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특허 상세정보

Method and device for controlling the thrust of a multi-engine aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G05D-001/00   
미국특허분류(USC) 701/008; 701/004; 701/014; 701/099; 701/100; 701/123; 340/963; 340/966; 244/076R; 244/183; 244/184
출원번호 US-0162774 (2007-03-08)
등록번호 US-8359129 (2013-01-22)
우선권정보 FR-06 02249 (2006-03-15)
국제출원번호 PCT/FR2007/000415 (2007-03-08)
§371/§102 date 20080730 (20080730)
국제공개번호 WO2007/104851 (2007-09-20)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 3  인용 특허 : 15
초록

A method and device control the thrust of a multi-engine aircraft. At least one engine command is determined by a command determining unit, with the determined command commanding each engine that has not failed to deliver a thrust substantially equal to a reduced thrust value. A command application unit is configured to apply the determined command to each aircraft engine that has not failed. The reduced thrust value is determined, by a weight determining device, according to the current weight of the aircraft and according to a reduced thrust value FOEI...

대표
청구항

1. A method for controlling the thrust of a multi-engine aircraft, said method comprising: c) determining at least one engine command, by a command determining unit, wherein said at least one engine command commands each engine of said aircraft that has not failed to deliver a thrust substantially equal to a reduced thrust value; andd) applying, by a command application unit, said command determined in step c) to each of the engines of the aircraft that has not failed, wherein, said reduced thrust value determined in step c) is determined according to:a)...

이 특허에 인용된 특허 (15)

  1. Summerfield Leslie R. (Bristol GB2). Aircraft engine emergency control system. USP1995085440490.
  2. Orgun Munir (Woodinville WA) Nguyen Dung D. (Edmonds WA). Apparatus and methods for controlling commanded operation of an aircraft within a predetermined flight parameter limit. USP1992035096146.
  3. Larramendy Panxika,FRX ; Zaccaria Patrick,FRX ; Clavel Thierry,FRX ; Garavel Fran.cedilla.ois,FRX. Device for controlling the thrust of a multi-engine aircraft. USP1999075927655.
  4. Burcham ; Jr. Frank W. ; Burken John J. ; Le Jeanette. Emergency flight control system using one engine and fuel transfer. USP2000106126111.
  5. Rice Robert W. (Sandy Hook CT) Sweet David H. (Tequesta FL). Engine failure monitor for a multi-engine aircraft having partial engine failure and driveshaft failure detection. USP1994115363317.
  6. Martin Anthony N. (Simsbury CT). Engine speed control apparatus. USP1989104875168.
  7. Huynh, Kiet T.. Engine thrust management?new design architecture. USP2005056886786.
  8. McCuen Michael S. (Kirkland WA). Full authority engine-out control augmentation subsystem. USP1990064935682.
  9. Hernandez-Diaz Jorge H. (Minillas Sta. Box 41267 Santurce PR 00940). Method and apparatus for limiting adverse yaw-induced roll during engine failure in multiengine aircraft. USP1989114884205.
  10. David Burson FR. Method for determining a minimum control speed for an aircraft. USP2002096453221.
  11. Vladimir Ziberov A.,RUX ; Alexander Koupziyanov V.,RUX ; Oleg Kosolapov A.,RUX. Method of intelligence support of aircraft crew. USP1998045739769.
  12. Gates, Patrick Joseph; Saario, Teuvo. One-engine-inoperative training method and system. USP2011098025503.
  13. Gautier Jean-Pierre,FRX ; Ortega Jean-Marc,FRX. Process and device for the control of the rudder of an aircraft. USP2001036206329.
  14. Pettigrew,James L.; Boeshart,Mitchell T.. System and method for monitoring aircraft engine health and determining engine power available, and applications thereof. USP2006047031812.
  15. Lambregts, Antonius A.. Total energy based flight control system. USP1985084536843.