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특허 상세정보

Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/16    B64C-009/00   
미국특허분류(USC) 244/216; 244/213; 244/215
출원번호 US-0188988 (2002-07-02)
등록번호 US-7258308 (2007-08-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 13  인용 특허 : 61
초록

A method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface. The airfoil can include a first portion having a first leading edge, a first flow surface, and a second flow surface facing opposite from the first flow surface. The airfoil can further include a second portion having a second leading edge and a trailing edge, with at least part of the second portion being positioned aft of the first portion. The second portion is moveable relative to the first portion between a first position and a second po...

대표
청구항

We claim: 1. An airfoil assembly, comprising: a first portion having a first leading edge, a first flow surface, a second flow surface facing opposite from the first flow surface, and a hinge support; a second portion having a trailing edge body, a leading edge body, a second leading edge and a trailing edge, at least part of the second leading edge being positioned aft of the first leading edge, the second portion being movable relative to the first portion between a first position and a second position, wherein the second leading edge is separated fr...

이 특허에 인용된 특허 (61)

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이 특허를 인용한 특허 피인용횟수: 13

  1. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
  2. 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.
  3. 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. USP2011108038103.
  4. 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. USP2010067744040.
  5. 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. USP2009017475854.
  6. Droney, Christopher K.; Rawdon, Blaine K.. Aircraft wing assemblies. USP2017019550559.
  7. Saliveros, Efstratios; Friedel, Hendrik. Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system. USP2017119815547.
  8. Beyer, Kevin W.; Sakurai, Seiya; Stephenson, Martin F.. Hinged panel operation systems and methods. USP2015069061753.
  9. Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
  10. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  11. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2011027891611.
  12. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael. Systems and methods for providing differential motion to wing high lift device. USP2010067726610.
  13. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.