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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Link mechanisms for gapped rigid krueger flaps, and associated systems and methods

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-003/00   
미국특허분류(USC) 244/214
출원번호 UP-0453596 (2006-06-14)
등록번호 US-7578484 (2009-09-08)
발명자 / 주소
  • Fox, Stephen J.
  • Sakurai, Seiya
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 16  인용 특허 : 183
초록
▼

Link mechanisms for gapped rigid Krueger flaps, and associated methods and systems are disclosed. A system in accordance with one embodiment includes a deployable leading edge assembly that in turn includes a deployable leading edge panel having a generally fixed-shape flow surface, a bullnose coupled to the panel, and a link mechanism coupled to the panel and the bullnose to move the panel between a stowed position and a deployed position. The mechanism can include a first support link, a second support link, and first, second, and third positioning li...

대표
청구항
▼

We claim: 1. An aircraft system, comprising: a deployable leading edge assembly that includes: a deployable leading edge panel that forms a gap with an airfoil when in a deployed position, wherein the deployable leading edge panel has a generally fixed-shape flow surface extending from a leading end to the gap when in the deployed position, and has the same generally fixed shape flow surface when in a stowed position; a bullnose pivotably coupled to the leading edge panel; a link mechanism coupled to the leading edge panel and the bullnose at a wing spa...

인용문헌 (183)

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이 특허를 인용한 특허 (16)

  1. Johnson, Patterson; Sakurai, Seiya; Santini, Gregory M.; Konings, Christopher A.; Clark, Adam M., Actuator assemblies to deploy aircraft leading edge flaps and seals for aircraft leading edge flaps.
  2. Eden, James, Aircraft assembly and spar.
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  4. 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.
  5. Hoffenberg, Robert, Compound leading edge device for aircraft.
  6. Povinelli, Anthony J.; Matthews, Martin R., Deployable aerodynamic side panel system.
  7. Schröder, Karsten, High lift system for an aircraft.
  8. Hue, Xavier; Schlipf, Bernhard, High lift system for an aircraft and method for influencing the high lift characteristics of an aircraft.
  9. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor H., High-positioned 2-position variable camber Krueger.
  10. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor H., High-positioned 2-position variable camber Krueger.
  11. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor; Charles, Kara Marie, High-positioned 3-position variable camber krueger.
  12. Beyer, Kevin W.; Sakurai, Seiya, Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods.
  13. Wölcken, Piet-Christof, Morphing trailing edge device for an airfoil.
  14. Herrmann, Otfrid, Speed brake for aircraft.
  15. Bleazard, Mark, Torque tube door.
  16. Amorosi, Stephen R.; Santini, Gregory M.; Anderson, Matthew Leroy; Hinrichs, Steve C.; Jarecki, Walter J.; Bennett, Nicholas I.; Pham, Quang Minh; Lai, Paul Hungwai; Rupert, Gregory E.; Osaki, Carl F., Wing leading edge architecture suitable for laminar flow.

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