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특허 상세정보

Controlling aircraft using thrust differential trim

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-031/06    G05D-001/08    B64C-015/02    B64D-045/00   
출원번호 US-0184196 (2016-06-16)
등록번호 US-10005561 (2018-06-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    General Electric Company
인용정보 피인용 횟수 : 0  인용 특허 : 18
초록

Systems and methods for stabilizing an aircraft in response to a yaw movement are provided. In one embodiment, a method includes detecting a yaw movement of the aircraft. The yaw movement can cause a front portion of the aircraft to move towards a first side of the aircraft. The method can further include, in response to the yaw movement, initiating a trim process resulting in a thrust differential. The trim process can include increasing thrust in one or more engines on the first side of the aircraft and decreasing thrust in one or more engines on a sec...

대표
청구항

1. An aircraft comprising: one or more first engines located on a first side of the aircraft;one or more second engines located on a second side of the aircraft;a rudder;a computing system comprising one or more processors and one or more memory devices located on the aircraft, the one or more memory devices storing instructions that when executed by the one or more processors cause the one or more processors to perform operations comprising: detecting a rudder deflection on a first side of the aircraft; andperforming a trim process in response to the ru...

이 특허에 인용된 특허 (18)

  1. McCollum James H. (Cedar Rapids IA) Forquer Gary E. (Cedar Rapids IA). Aircraft autopilot with yaw control by rudder force. USP1991024992713.
  2. Beaufrere, Henry L.. Aircraft backup control. USP2013038393583.
  3. Beaufrere, Henry L.. Aircraft backup control. USP2011098016243.
  4. Bacon, Peter William; Tucker, David Roy; McLoughlin, Adam John; Coleman, David. Aircraft flight surface control system. USP2005036860452.
  5. Watts John. Airplane pirouette steering system. USP1998015704568.
  6. Croston Leon J. (Rt. 1 ; Box 892 Bois d\Arc MO 65612). All wing aircraft. USP1992015082204.
  7. Marino, Mark G.; Tillotson, John K.; Kosht, Danial L.. Cogless motor driven active user interface haptic feedback system. USP2010077759894.
  8. Nowlan, Daniel Ralph. Differential throttling control enhancement. USP2015048998131.
  9. Burken John J. ; Burcham ; Jr. Frank W. ; Bull John. Emergency multiengine aircraft system for lateral control using differential thrust control of wing engines. USP2000086102330.
  10. McCuen Michael S. (Kirkland WA). Full authority engine-out control augmentation subsystem. USP1990064935682.
  11. Deck Timothy D. (Renton WA) Lochtie David W. (Bellevue WA). Method and apparatus for providing a dynamic thrust asymmetry rudder compensation command with no direct thrust measurem. USP1997085657949.
  12. George Washington Bennett ; Sridhar Adibhatla ; Matthew William Wiseman. Methods and apparatus for trimming engine control systems. USP2002106459963.
  13. Firuz,Guner; Jaeger,Michael H.; Agate,Robert M.; Bresley,William M.. Methods and systems for automatically controlling aircraft takeoff rolls. USP2008047364121.
  14. Hanlon, Casey; Kern, James I.; Smith, Douglas C.; Cowling, David. Motor balanced active user interface assembly. USP2010047701161.
  15. Shepler, Angela J.. Turbine engine thrust scheduling. USP2014038682562.
  16. Shapiro, Daniel R.; Eggold, David Paul. Variable maximum commandable roll rate for directional control during engine-out rolling maneuver. USP2013048423206.
  17. Eggold, David P.; Shapiro, Daniel R.; Gardner, Kyle J.. Varying engine thrust for directional control of an aircraft experiencing engine thrust asymmetry. USP2013018352099.
  18. Eggold, David P.; Shapiro, Daniel R.; Gardner, Kyle J.. Varying engine thrust for directional control of an aircraft experiencing engine thrust asymmetry. USP2014128918235.