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특허 상세정보

Aircraft flight instrument display system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G01C-023/00    G06K-015/20    G01C-021/00   
미국특허분류(USC) 340/27NA ; 116/DIG ; 43 ; 244/181 ; 340/721
출원번호 US-0936275 (1978-08-23)
발명자 / 주소
  • Miller Harry (Scottsdale AZ) Narveson Parm L. (Phoenix AZ) Hancock William R. (Phoenix AZ) Hsu Joseph P. (Phoenix AZ)
출원인 / 주소
  • Sperry Corporation (New York NY 02)
인용정보 피인용 횟수 : 86  인용 특허 : 3
초록

Apparatus for providing an integrated display of flight instrument parameters on the screen of a single cathode ray tube is presented. The synthetically generated symbology provides the pilot with an integrated display of substantially all aircraft attitude and flight path command and control parameters including attitude and magnetic heading, barometric and radiometric attitude, vertical spread, critical take-off speeds, true airspeed and Mach airspeed, flight path angle, flight director path control commands, and mode annunciation for the flight direct...

대표
청구항

Display apparatus for aircraft for indicating to the pilot the pitch and roll attitude of the aircraft comprising: (a) means defining a display field of view including a reference index generally in the center of said field and having the general shape of an aircraft and comprising a fuselage portion and wing portions laterally extending therefrom, (b) means for providing a horizon defining line in said field and including means responsive to the pitch and roll attitude of said craft for correspondingly positioning said horizon line relative to said refe...

이 특허를 인용한 특허 (86)

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