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특허 상세정보

System for controlling roll and yaw of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/22   
미국특허분류(USC) 244/195 ; 244/228 ; 244/194 ; 244/196
출원번호 US-0320094 (1989-01-09)
우선권정보 FR-0008870 (1987-06-24)
국제출원번호 PCT/FR88/00329 (1988-06-20)
§371/§102 date 19890109 (19890109)
국제공개번호 WO-8810458 (1988-12-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 32  인용 특허 : 4
초록

System for controlling roll and yaw of an aircraft. The system includes a device capable of elaborating, from electric signals respectively representative of the position of a first voluntary actuation member, the rolling speed, the attitude, the yaw speed, the sideslip and of the position of a second voluntary actuation member, a single electrical order for roll control formed by a linear combination of the electric signals. There is a device capable of elaborating, from the same electric signals, an electrical order for yaw control formed by a linear c...

대표
청구항

System for controlling roll and yaw of an aircraft (1) comprising roll control surfaces (8, 9) actuated from a first voluntary actuation member (14) and a rudder (11) actuated from a second voluntary actuation member (15), via a mechanical transmission (24), said first and second voluntary actuation members (14, 15) being associated with transducers (37, 39-41) delivering respectively first and second electrical signals depending on the position of said members, said aircraft comprising in addition means (43, 47) capable of delivering third, fourth, fift...

이 특허를 인용한 특허 피인용횟수: 32

  1. Recksiek,Martin; Rechter,Harald; Besing,Wolfgang. Adaptive flap and slat drive system for aircraft. USP2006057048234.
  2. Lam, Michael; Cole, Greg. Aircraft wing structure and control system. USP2017129846432.
  3. Pohl,Ulrich; Thomas,Carsten; Lulla,Christian; Kloenne,Martin. Apparatus for driving and adjusting flaps hinged to an aircraft. USP2007067226020.
  4. Carl,Udo; V��tter,Axel. Apparatus for the adjustment of horizontal stabilizers for aircraft. USP2008127464896.
  5. Whitmore Stephen A.. Closed-form integrator for the quaternion (euler angle) kinematics equations. USP2000056061611.
  6. Ferro, Daniel. Device and method for assisting in the management of an engine failure on an aircraft. USP2012048155803.
  7. Johnson, Andrew T.; Hanlon, Casey; Potter, Calvin C.. Distributed flight control surface actuation system. USP2009077556224.
  8. Parks, Robert. Ducted spinner for engine cooling. USP2009077559191.
  9. Burcham ; Jr. Frank W. ; Burken John J. ; Le Jeanette. Emergency flight control system using one engine and fuel transfer. USP2000106126111.
  10. Cline, Paul J.; Huynh, Neal V.; Inderhees, Leonard J.; Orgun, Munior; Smith, Mark H.; Oleson, Alexander Craig. Enhanced rudder control system. USP2005086923405.
  11. Wingett, Paul T.; Potter, Calvin C.; Hanlon, Casey; Benson, Dwayne M.. Flight control surface actuation system with redundantly configured and lockable actuator assemblies. USP2009107607611.
  12. Hagerott, Steven G.; Hammer, James L.; Ciholas, Philippe A.; Palmer, Mark W.. Flight control system. USP2014058725321.
  13. Hagerott, Steven G.; Hammer, James L.; Ciholas, Phillippe A.; Palmer, Mark W.. Flight control system. USP2016059340278.
  14. Ciholas, Philippe A.; Palmer, Mark W.. Flight control systems. USP2013038401716.
  15. Parks,Robert. Inbound transition control for a tail-sitting vertical take off and landing aircraft. USP2009037506837.
  16. Ciholas, Philippe A.; Palmer, Mark W.. Manual and computerized flight control system with natural feedback. USP2013028380364.
  17. Ezerzere, Pierre; Puig, Stéphane. Method and device for automatically detecting a lateral dissymetry of an aircraft. USP2013058447444.
  18. Boe, Regis; Chatrenet, Dominique. Method and device for detecting a lateral dissymmetry of an aircraft. USP2012058190309.
  19. Delannoy, Stéphane; Bertin, Thierry. Method and device for piloting an aircraft about a piloting axis. USP2012038141824.
  20. Puig, Stephane; Byzery, Romeo. Method and device for reducing on an aircraft lateral effects of a turbulence. USP2012078219266.
  21. David Burson FR. Method for determining a minimum control speed for an aircraft. USP2002096453221.
  22. Klingensmith Wallace Neil. Multi-thrustered hover craft. USP2001076260796.
  23. Conway Robert ; Strong Edward. Personnel guided aerial delivery device. USP1999055899415.
  24. Ezerzere, Pierre; Puig, Stéphane; Calderara, Fabien. Process and device for optimising the performance of an aircraft in the presence of a lateral dissymmetry. USP2013098527116.
  25. Gautier Jean-Pierre,FRX ; Ortega Jean-Marc,FRX. Process and device for the control of the rudder of an aircraft. USP2001036206329.
  26. Parks,Robert. System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft. USP2008107441724.
  27. Parks,Robert; Led��,Jean Charles; Drela,Mark. System and method for controlling engine RPM of a ducted fan aircraft. USP2008047364115.
  28. Garnaud,Christian; Fernandez,Brice. System for controlling the operation of at least one aircraft engine. USP2007037188008.
  29. Panxika Larramendy FR. System for the yaw control of an aircraft. USP2002036352223.
  30. Parks, Robert; Ledé, Jean-Charles. Vibration isolation engine mount system and method for ducted fans. USP2011088001764.
  31. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2013128620492.
  32. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E.. Yaw damping system and method for aircraft. USP2014108874286.