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특허 상세정보

Method and system for controlling the elevator assemblies of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00   
미국특허분류(USC) 244/75R ; 244/87 ; 244/228
출원번호 US-0094831 (1987-09-09)
우선권정보 DE-3631089 (1986-09-12); DE-3632068 (1986-09-20); DE-3638818 (1986-11-13)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 24  인용 특허 : 0

A fly-by-wire control system for the elevator assemblies of an aircraft is equipped with a mechanical auxiliary control (8) and with a synchronizing coupling (10). The electrical control links connecting the controlling computers to the elevator drives are each equipped with an override mechanism (4,2). A mechanical cable link (9) of the auxiliary mechanical control (8) connects a pilot operated mechanical control member such as a pitch control wheel having a detent to the respective override mechanism. This combination makes sure that the pilot initiate...


A method for controlling elevator assemblies of an aircraft, comprising the following steps: (a) normally supplying identical electrical flight control signals in parallel through two electrical control units each including an override mechanism arranged in series between each electrical control unit and respective mechanical control links to a plurality of drive means for each of said elevator assemblies, (b) supplying, in an emergency, mechanically generated control signals through dual mechanical control links to each of said override mechanisms, (c) ...

이 특허를 인용한 특허 피인용횟수: 24

  1. Recksiek,Martin; Rechter,Harald; Besing,Wolfgang. Adaptive flap and slat drive system for aircraft. USP2006057048234.
  2. Pohl,Ulrich; Thomas,Carsten. Aircraft flap or slat drive system with redundant drives and shaft drive lines. USP2006057051975.
  3. Ouellette, Benoit; Duchesne, Sophie; Lecoq, Frederic. Aircraft sidestick priority and dual input control logic. USP2017069690291.
  4. Pohl,Ulrich; Thomas,Carsten; Lulla,Christian; Kloenne,Martin. Apparatus for driving and adjusting flaps hinged to an aircraft. USP2007067226020.
  5. Yoeli, Raphael. Apparatus for generating horizontal forces in aerial vehicles and related method. USP2010057717368.
  6. Carl,Udo; V��tter,Axel. Apparatus for the adjustment of horizontal stabilizers for aircraft. USP2008127464896.
  7. Yoeli, Raphael. Control flows and forces in VTOL vehicles. USP2013078496200.
  8. Yoeli, Raphael. Ducted fan VTOL vehicles. USP2010127857253.
  9. Yoeli, Raphael. Ducted fan VTOL vehicles. USP2010107806362.
  10. Yoeli, Raphael. Ducted fan VTOL vehicles. USP2014018622335.
  11. Yoeli, Raphael. Ducted fan for VTOL vehicles with system and method to reduce roll moments. USP2014118876038.
  12. Yoeli,Rafi. Ducted fan vehicles particularly useful as VTOL aircraft. USP2007107275712.
  13. Yoeli, Raphael. Ground effect vanes arrangement. USP2011098020804.
  14. Carton, Mathieu; Debusschere, Pierre; Albugues, Laurent. Method and system for controlling the flight of an aircraft with respect to the pitch axis. USP20180710023301.
  15. Fukada, Yoshiki. Method of lift control of aircraft and system therefor. USP2004046722616.
  16. Chaduc, Bruno; Grohmann, Boris; Tempier, Christophe. Primary flight controls. USP2014118888036.
  17. Gautier, Jean-Pierre; Peransin-Delage, Cecile. Process and control system for an aircraft control surface actuated by multiple hydraulic jacks and with modular power. USP2003116651930.
  18. Gautier Jean-Pierre,FRX ; Ortega Jean-Marc,FRX. Process and device for the control of the rudder of an aircraft. USP1998085791596.
  19. DuRant,Cecil John. Servo mounting system for direct drive of an aircraft control surface. USP2007067229046.
  20. Grohmann, Boris; Buro, Thomas. System and a method for controlling pitching stabilizer means of an aircraft. USP2017059643717.
  21. Yoeli, Raphael. VTOL vehicle with coaxially tilted or tiltable rotors. USP2013018342441.
  22. Yoeli, Rafi. Vehicles particularly useful as VTOL vehicles. USP2010097789342.
  23. Yoeli,Rafi. Vehicles particularly useful as VTOL vehicles. USP2007077246769.
  24. Yoeli, Raphael. Wall effects on VTOL vehicles. USP2014098833692.