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Emergency flight control system using one engine and fuel transfer

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-017/10    B64C-015/02   
미국특허분류(USC) 24/407.5R ; 24/405.1 ; 24/413.5C
출원번호 US-0112067 (1998-07-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kusmiss
인용정보 피인용 횟수 : 16  인용 특허 : 18
초록
▼

A system for emergency aircraft control uses at least one engine and lateral fuel transfer that allows a pilot to regain control over an aircraft under emergency conditions. Where aircraft propulsion is available only through engines on one side of the aircraft, lateral fuel transfer provides means by which the center of gravity of the aircraft can be moved over to the wing associated with the operating engine, thus inducing a moment that balances the moment from the remaining engine, allowing the pilot to regain control over the aircraft. By implementin...

대표
청구항
▼

[ What is claimed is:] [1.] A navigational control for an aircraft having an engine and the ability to laterally transfer fuel between fuel tanks, comprising:a thrust control, said thrust control controlling thrust of the engine;a lateral fuel transfer control, said lateral fuel transfer control controlling lateral transfer of fuel between said fuel tanks to control and shift a center of gravity of the aircraft; anda coordinator, said coordinator coupled to said thrust control and said lateral fuel transfer control, said coordinator coordinating said thr...

이 특허에 인용된 특허 (18)

  1. Orgun Munir (Woodinville WA) McRoberts Timothy C. (Bothell WA) Virdee Arvinder S. (Kirkland WA). Aircraft automatic landing system with engine out provisions. USP1992055113346.
  2. Martorella Romeo P. (Dix Hills NY). Aircraft precision approach control system. USP1991035000404.
  3. Roberts Lawrence T. (Kent WA) Strom Thomas H. (Williamsburg VA). All-axis control of aircraft in ultra deep stall. USP1981044261533.
  4. Bell Douglas A. (Glendale AZ). Apparatus for controlling fuel transfers in a distributed fuel tank system. USP1994065321945.
  5. Spitzer ; Robert E. ; May ; III ; Fred W.. Engine out control system for STOL aircraft. USP1978084106730.
  6. Moore M. Samuel (Northridge CA) Paluka Charles F. (Northridge CA). Engine power management system. USP1980014185460.
  7. Grafwallner Franz (Tegernsee DEX) Luger Peter (Hohenkirchen-Siegertsbrunn DEX) Peller Helmuth (Hohenkirchen-Siegertsbrunn DEX) Muller Martin (Hohenkirchen-Siegertsbrunn DEX) Malyshev Valentin V. (Mos. Fuel supply system. USP1997085660358.
  8. Vardaman Billy G. (Albany GA) Meyer Corwin W. (Ocala FL). Fuel system for Canard aircraft. USP1990044913380.
  9. Secchiaroli Lawrence N. (Stratford CT) Cresiski ; Jr. Raymond C. (Milford CT) Wilson Thomas P. (Trumbull CT). Fuel transfer system for aircraft. USP1990064932609.
  10. McCuen Michael S. (Kirkland WA). Full authority engine-out control augmentation subsystem. USP1990064935682.
  11. Hudson William A. (Fountain Valley CA) Levin Mark L. (Hermosa Beach CA). Integrated aircraft fuel thermal management system. USP1988104776536.
  12. Diamond Edmond D. (Huntington CT) Maciolek Joseph R. (Milford CT) Kingston Leo (Stratford CT). Multi-axis force stick, self-trimmed aircraft flight control system. USP1983124420808.
  13. Buus Henning (Woodinville WA). Multiaxis redundant fly-by-wire primary flight control system. USP1996025493497.
  14. Kelley Wendell W. (Newport News VA). Pitch attitude stabilization system utilizing engine pressure ratio feedback signals. USP1981054266743.
  15. Buisson Dominique (Villemur FRX) Moline Augustin (Pibrac FRX). Process and system for determining the longitudinal position of the center of gravity of an aircraft provided with an ad. USP1990064937754.
  16. Farineau Jacques (Toulouse FRX). System for controlling roll and yaw of an aircraft. USP1990104964599.
  17. Farineau Jacques (Toulouse FRX) Larramendy Panxika (Toulouse FRX). System for integrated pitch and thrust control of an aircraft. USP1992075127608.
  18. Dahl Robert M. (108-A Castle Rock Rd. Walnut Creek CA 94598-4515). Wireless flight control system. USP1996075531402.

이 특허를 인용한 특허 피인용횟수: 16

  1. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torisionally flexible wing. USP2015099120555.
  2. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torsionally flexible wing. USP2017099764819.
  3. Kendall, Greg T.; Morgan, Walter R.. Aircraft control system. USP2010097802756.
  4. Lisoski,Derek L.; Kendall,Greg T.. Aircraft control system. USP2007047198225.
  5. Kulkarni, Nilesh V.; Kaneshige, John T.; Krishnakumar, Kalmanje S.; Burken, John J.. Aircraft system modeling error and control error. USP2012108285659.
  6. De Magalhães Gomes, Ierko. Asymmetry-proof multi-engine aircraft. USP20190310227138.
  7. Neto, Rubens Domecildes. Continuous fuel management system for automatic control of aircraft center of gravity. USP2012078226040.
  8. Wolfram, Jens; Greiser, Steffen; Seher-Weiss, Susanne. Determination of the center of gravity. USP2014108874357.
  9. Poster, Scott. Dual-path fluid injection jet. USP2014108869941.
  10. Lemaignan, Benoît; Mathieu, Gérard. Method and device for controlling the thrust of a multi-engine aircraft. USP2013018359129.
  11. Delporte, Martin; Essadouni, Malika. Method and device for correcting the lateral dissymmetry of an aircraft. USP2012078231082.
  12. Delporte, Martin; Lambeaux, Sophie; Ronceray, Didier; Legier, Jean-Philippe. Method and device for limiting the roll command of an aircraft as a function of a thrust asymmetry. USP2011118050808.
  13. Paillard, Pierre; Larcher, David. Method and system for maneuvering an aircraft by shifting its center of gravity. USP2013108548721.
  14. Rupe,Kurt A.. Methods and apparatus for fuel control using inertial measurement data. USP2006037010399.
  15. Cogan, Bruce R.. Propulsion controlled aircraft computer. USP2010057711455.
  16. Ishiba, Masatsugu. Vertical takeoff and landing aircraft. USP2009087568655.

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