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특허 상세정보

Process for the control of the control surfaces of an aircraft for the low speed compensation of a lateral path deviatio

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00    B64C-013/16   
미국특허분류(USC) 244/75R ; 244/76C ; 244/184 ; 244/90R
출원번호 US-0105498 (1993-08-11)
우선권정보 FR-0010038 (1992-08-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 19  인용 특허 : 0
초록

The present invention relates to a process for the automatic control of the control surfaces of an aircraft for the low speed compensation of a lateral path deviation, in which beyond a given deflection threshold (20) of the deflected rudder (17), there is a control of a deflection, proportional to the exceeding of the threshold, of the wing surfaces (13, 14) of one of the two wings (18), said wing being that on the side of the deflected rudder (17), so as to provide a drag supplement to said wing and therefore yaw on the aircraft. Application to the tak...

대표
청구항

Process for automatically controlling the control surfaces of an aircraft so as to compensate for lateral path deviation at low speed, with said aircraft having two main wings each of which includes several control surfaces with at least one aileron and one spoiler and said aircraft having a rudder for controlling yaw, comprising the steps of: detecting rudder deflection and the direction of said deflection; computing rudder deviation beyond a given deflection threshold; calculating a drag supplement proportional to the deflection of the rudder beyond sa...

이 특허를 인용한 특허 피인용횟수: 19

  1. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2007037185859.
  2. Harrigan,Jeffery S.; Beaufrere,Henry L.. Aerospace vehicle yaw generating systems and associated methods. USP2008057367530.
  3. Andre,Joan; Andrieu,Laurent. Aircraft provided with thrust reversers. USP2006097107757.
  4. Giesseler, Hans-Gerd. Aircraft with a device for directionally stabilizing the aircraft, computer program product and method for directionally stabilizing the aircraft. USP2016039274523.
  5. Wilson, Douglas L.; Brightwell, Julie R.; Beamis, Christopher P.. Autodrag function for glide slope control. USP2011118052095.
  6. Gast Mark E.. Autopilot/flight director overspeed protection system. USP1998115833177.
  7. Gast Mark E.. Autopilot/flight director underspeed protection system. USP1998055746392.
  8. Gast Mark E.. Autopilot/flight director underspeed protection system. USP1998115836546.
  9. Enzinger,Michael; Kordt,Michael. Device and method for damping at least one of a rigid body mode and elastic mode of an aircraft. USP2007087258307.
  10. Becker, Juergen. Flight control device for improving the longitudinal stability of an automatically controlled airplane and method of operating same. USP2004056729579.
  11. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W.. Horizontal tail load alleviation system. USP2013018342445.
  12. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W.. Horizontal tail load alleviation system. USP2014068752789.
  13. Joalland, Benoit; Delporte, Martin. Method and apparatus for improved lateral control of an aircraft on the ground during takeoff. USP2016039272770.
  14. Wildschek, Andreas; Hanis, Tomas. Method and apparatus for minimizing dynamic structural loads of an aircraft. USP2016099446837.
  15. Villaume,Fabrice; Duprez,Jean. Method and device for piloting an aircraft. USP2007127305285.
  16. Mathieu Gerard,FRX. Method for controlling an aeroplane control surfaces to counter ground lateral drift. USP2001066241183.
  17. Verde Preckler, Jorge Pablo; Vizarro Toribio, Jose Miguel. Stabilizing and directional-control surface of aircraft. USP2012048152097.
  18. Clark, Walter D.. System and method for controlling an aircraft. USP2003116641086.
  19. Najmabadi, Kioumars; Shivitz, William F.; Coleman, Edward Ernest; Ho, John Koon-hung; Johnson, Richard D.; Carver, William F.; Grubb, David W.; McIntosh, Robert James. Wing-body load alleviation for aircraft. USP2011098024079.