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System and method for controlling an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00   
미국특허분류(USC) 244/075.R
출원번호 US-0930339 (2001-08-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Baker Botts L.L.P.
인용정보 피인용 횟수 : 6  인용 특허 : 16
초록
▼

A system for controlling an aircraft includes an airframe, a first airfoil, and a second airfoil. At least a portion of the first airfoil and the second airfoil are controllably deflectable so that, during a roll maneuver, the first airfoil generates increased lift and a consequent increased drag, and the second airfoil generates negative lift and a consequent increased drag, the increased lift and the decreased lift generating a roll moment, and the increased drag of the second airfoil producing a yaw moment that counteracts the yaw moment produced by t...

대표
청구항
▼

A system for controlling an aircraft includes an airframe, a first airfoil, and a second airfoil. At least a portion of the first airfoil and the second airfoil are controllably deflectable so that, during a roll maneuver, the first airfoil generates increased lift and a consequent increased drag, and the second airfoil generates negative lift and a consequent increased drag, the increased lift and the decreased lift generating a roll moment, and the increased drag of the second airfoil producing a yaw moment that counteracts the yaw moment produced by t...

이 특허에 인용된 특허 (16)

  1. Woodcock Robert R. (Sylmar CA). 90 degree rotation aircraft wing. USP1991034998689.
  2. Borzachillo Angelo (San Marcos CA). Aeroelastic control flap. USP1988034729528.
  3. Lam Lawrence Y. ; Lam Michael. Aileron for fixed wing aircraft. USP2000066079672.
  4. Gerhardt Heinz A. (Redondo Beach CA). Aircraft outboard control. USP1992105156358.
  5. Peters ; Jr. Spence E.. Aircraft structure to improve directional stability. USP2000086098923.
  6. Borzachillo Angelo (Torrance CA). Auxiliary flaperon control for aircraft. USP1979034146200.
  7. Burnham Robert W. (Seattle WA). Directional control device for aircraft. USP1984084466586.
  8. Whitaker ; Sr. Robert H. (Atlanta GA). Flight control device for airplanes. USP1984064455004.
  9. Lewis George E. (Renton WA). Maneuver load alleviation system. USP1989014796192.
  10. Codina George. Method and apparatus for countering asymmetrical aerodynamic process subjected onto multi engine aircraft. USP2000086095459.
  11. Mathieu Gerard,FRX. Method for controlling an aeroplane control surfaces to counter ground lateral drift. USP2001066241183.
  12. Farineau Jacques (Toulouse FRX). Pitch control system for aircraft. USP1992055112009.
  13. Rivron Vincent (Toulouse FRX) Vollard Ccile (Toulouse FRX). Process for the control of the control surfaces of an aircraft for the low speed compensation of a lateral path deviatio. USP1994125375793.
  14. Pohl Ulrich (Bremen DEX) Renken Juergen (Freyersen DEX). Segmentized flap system. USP1990014892274.
  15. Palmer Harry W. (P.O. Box 821 Denmark ME 04022). Torsional twist airfoil control means. USP1997105681014.
  16. Dahl Robert M. (108-A Castle Rock Rd. Walnut Creek CA 94598-4515). Wireless flight control system. USP1996075531402.

이 특허를 인용한 특허 피인용횟수: 6

  1. Clark, Walter Dennis. Aircraft with forward opening inlay spoilers for yaw control. USP2005056892982.
  2. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W.. Horizontal tail load alleviation system. USP2013018342445.
  3. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W.. Horizontal tail load alleviation system. USP2014068752789.
  4. Van De Kreeke, Marc; Cassein, Guillaume. Method and system for controlling an aircraft control surface. USP2005036863242.
  5. Sauvinet, Frederic. Method for improving roll steering of an aircraft and aircraft using same. USP2011037896288.
  6. 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.

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