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특허 상세정보

Vortex generation for control of the air flow along the surface of an airfoil

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/16    B64C-021/04    B64C-021/06    B64C-023/06    B64C-001/38   
미국특허분류(USC) 244/203 ; 244/199 ; 244/130 ; 244/209 ; 244/208
출원번호 US-0480198 (2000-01-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    MacMillan, Sobanski & Todd, LLC
인용정보 피인용 횟수 : 16  인용 특허 : 10
초록

Apparatus for generating vortices to control the flow of air across a airfoil of an aircraft includes a series of pressure active regions arranged along the leading edge of the airfoil. The pressure active regions include spaced apart valves connected to a source of vacuum, a controller for activating the valves, and sensors for sensing air pressure. The controller is configured to activate the valves in response to the pressure sensed by the sensors, wherein the spaced apart valves are connected to a source of pressurized air as well as to the source of...

대표
청구항

[ What is claimed is:] [1.]1. An apparatus for generating vortices to control the flow of air across an airfoil of an aircraft comprising a series of pressure active regions arranged along the leading edge of the airfoil wherein the pressure active regions include spaced apart valves connected to a source of vacuum, a controller for activating the valves, a plurality of sensors for sensing air pressure, wherein the controller is configured to activate the valves in response to the pressure sensed by the sensor, and said pressure sensors are interspersed ...

이 특허를 인용한 특허 피인용횟수: 16

  1. Hassan, Ahmed A.; Madsen, Casey L.; Billman, Garrett M. Active flow control for transonic flight. USP2018039908617.
  2. DiCocco, Jack; Prince, Troy; Patel, Mehul; Ng, Tsun Ming Terry. Aircraft and missile afterbody flow control device and method of controlling flow. USP2017059637223.
  3. Meister, Juergen. Aircraft component exposed to streaming surrounding air. USP2010037673832.
  4. Hassan, Ahmed A.; Osborne, Bradley A.; Schwimley, Scott; Billman, Garry; Billman, legal representative, Mary. Dynamic bumps for drag reduction at transonic-supersonic speeds. USP2011098016245.
  5. Billman, Garrett M.; O'Neil, Patrick J.. Forebody vortex alleviation device. USP2003096612524.
  6. Jay Lipeles ; R. Glenn Brosch. Guided bullet. USP2002116474593.
  7. Low, Richard; Deeds, Michael; Jean, Daniel L.; Hovland, Christopher. MEMS control surface for projectile steering. USP2009127628352.
  8. Hassan, Ahmed A.; JanakiRam, Ram D.. Method and device for altering the separation characteristics of air-flow over an aerodynamic surface via intermittent suction. USP2005036866234.
  9. Hassan, Ahmed A.; JanakiRam, Ram D.; Cerchie, Dino A.. Method and device for altering the separation characteristics of flow over an aerodynamic surface via hybrid intermittent blowing and suction. USP2005056899302.
  10. Cueman, Michael Kent; Saddoughi, Seyed Gholamali. Method and system for flow control with arrays of dual bimorph synthetic jet fluidic actuators. USP2012038136767.
  11. Van Dam,Cornelis P.; Yen,Dora T.; Smith,Rosemary L.; Collins,Scott D.. Microfabricated translational stages for control of aerodynamic loading. USP2006047028954.
  12. Patel, Mehul P.; DiCocco, Jack M; Prince, Troy. Reconfigurable porous technology for fluid flow control and method of controlling flow. USP2005036866233.
  13. Boldrin, Clete M.; Hassan, Ahmed A.. Vernier active flow control effector. USP2012038128036.
  14. Boldrin,Clete M.; Hassan,Ahmed A.. Vernier active flow control effector. USP2007087255309.
  15. McVeigh, Michael A.; Maciolek, Robert F.. Vortex generators on rotor blades to delay an onset of large oscillatory pitching moments and increase maximum lift. USP2010077748958.
  16. Gieseke, Thomas J.. Vortex-assisted pressure control at inlet of underwater launch system. USP2005086932016.