (11, 12, 13, 14)
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Specification