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Fault-tolerant actuating system for adjusting flaps of an aircraft, comprising adjustment kinematics with a fixed pivot, and a method for monitoring an actuating system

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/38
출원번호 US-0991174 (2009-05-05)
등록번호 US-8814085 (2014-08-26)
우선권정보 DE-10 2008 022 092 (2008-05-05)
국제출원번호 PCT/EP2009/003219 (2009-05-05)
§371/§102 date 20101123 (20101123)
국제공개번호 WO2009/135653 (2009-11-12)
발명자 / 주소
  • Richter, Martin
  • Fleddermann, Andreas
출원인 / 주소
  • Airbus Operations GmbH
대리인 / 주소
    Ingrassia Fisher & Lorenz P.C.
인용정보 피인용 횟수 : 6  인용 특허 : 33

초록

A fault-tolerant actuating system with at least one flap, adjustable on a respective wing of an aircraft, and with a control and monitoring device, includes: drive devices that are functionally connected to the control and monitoring device, with one of these drive devices in each case being associa

대표청구항

1. A fault-tolerant actuating system, comprising: at least one flap, adjustable on a respective wing of an aircraft;a control and monitoring device;drive devices that are functionally connected to the control and monitoring device, each drive device being associated with a respective flap, each driv

이 특허에 인용된 특허 (33)

  1. Matsui, Gen; Tanaka, Teruaki; Yamamoto, Tsuyoshi, Actuator control apparatus.
  2. Andrew E. Uttley GB; Peter William Chambers GB; Nigel Blackwell GB; Brian Weller GB, Actuator system for aerospace controls and functions.
  3. Pohl,Ulrich; Thomas,Carsten, Aircraft flap or slat drive system with redundant drives and shaft drive lines.
  4. Bacon, Peter William; Tucker, David Roy; McLoughlin, Adam John; Coleman, David, Aircraft flight surface control system.
  5. Pohl,Ulrich; Thomas,Carsten; Lulla,Christian; Kloenne,Martin, Apparatus for driving and adjusting flaps hinged to an aircraft.
  6. Carl,Udo; V��tter,Axel, Apparatus for the adjustment of horizontal stabilizers for aircraft.
  7. Degenholtz, Arthur; Mayer, Edward; Vaghela, Naresh P., Arrangement and associated system having an actuator and a tubular flap-drive member about the actuator.
  8. Herzog Hans K. (Bellevue WA) Sakurai Seiya (Seattle WA), Avionic control system.
  9. Johnson, Andrew T.; Hanlon, Casey; Potter, Calvin C., Distributed flight control surface actuation system.
  10. White Albert H. (Wethersfield CT) Peck Robert E. (Prospect CT) Meyer Gene A. (W. Simsbury CT) Devanney Raymond H. (Winsted CT), Dual stepper motor actuator for fuel metering valve.
  11. Hanlon, Casey; Wingett, Paul T.; Potter, Calvin C., Electric flight control surface actuation system for aircraft flaps and slats.
  12. Wagner ; III Fred A., Extendable/retractable airfoil assembly for fixed wing aircraft.
  13. Miller Harry (Scottsdale AZ), Fail-safe dual channel automatic pilot with maneuver limiting.
  14. Elbert Ralph P. ; Hafner Michael A., Fault tolerant actuation system for flight control actuators.
  15. David W. Vos, Fault tolerant automatic control system utilizing analytic redundancy.
  16. Gillingham Gary D. ; Miles Gary L., Flap/slat actuation system for an aircraft.
  17. Wingett, Paul T.; Gaines, Louie T.; Evans, Paul S.; Kern, James I., Flight control actuation system.
  18. Collins, Andrew J., Flight control surface actuation system.
  19. Farley Brian,GBX ; Morgan Antony,GBX ; Mountney Arthur Derek,GBX ; Matthews Timothy Robert,GBX, Flight control surface actuation system.
  20. Wingett, Paul T.; Hanlon, Casey; Potter, Calvin C., Flight control surface actuator assembly including a free trial mechanism.
  21. Takats Imre J. (Bellevue WA) Aziz George W. (Seattle WA), Flight control system employing two dual controllers operating a dual actuator.
  22. Flatt,James E., Jam tolerant electromechanical actuation systems and methods of operation.
  23. Trikha, Arun K., Method and apparatus for controlling aircraft devices with multiple actuators.
  24. Lindstrom Jeffrey V. ; Reed R. David ; Platin Bradley E. ; Beyer Kevin W. ; Reusch David C., Method and apparatus for detecting skew and asymmetry of an airplane flap.
  25. Gleine Wolfgang,DEX ; Hilbig Reinhard,DEX ; Wendt Hans-Joachim,DEX, Method and apparatus for optimizing the aerodynamic effect of an airfoil.
  26. Edward Emaci ; Scott Wilkinson ; William Leden, Method and apparatus for sensing skews and disconnects of adjacent movable components.
  27. Ortega, Jean-Marc; Garcia, Jean-Pierre, Method and device for controlling an aircraft maneuvering components, with electrical standby modules.
  28. Urnes, Sr., James M.; Hood, Mark B., Method and system for in-flight fault monitoring of flight control actuators.
  29. Carl, Udo; Neumann, Uwe; Holert, Ben, Method for load limiting in drive systems for aircraft high lift systems.
  30. Buus Henning (Woodinville WA), Multiaxis redundant fly-by-wire primary flight control system.
  31. Takats Imre J. (Bellevue WA) Chenoweth Charles C. (Bellevue WA), Multiple-voting fault detection system for flight critical actuation control systems.
  32. Gardner, Conrad O., Supervisory control system for aircraft flight management during pilot command errors or equipment malfunction.
  33. Durandeau Michel,FRX ; Foch Etienne,FRX, System for controlling an aircraft control surface tab.

이 특허를 인용한 특허 (6)

  1. Brady, Michael; Winkelmann, Christoph, Actuation system for flight control surface.
  2. Rechsiek, Martin; Ellmers, Wilfried; Winkelmann, Christoph, Adjustment system of an aeroplane with an adjustable flap.
  3. Moser, Matthew A.; Finn, Michael R.; Thoreen, Adam, Control interface for leading and trailing edge devices.
  4. Richter, Martin, High lift system for an aircraft with two separate drive units.
  5. Catt, Christopher Joseph; Howard, Julia Ann, Method for diagnosing a speed brake system fault.
  6. Moser, Matthew A.; Finn, Michael R.; Gardner, Mark J.; Murphy, Robert M.; Thoreen, Adam, System and method for optimizing performance of an aircraft.
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