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Extendible leading edge flap

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/44
출원번호 US-0936631 (1997-09-25)
발명자 / 주소
  • Appa Kari
출원인 / 주소
  • Northrop Grumman Corporation
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 39  인용 특허 : 9

초록

A flight control system comprises trailing edge airfoil members pivotally mounted at the trailing edge of each wing of an aircraft and selectively movable on a laterally extending axis between raised and lowered positions for imparting rolling motion to the aircraft. Leading edge airfoil members mou

대표청구항

[ What is claimed is:] [1.] A flight control system for an aircraft including a fuselage having a longitudinal axis and fixed wings supported on and extending laterally from said fuselage, said wings having leading and trailing edges, respectively, said flight control system comprising:trailing edge

이 특허에 인용된 특허 (9)

  1. Tulinius Jan (Huntington Beach CA), Active flexible wing aircraft control system.
  2. Fitzgibbon Thomas F. (Long Beach CA) Hamilton Paul U. (Palos Verdes Est. CA), Actuating system for aircraft wing slat and flap panels.
  3. Borzachillo Angelo (San Marcos CA), Aeroelastic control flap.
  4. Gerhardt Heinz A. (Redondo Beach CA), Aircraft outboard control.
  5. Krafka Herfried (Toulouse FRX), Device for automatically controllable unloading of aircraft wings.
  6. Whitaker ; Sr. Robert H. (Atlanta GA), Flight control device for airplanes.
  7. Lewis George E. (Renton WA), Maneuver load alleviation system.
  8. Gleine Wolfgang,DEX ; Hilbig Reinhard,DEX ; Wendt Hans-Joachim,DEX, Method and apparatus for optimizing the aerodynamic effect of an airfoil.
  9. Brown Robert B. (Kent WA), Wing leading edge slat.

이 특허를 인용한 특허 (39)

  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. Voogt,Nicolaas, Aerospace vehicle fairing systems and associated methods.
  4. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  5. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  6. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  8. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  9. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  10. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  11. 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.
  12. 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.
  13. 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.
  14. 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.
  15. 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.
  16. Arata,Allen A.; Graham,David H., Aircraft with articulated leading edge of fuselage and wings.
  17. Arata,Allen A., Aircraft with extendable leading edge of fuselage and wings.
  18. Arata,Allen A., Aircraft with rotatable leading edge of fuselage and wings.
  19. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas, Airplane with unswept slotted cruise wing airfoil.
  20. Volk, John A., Control system for alleviating a gust load on an aircraft wing.
  21. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W., Horizontal tail load alleviation system.
  22. Tran, Chuong B.; Najmabadi, Kioumars; Coleman, Edward E.; Grubb, David W., Horizontal tail load alleviation system.
  23. Bowcutt, Kevin G., Hypersonic waverider variable leading edge flaps.
  24. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  25. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  26. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  27. Beyer, Kevin W.; Sakurai, Seiya, Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods.
  28. Dun, Roy, Methods and apparatuses for controlling airflow proximate to engine/airfoil systems.
  29. Hinnant, Harris O.; Black, David J.; Brekke, Darin W.; Castelluccio, Mark A.; Dickerson, Matt R., Methods and systems for active wing and lift surface control using integrated aeroelasticity measurements.
  30. Sakurai,Seiya; Fox,Stephen J.; Beyer,Kevin W.; Lacy,Douglas S.; Johnson,Paul L.; Wells,Stephen L.; Noble,Jack S.; Meredith,Paul T.; Huynh,Neal V.; Christianson,Russell R.; Vijgen,Paul M.; Fitzpatrick, Multi-function trailing edge devices and associated methods.
  31. Kordel, Jan A.; Sakurai, Seiya; Bowers, Bret A.; Glassmoyer, Christopher G.; Williams, Darren B., Seal assemblies for use with drooped spoilers and other control surfaces on aircraft.
  32. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  33. Delaplace,Franck; Buisson,Dominique, System for automatically controlling lift-enhancing devices of an aircraft, in particular wing leading edge slats.
  34. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  35. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  36. Huynh,Neal V., Systems, apparatuses, and methods for moving aircraft control surfaces.
  37. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  38. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  39. 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.
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