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특허 상세정보

Supersonic vortex generator

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06   
미국특허분류(USC) 244/199 ; 244/198 ; 244/200 ; 296/1801
출원번호 US-0356646 (1994-12-15)
발명자 / 주소
  • Farokhi Saeed (Lawrence KS) Taghavi Ray R. (Lawrence KS)
출원인 / 주소
  • University of Kansas Center for Research Inc. (Lawrence KS 02)
인용정보 피인용 횟수 : 60  인용 특허 : 6
초록

A vortex generator for attenuating flow separation which occur during supersonic flow of air over structure such as an aircraft airfoil, its fuselage, surfaces forming a part of a jet propulsion unit, turbine or compressor blades, or similar surfaces subjected to supersonic airflow. A series of vortex generators are provided each of which comprises a cavity in the component over which the supersonic air is flowing that is configured to generate a spiral vortex which attenuates flow separation and weight drag resulting from the supersonic airflow. Each ca...

대표
청구항

A vortex generator for attenuating flow separation which occurs during supersonic flow of fluid in one direction over the surface of a component from the leading edge of the component toward the trailing edge portion thereof, said vortex generator comprising: structure presenting a cavity in the component located below said surface thereof downstream of said leading edge and upstream of the point on the surface where flow separation would occur without said cavity, said cavity being defined at least in part by elongated side wall means located in disposi...

이 특허를 인용한 특허 (60)

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  3. Couilleaux, Alexandre Gérard François; Ferrier, Romain Jean-Claude; Sirvin, Nicolas Joseph, Air guidance device for a turbomachine with grooves to maintain boundary layer.
  4. Silkey, Joseph S.; Wilson, Christopher D.; Dyer, Richard S., Air induction control.
  5. Gemma, Riccardo, Air intake, in particular for an aircraft chaff dispenser.
  6. Prince, Troy; Lisy, Frederick J.; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N., Aircraft and missile forebody flow control device and method of controlling flow.
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  9. Maris, John M., Airfoil performance monitor.
  10. Ireland, Peter, Application of elastomeric vortex generators.
  11. Kallinen,Risto, Arrangement for generating vortexes.
  12. Kucherov, Yan R.; Hubler, Graham K., Blast wave effects reduction system.
  13. Exton, Reginald J, Boundary layer flow disruptors for delaying transition to turbulent flow.
  14. Slocum, Alexander H.; Buongiorno, Jacopo; Forsberg, Charles Winfield; Codd, Daniel S., Concentrated solar power system.
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  20. Hutcheson, Florence V.; Brooks, Thomas F., Flow disruption devices for the reduction of high lift system noise.
  21. Fujino Michimasa,JPX ; Kawamura Yuichi,JPX, Flow separator reducer.
  22. Hamilton, Terry Wayne, Hamilton H.N2 laminar flow diskette wing.
  23. Maldonado, Jaime, Heat transfer enhancement in internal cavities of turbine engine airfoils.
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  27. Dixon Charles J., Method and apparatus for generating a stable leading-edge lifting-vortex controller.
  28. Whitmore, Stephen A.; Saltzman, Edwin J.; Moes, Timothy R.; Iliff, Kenneth W., Method for reducing the drag of blunt-based vehicles by adaptively increasing forebody roughness.
  29. Shahbazi,Khosrow, Methods for reducing the aerodynamic drag of vehicles.
  30. Bauer Steven X. S. ; Wood Richard M., Micro-drag generators for aerodynamic and hydrodynamic braking and control.
  31. Meyer, Robert, Nozzle, structural element, and method of producing a nozzle.
  32. Petrus Gerardus Marie Reivers NL, Open roof construction for a vehicle.
  33. Reivers, Petrus Gerardus Marie, Open roof construction for a vehicle.
  34. Steinert, Martin; Kameier, Frank; Vranjes, Dusan, Outflow valve for an aircraft.
  35. Domel, Neal D.; Baruzzini, Dan J.; Miller, Daniel N., Passive robust flow control micro device.
  36. Shahbazi,Khosrow, Pressure drag reduction system with a side duct.
  37. Shahbazi,Khosrow, Pressure drag reduction system with an internal duct.
  38. Miller, Daniel N.; Baruzzini, Dan J., Prismatic-shaped vortex generators.
  39. Kim, Nak Hwe, Propulsion device using fluid flow.
  40. 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.
  41. Emerick, Mark F., Recessed lift spoiler assembly for airfoils.
  42. Olsen, Fred; Oigarden, Hans, Recesses on a surface.
  43. Lang, James D., Reducing runway requirement for aircraft.
  44. Narramore, Jimmy Charles, Retractable vortex generator.
  45. Lang Renee M. ; Blaisdell George L., Self-aligning vortex snow fence.
  46. Gionta, Matthew; Karkow, Jon; Roncz, John; Koehler, Dieter; Lednicer, David, Spin resistant aircraft configuration.
  47. Gionta, Matthew; Karkow, Jon; Roncz, John; Koehler, Dieter; Lednicer, David, Spin resistant aircraft configuration.
  48. Reimann, Daniel D.; Richards, Jeffery R.; Hoke, Charles M.; Travis, Robert D., Stage separation mechanism and method.
  49. Candela, Franco; Migliozzi, Giuseppe, Structural element for covering an elongate gap on an aerodynamic surface of an aircraft.
  50. Harrison, Neal A.; Dehaan, Mark; Vassberg, John C.; Sclafani, Anthony J., Submerged vortex generator.
  51. Quackenbush, Todd R.; McKillip, Jr., Robert M.; Danilov, Pavel V., Supersonic engine inlet diffuser with deployable vortex generators.
  52. Gupta, Anurag; Yao, Jixian, System and method for enhanced turbine wake mixing via fluidic-generated vortices.
  53. Tyree, Anthony K., System and method for navigating an object.
  54. Sutton, Drew, System and method for reducing rotor blade noise.
  55. Wang, Anquan; Wang, Guanghua; DeLancey, James Peter, System and methods of inspecting a component.
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  57. Ng T. Terry, Vortex generation for control of the air flow along the surface of an airfoil.
  58. Babinsky, Holger; Loth, Eric; Lee, Sang, Vortex generators to control boundary layer interactions.
  59. Fuglsang, Peter; Bove, Stefano, Wind turbine blade with submerged boundary layer control means.
  60. Fuglsang, Peter; Bove, Stefano, Wind turbine blade with submerged boundary layer control means comprising crossing sub-channels.