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특허 상세정보

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내보내기 페이스북 공유 카카오톡 공유

Real time performance monitoring of gas turbine engines

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G06F-015/20    G06F-015/32   
미국특허분류(USC) 364/551 ; 364/431 ; 73/116
출원번호 US-0923950 (1978-07-13)
발명자 / 주소
  • Bernier Joseph L. (Issaquah WA) Kamber Peter W. (Hawi HI)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 129  인용 특허 : 3
초록
▼

A real-time gas turbine engine monitoring system is disclosed which includes a digital processor that utilizes a set of scalar coefficients and the current value of various engine operating parameters to predict the current value of a set of engine performance parameters. The actual values of these performance parameters are monitored and compared with the predicted values to supply deviation or error signals to monitoring logic which provides an indication of faults within the digital processor, within the sensor units which provide the actual values of...

대표
청구항
▼

A system for monitoring at least one performance parameter of a gas turbine engine installation comprising: first sensor means for supplying a signal representative of the current value of each monitored performance parameter; second sensor means for supplying a first plurality of signals representative of the current values of an associated plurality of operating parameters of the engine installation being monitored, said plurality of signals being selected so that a signal [Figure] provides a current estimate of each monitored performance parameter whe...

이 특허에 인용된 특허 (3)

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