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특허 상세정보

Method for manufacturing a nacelle strake

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-005/06    B29C-053/38    B64F-005/10   
출원번호 US-0626694 (2015-02-19)
등록번호 US-9937998 (2018-04-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    O'Shea Getz P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 20
초록

A method for manufacturing a strake is provided. The method includes: providing a first thermoplastic laminate panel; providing a second thermoplastic laminate panel; attaching the first thermoplastic laminate panel to the second thermoplastic laminate panel such that at least a portion of the attachment surface of the first thermoplastic laminate panel is attached to the attachment surface of a portion of the second thermoplastic laminate panel, which attached portions form a body of the strake; forming a first flange from a portion of the first thermop...

대표
청구항

1. A method of manufacture, comprising: providing a first thermoplastic laminate panel, having a thickness extending between an exterior surface and an attachment surface;providing a second thermoplastic laminate panel, having a thickness extending between an exterior surface and an attachment surface;attaching the first thermoplastic laminate panel to the second thermoplastic laminate panel such that at least a portion of the attachment surface of the first thermoplastic laminate panel is attached to the attachment surface of a portion of the second the...

이 특허에 인용된 특허 (20)

  1. Murri Daniel G. (Grafton VA). Actuated forebody strakes. USP1990044917333.
  2. Wainfan Barnaby S. ; Mrdeza Matthew N.. Aerodynamic control effector. USP1999105961068.
  3. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.; Lan, Justin. Aircraft configuration. USP2014018628040.
  4. Desroche, Robert J.. Aircraft stabilization systems and methods of modifying an aircraft with the same. USP2015038985503.
  5. Lawson Dale W. R. (Bonita CA). Aircraft turbine engine thrust reverser. USP1993075230213.
  6. Schwetzler, Detlev. Engine pod for an aircraft with a vortex generator arrangement. USP2012058181912.
  7. Wainfan Barnaby S. (Long Beach CA) Mrdeza Matthew N. (Norwalk CA). High-lift device for aircraft. USP1994115366180.
  8. Lippert ; Jr. Joseph (Locust Valley NY). Means to reduce and/or eliminate vortices, caused by wing body combinations. USP1976063960345.
  9. Heffner George (University City CA). Mechanism for assemblying multi-strate panel with plastic keys. USP1977104054481.
  10. Porter Richard G. (Burleson TX) Guzzardo Bryan J. (Fort Worth TX). Method for modifying aircraft strake. USP1994015275360.
  11. Lengsfeld, Hauke; Luebbering, Christian. Method for producing a T-stringer. USP2013108545659.
  12. Amano Kanichi (Tokyo JPX) Tani Yasuhiro (Utsunomiya JPX). Nacelle apparatus for an airplane. USP1997085653406.
  13. Konings, Christopher A.. Nacelle chine installation for drag reduction. USP2005116964397.
  14. Wang, Timothy; Zierten, Thomas A.. Nacelle/wing assembly with wake control device. USP1985094540143.
  15. Brennan, Joseph D.; Hempstead, George D.; Jones, Darrell D.; Lum, Matthew K.; McCowin, Peter D.; Rowe, Terrence J.; Schlosstein, Hugh R.. Pre-patterned layup kit and method of manufacture. USP2013108568551.
  16. Sclafani, Anthony J.; Konings, Christopher A.. Retractable nacelle chine. USP2012018087617.
  17. Skow Andrew (Rolling Hills Estates CA). Strakes for landing speed reduction. USP1993105249762.
  18. Grove, Darren V.. Transonic flow shockwave position stabilizer. USP2003026513754.
  19. Wood,Richard M.. Vortex strake device and method for reducing the aerodynamic drag of ground vehicles. USP2007087255387.
  20. Morgenstern,John M.; Arslan,Alan E.. Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance. USP2009017475848.