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특허 상세정보

Multiaxis redundant fly-by-wire primary flight control system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00   
미국특허분류(USC) 364/434 ; 318/564 ; 244/194
출원번호 US-0893339 (1992-06-03)
발명자 / 주소
  • Buus Henning (Woodinville WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 88  인용 특허 : 0
초록

A redundant, multi-channel fly-by-wire control system for use in an aircraft is disclosed. The system includes a left flight control channel (60), a center flight control channel (80) and a right flight control channel (90). Each control channel is capable of flying the aircraft in the event the other two channels fail. Included within each control channel is an actuator controller electronics unit (ACE (62, 82, 92)), which transmits a series of pilot control transducer signals to a set of primary flight computers (64, 84, and 94). The primary flight com...

대표
청구항

A fly-by-wire flight control system for an aircraft that monitors the position of pilot controls and produces flight surface commands that control the movement of a plurality of flight control surfaces on the aircraft to adjust the attitude of the aircraft about roll pitch, and yaw directional axes, the system comprising: (a) a plurality of transducers associated with the pilot controls, each of said plurality of transducers producing a signal indicative of the position of a corresponding pilot control; (b) a plurality of isolated flight control channels...

이 특허를 인용한 특허 (88)

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