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특허 상세정보

Vortex generators for inlets

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 244/53B ; 244/199
출원번호 US-0885062 (1986-07-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 0

A pair of vortex generators are attached to the exterior surface of an aircraft and located forwardly of a flush inlet so as to effectively remove or reduce the thickness of a slower-moving boundary layer airflow ajdacent to the exterior aircraft surface and increase the mass airflow into the flush inlet. The pair of vortex generators induce higher mean total pressure airflow into the area between the vortex generators and downstream thereof and in front of to the flush inlet, thereby resulting in an increase in mass airflow into the flush inlet for a gi...


Inlet fluid flow inducing means, comprising: a pair of fin-like elements mounted upstream to the direction of free stream fluid flow over an inlet; said pair of fin-like elements being spaced apart normal to the direction of the free stream fluid flow for producing a pair of trailing vortex filaments therefrom; said pair of trailing vortex filaments, in cross-section, having adjacent counter-rotating vortices that merge in a similar-directional fluid flow into a downstream area between the fin-like elements and the inlet; said pair of fin-like elements b...

이 특허를 인용한 특허 피인용횟수: 22

  1. Gemma, Riccardo. Air intake, in particular for an aircraft chaff dispenser. USP2013078485467.
  2. Zachrisson, Björn. Arrangement and method for launching counter-measures. USP2013078490924.
  3. Zätterqvist, Christer. Arrangement for storing and launching payloads. USP2013108549976.
  4. Kreuzer, Peter; Schaber, Sven; Goldhahn, Iris. Arrangement of aerodynamic auxiliary surfaces for an aircraft. USP2015059038950.
  5. Vassberg, John C.; Yeh, David T.; DeHaan, Mark A.; Harrison, Neal A.; Ullman, Alan Z.; Traffenstedt, Michael W.. Beam director flow control. USP2010107815150.
  6. Owens, Lewis R.; Allan, Brian G.. Boundary-layer-ingesting inlet flow control system. USP2010087784732.
  7. Zätterqvist, Christer. Closable counter-measure compartments for a dispenser unit. USP2014058720829.
  8. Zätterqvist, Christer. Countermeasure arrangement. USP2013128607682.
  9. Bonnaud, Cyril; Stevens, Thomas; Roche, Frédéric; Dostes, Stéphane. Device for generating aerodynamic disturbances so as to protect the outer surface of an aircraft against elevated temperatures. USP2012058172178.
  10. Hebert Leonard J. ; Miller Wendell R. ; Nesbitt Eric H. ; Piro Jerry ; Sangwin Michael L.. Flow control device to eliminate cavity resonance. USP2000046050527.
  11. Silkey, Joseph S.; Wilson, Christopher D.; Dyer, Richard S.. Inlet distortion and recovery control system. USP2009127637455.
  12. Daggett, David Lee; Utendorf, Randy; Lawson, Irwin. Low drag skin heat exchanger. USP20180810059435.
  13. Fransson, Mats; Salib, Ramses. Method for launching counter-measures, and arrangement for storing and launching counter-measures. USP2003096619178.
  14. Dahm, Werner J. A.; Lapsa, Andrew P.. Passive boundary layer control elements. USP2013098528601.
  15. Sheoran, Yogendra Y.; Bouldin, Bruce D.. Plenum entry bulk swirl generator. USP2003026520738.
  16. Rybalko, Michael; Conners, Timothy R.; Wayman, Thomas R.. Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system. USP2018029884688.
  17. Quackenbush, Todd R.; McKillip, Jr., Robert M.; Danilov, Pavel V.. Supersonic engine inlet diffuser with deployable vortex generators. USP2016089429071.
  18. Evans, Robert B.. Surface flow enhancement device and method of using the same on a vehicle. USP2014108852710.
  19. Evans, Robert B.. Surface flow enhancement device and method of using the same on a vehicle. USP2016119481405.
  20. Miller,Daniel N.; Truax,Philip P.; Yagle,Patrick J.. System and method to control flowfield vortices with micro-jet arrays. USP2009037510149.
  21. Gieseke, Thomas J.. Vortex-assisted pressure control at inlet of underwater launch system. USP2005086932016.
  22. Fuglsang, Peter; Bove, Stefano. Wind turbine blade with submerged boundary layer control means. USP2013118579594.