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특허 상세정보

Vortex generation

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06    B64C-009/24   
출원번호 US-0466202 (2012-05-08)
등록번호 US-9505485 (2016-11-29)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Reising Ethington P.C.
인용정보 피인용 횟수 : 2  인용 특허 : 30
초록

A vortex generation apparatus including a vortex generator that deploys in response to deployment of a wing leading edge lift augmentation device. The vortex generator deploys into a position to generate vortices over a main wing body upper surface region trailing the vortex generator.

대표
청구항

1. A vortex generation apparatus comprising a vortex generator coupled to a trailing edge of a wing leading edge lift augmentation device, and configured to deploy with the wing leading edge lift augmentation device into a position where the vortex generator will generate vortices over at least a portion of a main wing body upper surface region trailing the vortex generator; wherein the leading edge lift augmentation device comprises a leading edge flap having a flap seal; andwherein the vortex generator is incorporated into a trailing edge of the flap s...

이 특허에 인용된 특허 (30)

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  2. Collett Edward,GBX. Aircraft wing leading edge high lift device with suction. USP2000106135395.
  3. Wang Timothy (Bellevue WA). Aircraft wing stall control device and method. USP1987104702441.
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  13. Mau, Knut; Dobrzynski, Werner. Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing. USP2004096789769.
  14. Bauer Andrew B. (Orange CA). Hidden vortex generators. USP1977084039161.
  15. Rudolph Peter K. C. (Seattle WA). Hinge fairings for control surfaces. USP1995025388788.
  16. Coplin John F. (Derby GB2). Low drag surface. USP1990094955565.
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  18. Ingo Borchers DE; Roger Drobietz DE; Michael Gruenewald DE; Knut Mau DE; Johann Reichenberger DE. Noise reducing vortex generators on aircraft wing control surfaces. USP2002126491260.
  19. Gilbertson Frederick L. (Toronto CAX) Garland Douglas B. (Toronto CAX) Whittley Donald C. (Toronto CAX). Nozzle structure with notches. USP1982014311291.
  20. Martín Hernández, Agustin Mariano. Reinforced cover for cut-outs in an aerodynamic contour. USP2010107815147.
  21. Martín Hernández, Agustín Mariano. Reinforced cover for gaps in an aerodynamic contour. USP2010037669800.
  22. Fox, Bruce R.; Fox, Stephen J.. Retractable vortex generator for reducing stall speed. USP2014028657238.
  23. Bender, Klaus. Rudder of a commercial aircraft. USP2011118061652.
  24. Vijgen Paul M. H. W. (Hampton VA) Howard Floyd G. (Hampton VA) Bushnell Dennis M. (Wicomico VA) Holmes Bruce J. (Newport News VA). Serrated trailing edges for improving lift and drag characteristics of lifting surfaces. USP1992025088665.
  25. Dizdarevic Faruk. Slot forming segments and slot changing spoilers. USP2001126328265.
  26. Jorgensen, Bernard J.. Spoiler device for attachment to a leading edge slat. USP1985114553721.
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