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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Apparatus and method for backup control in a distributed flight control system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G05D-001/00   
미국특허분류(USC) 244/194; 244/195; 244/196
출원번호 US-0167447 (2011-06-23)
등록번호 US-8235328 (2012-08-07)
발명자 / 주소
  • Hirvonen, Jukka Matti
출원인 / 주소
  • Gulfstream Aerospace Corporation
대리인 / 주소
    Ingrassia Fisher & Lorenz, P.C.
인용정보 피인용 횟수 : 3  인용 특허 : 71
초록
▼

Embodiments of the invention relate to a flight control system for controlling an aircraft during flight. The flight control system may include a primary controller configured to receive an input from a pilot and to output a primary control signal and a primary transmission path connected to the primary controller and configured to relay the primary control signal. The flight control system may also include a backup controller configured to receive the input from the pilot and to output a backup control signal and a backup transmission path connected to ...

대표
청구항
▼

1. A flight control system for controlling an aircraft, the flight control system comprising: a first controller configured to receive a first input and to output a primary control signal;a first transmission path coupled to the first controller and configured to relay the primary control signal;a second controller configured to receive a second input and to output a backup control signal;a second transmission path coupled to the second controller and configured to relay the backup control signal; andan actuator having actuator electronics configured to ...

이 특허에 인용된 특허 (71)

