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특허 상세정보

Method for a leading edge slat on a wing of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-009/22    B64C-009/24    B64C-007/00   
출원번호 US-0955126 (2013-07-31)
등록번호 US-9446836 (2016-09-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Yee & Associates, P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 29
초록

A method for managing a flight control surface system. A leading edge device is moved on a leading edge from an undeployed position to a deployed position. The leading edge device has an outer surface, an inner surface, and a deformable fairing attached to the leading edge device such that the deformable fairing covers at least a portion of the inner surface. The deformable fairing changes from a deformed shape to an original shape when the leading edge device is moved to the deployed position. The leading edge device is then moved from the deployed posi...

대표
청구항

1. A method of controlling lift using a flight control surface system, the method comprising: moving a leading edge device on a wing from an undeployed position to a deployed position, the leading edge device comprising an outer surface, an inner surface, and a deformable fairing attached to the leading edge device the deformable fairing covers at least a portion of the inner surface;changing the deformable fairing from a deformed shape, conforming to a leading edge surface of the wing, to an original shape reducing a noise level produced from air flowin...

이 특허에 인용된 특허 (29)

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  3. Broadbent, Michael Craig. Contiguous variable camber device. USP2004016682023.
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  8. Bliesner Wayne T. (Snohomish WA). Leading edge slat/wing combination. USP1996085544847.
  9. Shmilovich, Arvin; Yadlin, Yoram. Low noise wing slat system with rigid cove-filled slat. USP2013048424810.
  10. Joyce Michael A. (Balderstone GB3) Thompson William (Bury GB3). Manufacture of aircraft track-cans and the like. USP1993065222653.
  11. Zeumer, Claus M. Method and apparatus for deploying an auxiliary lift foil. USP2011088006940.
  12. Gleine, Wolfgang; Mau, Knut; Carl, Udo. Pressure control system for a pressure-expandable displacement element. USP2003036536714.
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  19. Henry, Christopher P.; McKnight, Geoffrey P.; Herrera, Guillermo A.; Doty, Robert E.; Clemons, Richard Lee; Drouin, Jr., Donald V.. Thermally activated variable stiffness composites for aircraft seals. USP2013078476564.
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  24. Cole James B. (Mercer Island WA). Wind edge movable airfoil having variable camber. USP1987034650140.
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