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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Flaperon system for tilt rotor wings

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/02   
미국특허분류(USC) 244/214 ; 244/130 ; 244/219
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. Interconnecting structure is provided between the main portion of the wing and the flaperon seal. Such structure is operable to pivot the seal flap such that the opening between the trailing edge of the main wing portion (20b) and the leading edge of said movabl...

대표
청구항
▼

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 for angularly positioning said flaperon seal relative to said flaperon as said flaperon is pivoted relative to said main wing portion, said control means comprising: (i) a rigid arm attached to said flaperon seal; (ii) a cam follower attached to said rigid arm;...

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.
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  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.
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  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.
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  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.
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  42. Morris, Ralph F., Safety aileron system.
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  47. Yu-Hang Ho, System and method for deflecting an aerodynamic control surface.
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  56. Petrov, Val, Vertical takeoff and landing airframe.

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