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Flaperon system for tilt rotor wings 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-009/02
출원번호 US-0417811 (1989-10-13)
발명자 / 주소
  • Narramore Jimmy C. (Bedford TX)
출원인 / 주소
  • Bell Helicopter Textron Inc. (Fort Worth TX 02)
인용정보 피인용 횟수 : 56  인용 특허 : 0

초록

The present invention provides an aircraft wing (10) having a main portion (20) with a trailing edge (20b) and a movable flaperon (22) hingedly secured at the trailing edge. A movable flaperon seal (40) is hingedly attached at its leading edge to the trailing edge of the main portion of the wing. In

대표청구항

An aircraft wing assembly comprising: (a) a main wing portion having a trailing edge; (b) a pivotal flaperon directly attached to said main wing portion; (c) a flaperon seal pivotally attached to said main wing portion; (d) control means for interconnecting said flaperon and said flaperon seal and f

이 특허를 인용한 특허 (56)

  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. Okabe, Yoshinori; Ishihara, Kenya; Sugawara, Zenta, Aircraft.
  9. Morgan, Brian Herman; Hagen, David LeRoy, Aircraft attitude control configuration.
  10. Morgan, Brian Herman; Hagen, David LeRoy, Aircraft attitude control configuration.
  11. Morgan, Brian Herman; Hagen, David LeRoy, Aircraft attitude control configuration.
  12. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  13. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  14. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  15. 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.
  16. 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.
  17. 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.
  18. 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.
  19. 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.
  20. Weaver, Clive, Aircraft wing coupling arrangement.
  21. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  22. Reckzeh, Daniel; Dyke, Adrian R., Aircraft wing, method for operating an aircraft wing, and use of a pivotable trailing edge on a main wing of an aircraft, for adjusting the shape and width of an air gap.
  23. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas, Airplane with unswept slotted cruise wing airfoil.
  24. MacGregor, Keith; Croston, David, Bi-directional flight control surface utilizing a split-track mechanism.
  25. Caton John Harold ; Hobey Michael James ; Groeneveld John David ; Jacobs Jack Howard ; Wille Robert Henry ; Brase ; Jr. Lawrence Otto, Control surface for an aircraft.
  26. John Harold Caton ; Michael James Hobey ; John David Groeneveld ; Jack Howard Jacobs ; Robert Henry Wille ; Lawrence Otto. Brase, Jr., Control surface for an aircraft.
  27. Balayn Frederic,FRX ; Magre Eric,FRX, Convertible aircraft with tilting rotors.
  28. Krysinski, Tomasz; Ferrer, Rogelio; Manfredotti, Thomas; Magre, Eric; Klein, Jean-Marc, Convertible aircraft with tilting rotors.
  29. John Cleveland Waldrop, III ES, Elastic ground plane.
  30. Gartelmann, Rainer; Zapf, Bodo; Hachmann, Knut, Landing flap guide for aircraft.
  31. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  32. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  33. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  34. Beyer, Kevin W.; Fox, Stephen J.; Lacy, Douglas S.; Sakurai, Seiya, Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface.
  35. Dun, Roy, Methods and apparatuses for controlling airflow proximate to engine/airfoil systems.
  36. 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.
  37. Wakayama,Sean R., Reconfiguration control system for an aircraft wing.
  38. Dennison, William D.; May, Carl A., Removable horizontal stabilizer for helicopter.
  39. Dennison, William D.; May, Carl A., Removable horizontal stabilizer for helicopter.
  40. Narramore, Jimmy Charles, Retractable vortex generator.
  41. Kordel, Jan A.; Sakurai, Seiya, Rotary actuated high lift gapped aileron.
  42. Morris, Ralph F., Safety aileron system.
  43. 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.
  44. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  45. Jaggard, Philip R.; West, Robert H., Slat support funk plate.
  46. Dahl, Bruce A., Spring track roller assembly.
  47. Yu-Hang Ho, System and method for deflecting an aerodynamic control surface.
  48. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  49. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  50. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  51. Huynh,Neal V., Systems, apparatuses, and methods for moving aircraft control surfaces.
  52. Gemilang, Atra Surya; Voege, Wolfgang, Trail-edge flap system for a wing of an aircraft.
  53. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  54. Schlipf, Bernhard; Payne, Chris; Gibbert, Markus; Dostmann, Tom, Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device.
  55. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  56. Petrov, Val, Vertical takeoff and landing airframe.
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