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Flight control actuation system

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-013/40
  • B64C-013/00
  • B64C-013/48
출원번호 US-0874729 (2004-06-22)
발명자 / 주소
  • Wingett,Paul T.
  • Gaines,Louie T.
  • Evans,Paul S.
  • Kern,James I.
출원인 / 주소
  • Honeywell International, Inc.
대리인 / 주소
    Ingrassia Fisher &
인용정보 피인용 횟수 : 27  인용 특허 : 10

초록

A flight control actuation system comprises a controller, electromechanical actuator and a pneumatic actuator. During normal operation, only the electromechanical actuator is needed to operate a flight control surface. When the electromechanical actuator load level exceeds 40 amps positive, the cont

대표청구항

What is claimed is: 1. A flight control actuation system for use in a flight control system comprising: an electromechanical actuator responsive to a control signal, for operating a flight control surface, the electromechanical actuator operable to supply a load signal representative of a load ther

이 특허에 인용된 특허 (10)

  1. Andrew E. Uttley GB; Peter William Chambers GB; Nigel Blackwell GB; Brian Weller GB, Actuator system for aerospace controls and functions.
  2. Bauer Claus,DEX, Airfoil with a landing flap having a flexible trailing edge.
  3. Jeffrey D. Rowe, Attitude estimation in tiltable body using modified quaternion data representation.
  4. Terp Leslie S. (Scottsdale AZ), Electropneumatic rotary actuator having proportional fluid valving.
  5. Durandeau Michel,FRX ; Foch Etienne,FRX, Hybrid control system for an aircraft aerodynamic surface.
  6. Irick Stephen C. (Hampton VA), Hydraulic actuator mechanism to control aircraft spoiler movements through dual input commands.
  7. Raymond Eugene T. (Kent WA), Load-adaptive hybrid actuator system and method for actuating control surfaces.
  8. Wingett Paul, Pressure vessel bottle mount.
  9. Durandeau Michel,FRX ; Foch Etienne,FRX, System for controlling an aircraft control surface tab.
  10. Royer Wilson M. ; Gucker Mark J., Vent valve with pressure relief.

이 특허를 인용한 특허 (27)

  1. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya, Actuation device positioning systems and associated methods, including aircraft spoiler droop systems.
  2. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
  3. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  4. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  5. Chantriaux, Eric; Chretien, Pascal, Aircraft comprising a distributed electric power unit with free wheels.
  6. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  7. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V., Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods.
  8. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V., Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods.
  9. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya, Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods.
  10. Lacy,Douglas S.; Beyer,Kevin W.; Brown,Stephen T.; Dees,Paul W.; Huynh,Neal V.; Kordel,Jan A.; Prow,Clayton A.; Sakurai,Seiya, Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods.
  11. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  12. Carl,Udo; V��tter,Axel, Apparatus for the adjustment of horizontal stabilizers for aircraft.
  13. Shriver, Michael H.; Stevens, John W., Electric motor clamping system.
  14. Waaramaa, Todd, Electromechanical decoupler.
  15. Hagerott, Steven G.; Hammer, James L.; Ciholas, Philippe A.; Palmer, Mark W., Flight control system.
  16. Hagerott, Steven G.; Hammer, James L.; Ciholas, Phillippe A.; Palmer, Mark W., Flight control system.
  17. Cremers, Joerg, Fuel management system.
  18. Spiller, Olaf, High lift system for an aircraft and method for detecting faults in a high lift system for an aircraft.
  19. Hejda, Zdenek, Hybrid electromechanical/hydromechanical actuator and actuation control system.
  20. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  21. Lebrun, Jean-Louis, Secure monitoring and control device for aircraft piloting actuator.
  22. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  23. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  24. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  25. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  26. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  27. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
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