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  11. Bilange Thierry,FRX ; Divoux-Plantaz Marie-Laure,FRX, Aircraft with reduced wing structure loading.
  12. Briffe Michel,FRX ; Mitaux-Maurouard Guy,FRX, Apparatus and mehod for aircraft monitoring and control including electronic check-list management.
  13. Briffe Michel,FRX ; Mitaux-Maurouard Guy,FRX, Apparatus and method for aircraft display and control.
  14. Briffe Michel,FRX ; Mitaux-Maurouard Guy,FRX, Apparatus and method for graphically oriented aircraft display and control.
  15. Boehringer, Wilfred Earl, Augmenting flight control surface actuation system and method.
  16. Cooper Michael G. (Renton WA) Elliott Elden M. (Coupeville WA) Hartzell Dean A. (Bellevue WA), Autopilot flight director system.
  17. Osder Stephen S. (Scottsdale AZ), Back-up fly by wire control system.
  18. Pohling John G., Bobweight assembly for establishing a force feedback on a manually movable control element.
  19. Straub, Philip I.; Langner, Dale R., Cockpit instrument panel systems and methods with redundant flight data display.
  20. Langner, Dale R.; Straub, Philip I., Cockpit instrument panel systems and methods with variable perspective flight display.
  21. Wright David W. (Franklin WI), Color cockpit display for aircraft systems.
  22. Eccles Edward Stuart (Bishops Cleeve ; near Cheltenham EN), Control apparatus.
  23. Murray James B. (New Brighton MN), Control augmentation system for flight vehicles.
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  26. Doniger Jerry (Montvale NJ) Kirchhein Albert T. (Montvale NJ) Reynolds Gibson (Tuxedo NY), Controller for a dual servo system.
  27. Mark I. Snyder, Cursor management on a multiple display electronic flight instrumentation system.
  28. Damotte Sylvain Pascal Frederic,FRX, Device for actuating a controlled member for an aircraft, particularly such as a fly-by-wire helicopter.
  29. Zenon Szulyk ; Brian Dyra ; Alex Makhlin, Dual input servo coupled control sticks.
  30. Buus, Henning; MacFie, Thomas D.; Justad, Odd, Electric command spoiler system.
  31. Bilange Thierry (Tournefeuille FRX) Le Tron Xavier (Toulouse FRX), Electrical flight control system for an airplane, with attitude protection on takeoff.
  32. Devino Vincent A. (Hauppauge NY), Electronic standby flight instrument.
  33. O'Rourke, Kenneth; Wilkens, Dean; Beutler, Arthur D., Fail passive servo controller.
  34. Ferrell Philip J. (Seattle WA) Stern Alan D. (Bellevue WA) McFarland Melvin D. (Pacific WA), Fault scoring and selection circuit and method for redundant system.
  35. Elbert Ralph P. ; Hafner Michael A., Fault tolerant actuation system for flight control actuators.
  36. Le Dong Tuan (Lakewood CA) Huggett Colin E. (Torrance CA), Fault tolerant controller arrangement for electric motor driven apparatus.
  37. Herbermann Carl R. (Centerport NY), Fault tolerant interface station.
  38. Sutherland James F. (Plum Boro PA) Ghrist ; III William D. (Pittsburgh PA), Fault-tolerant analog output network.
  39. Gillingham Gary D. ; Miles Gary L., Flap/slat actuation system for an aircraft.
  40. Boehringer Wilfred E. ; Verhoeven Teunes, Flight control mechanical backup system.
  41. Larry Yount ; John Todd, Flight control module merged into the integrated modular avionics.
  42. Yount, Larry; Todd, John, Flight control module with integrated spoiler actuator control electronics.
  43. Yamamoto, Tsuyoshi, Flight control system.
  44. Takats Imre J. (Bellevue WA), Flight control system employing three controllers operating a dual actuator.
  45. Takats Imre J. (Bellevue WA) Aziz George W. (Seattle WA), Flight control system employing two dual controllers operating a dual actuator.
  46. Repperger Daniel W. (Vandalia OH), Flight control system with tactile feedback.
  47. Todeschi Michel,FRX ; Andrieu Laurent,FRX ; Vollard Cecile,FRX ; Perie Jean-Claude,FRX, Flying aid device for a fly-by-wire aircraft.
  48. Galus Dean M. (Endicott NY) Sill Brian E. (Binghamton NY), High performance control loading system for manually-operable controls in a vehicle simulator.
  49. Staple Alan E. (Stoke-sub-Hamdon GB2), Integrated vibration reducing and health monitoring system for a helicopter.
  50. Gregory William W. (St. Petersburg FL) Lance Wayne E. (Largo FL) Hegg Jeffrey W. (North Redington Beach FL), Integrator management for redundant active hand controllers.
  51. Graham Donald A. (Redmond WA) Edmonds Thomas E. (Bellevue WA), Intervention flight management system.
  52. Jackson Douglas O. (Mercer Island WA), Method and apparatus for implementing a databus voter to select flight command signals from one of several redundant asy.
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  54. Preissler, Dieter, Method and control arrangement for adjusting a flap that is pivotally supported in a rotor blade of a helicopter.
  55. Ortega, Jean-Marc; Garcia, Jean-Pierre, Method and device for controlling an aircraft maneuvering components, with electrical standby modules.
  56. Urnes, Sr., James M.; Hood, Mark B., Method and system for in-flight fault monitoring of flight control actuators.
  57. Nicholas, Jeffrey S.; Miller, David G., Method, system, and computer program product for tactile cueing flight control.
  58. Gold Phillip Jeremy ; Mayo John Randall, Model-following control system using acceleration feedback.
  59. Lance Wayne E. (Largo FL) Hegg Jeffrey W. (North Redington Beach FL), Moment cell counterbalance for active hand controller.
  60. Hickman Alan B., Monitoring systems for detecting failures in fly-by-wire aircraft flight control systems.
  61. Aldrich Allyn M. (Rockford IL), Multi-motor actuation system for a power drive unit.
  62. Buus Henning (Woodinville WA), Multiaxis redundant fly-by-wire primary flight control system.
  63. Murphy, Milford R.; Haskins, Delbert E., Multiple loop control system.
  64. Takats Imre J. (Bellevue WA) Chenoweth Charles C. (Bellevue WA), Multiple-voting fault detection system for flight critical actuation control systems.
  65. Gregory William W. (St. Petersburg FL) Kauffman James W. (Palm Harbor FL), Position dependent rate dampening in any active hand controller.
  66. Ferranti Michael J. (Naugatuck CT) Novis Ari M. (Rocky Hill CT) Durno Ronald A. (Trumbull CT), Programmable, linear collective control system for a helicopter.
  67. Kupersmit Carlos A. (Lake Worth FL), Self contained data acquisition apparatus and system.
  68. Kissel Gerhard K. (Ottobrunn DEX), Steering mechanism with an active force feedback, especially for aircraft.
  69. Hirvonen, Jukka Matti; Palfreyman, Gary, System and method for an integrated backup control system.
  70. Traverse Pascal (Tournefeuille FRX) Le Tron Xavier (Toulouse FRX), System for control of an aerodynamic surface of an aircraft.
  71. Gregory William W. (St. Petersburg FL) Lance Wayne E. (Largo FL) Hegg Jeffrey W. (North Redington Beach FL), Variable servo loop compensation in an active hand controller.

이 특허를 인용한 특허 (3)

  1. Fervel, Marc; Lecanu, Arnaud; Maussion, Antoine; Aubert, Jean-Jacques, Distributed flight control system implemented according to an integrated modular avionics architecture.
  2. Kamenetz, Jeffry K.; Johnston, Mark A.; Marotta, Edward John; Bleier, Cathleen R.; O'Neil, John M., Multi-channel control switchover logic.
  3. Noll, Christopher; Avritch, Steven A., Redundant two stage electro-hydraulic servo actuator control.

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