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특허 상세정보

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

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
출원인 / 주소
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...

이 특허에 인용된 특허 (183)

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  182. Lotz ; deceased Michael (late of Immenstaad DEX by Carla Lotz ne Post ; heir and Andreas Lotz ; heir) Vanino ; deceased Rdiger (late of Hagnau DEX H. L. I. M. Vanino ; heir) Khl Peter (Immenstaad DEX. Wing sections, in particular lift-wing sections for aircraft. USP1989084856735.
  183. Victor Paul F. (Issaquah WA). Wing trailing edge air dams. USP1986104618109.

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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. USP2013108567726.
  5. Hoffenberg, Robert. Compound leading edge device for aircraft. USP2014018622350.
  6. Povinelli, Anthony J.; Matthews, Martin R.. Deployable aerodynamic side panel system. USP20190110189517.
  7. Schröder, Karsten. High lift system for an aircraft. USP20190110183737.
  8. Hue, Xavier; Schlipf, Bernhard. High lift system for an aircraft and method for influencing the high lift characteristics of an aircraft. USP2017059656739.
  9. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor H.. High-positioned 2-position variable camber Krueger. USP2017069688386.
  10. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor H.. High-positioned 2-position variable camber Krueger. USP2016069365284.
  11. Sakurai, Seiya; Fox, Stephen J.; Reyes, Victor; Charles, Kara Marie. High-positioned 3-position variable camber krueger. USP2015049016637.
  12. Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
  13. Wölcken, Piet-Christof. Morphing trailing edge device for an airfoil. USP2018059957802.
  14. Herrmann, Otfrid. Speed brake for aircraft. USP2014028640989.
  15. Bleazard, Mark. Torque tube door. USP2017049623957.
  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. USP2018029896190.