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특허 상세정보

Reference system and method for diagnosing aircraft engine conditions

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G06F-015/20   
미국특허분류(USC) 364/42404 ; 364/55101 ; 364/554 ; 364/43101
출원번호 US-0379220 (1989-07-13)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 39  인용 특허 : 5
초록

An aircraft engine diagnostic apparatus is described. The diagnostic apparatus senses engine performance related parameters refers the data to a standard atmosphere condition and plots values relating to the functions of each engine performance related parameter with respect to other engine performance related parameters. The apparatus compares these actual engine operating parameter values with standard baselines for normal engines and calculates the deviation between the actual curve and the standard curve as referred engine diagnostic data (REDD), an ...

대표
청구항

A turbine engine diagnostic reference system for use with a turbine engine having performance related parameters and being subject to a plurality of causes of engine deterioration, comprising: sensing means, located at operable positions of said turbine engine, for detecting the engine performance related parameters; and processing means, electrically connected to said sensing means, for: (1) recording each sensed parameter as an actual function of another sensed parameter, (2) comparing the actual functions with predetermined standard baselines, (3) cal...

이 특허를 인용한 특허 피인용횟수: 39

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