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Ion doping apparatus and method for aerodynamic flow control 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-001/38
출원번호 US-0158502 (1998-09-23)
발명자 / 주소
  • Saeks Richard E
  • Kunhardt Erich E
  • Carlton Lindley A
  • Pap Robert M
출원인 / 주소
  • Accurate Automation Corporation
대리인 / 주소
    Schellin
인용정보 피인용 횟수 : 34  인용 특허 : 5

초록

Method and apparatus for impingement on the sonic wave produced by a supersonic gas flow and the gas flow in a boundary layer of a gas that interfaces with a solid substrate comprising providing a source of a mixture of ions and electrons, introducing said ions and electrons into the region behind t

대표청구항

[ What is claimed is:] [1.]1. Method for impingement on the sonic wave produced by a gas flow in a boundary layer of a gas that interfaces with a solid substrate comprising providing a source of ablative material as a source of electrons and ions, disassociating said ablative material to produce a m

이 특허에 인용된 특허 (5)

  1. Carpenter Donald G. (Box 62 A North Granby CT 06060), Electrical technique.
  2. Brice ; deceased Neil M. (R.R. No. 1 LATE OF King Ferry NY) Brice ; executrix by Marilyn J. (R.R. No. 1 King Ferry NY 13081), Method and apparatus for controlling earth orbiting satellites and vehicles inter alia.
  3. Roth John Reece (Knoxville TN), Method and apparatus for covering bodies with a uniform glow discharge plasma and applications thereof.
  4. Blackburn Ronald F. ; Warmkessel Barry M. ; Kawamoto Sonja M., System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion.
  5. Bushman Boyd B. (Lockheed Corporation ; Fort Worth Division ; Box 748 - MZ 5965 Fort Worth TX 76101), Wave attenuation.

이 특허를 인용한 특허 (34)

  1. Osborne, Bradley Alan; Wilson, Christopher Daniel, Airfoil trailing edge plasma flow control apparatus and method.
  2. Brandenburg, John E.; Kline, John F.; Resnick, Joshua H., Apparatus and methods for generating persistent ionization plasmas.
  3. Janeke, Charl E., Apparatus and methods for hypersonic stochastic switch.
  4. Krauss, Otto S.; Westbrook, III, John W., Charged projectiles and related assemblies, systems and methods.
  5. Nolcheff, Nick; Frias, Dan, Diffusers, diffusion systems, and methods for controlling airflow through diffusion systems.
  6. Kremeyer, Kevin, Laser-based flow modification to remotely control air vehicle flight path.
  7. Kremeyer, Kevin, Laser-based flow modification to remotely control air vehicle flight path.
  8. Kremeyer, Kevin, Laser-based flow modification to remotely control air vehicle flight path.
  9. Samimy, Mohammad; Adamovich, Igor, Localized arc filament plasma actuators for noise mitigation and mixing enhancement.
  10. Samimy,Mohammad; Adamovich,Igor, Localized arc filament plasma actuators for noise mitigation and mixing enhancement.
  11. Roy, Subrata, Method and apparatus for multibarrier plasma actuated high performance flow control.
  12. Daso, Endwell O.; Pritchett, II, Victor E.; Wang, Ten-See; Farr, Rebecca Ann, Method and system for control of upstream flowfields of vehicle in supersonic or hypersonic atmospheric flight.
  13. Daso, Endwell O.; Pritchett, II, Victor E.; Wang, Ten-See; Farr, Rebecca Ann; Auslender, Aaron Howard; Blankson, Isaiah M.; Plotkin, Kenneth J., Method and system for weakening shock wave strength at leading edge surfaces of vehicle in supersonic atmospheric flight.
  14. Miller, Paul A.; Aragon, Ben P., Method for generating surface plasma.
  15. Krauss, Otto S.; Westbrook, III, John W., Methods of utilizing projectiles.
  16. Quertelet, Clément, Missile provided with a separable protective fairing.
  17. Talmage, Jr.,Robert N., Modular aerospace plane.
  18. Wood, Tommie L.; Corke, Thomas C.; Post, Martiqua, Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft.
  19. Nolcheff, Nick, Plasma flow controlled diffuser system.
  20. Gonzalez,Encarnacion H., Power system for electrically powered land vehicle.
  21. Gonzalez,Encarnacion H., Power system for electrically powered land vehicle.
  22. Higman,Kumiko I., Pseudo surface microwave produced plasma shielding system.
  23. Minick, Alan B., Rotary wing system with ion field flow control.
  24. Kremeyer, Kevin, Shock wave modification method and system.
  25. Kremeyer,Kevin, Shock wave modification method and system.
  26. Enloe,Carl L.; McLaughlin,Thomas E.; Jumper,Eric J.; Corke,Thomas C., Single dielectric barrier aerodynamic plasma actuation.
  27. Malmuth, Norman D.; Fedorov, Alexander; Shalaev, Vladimir; Zharov, Vladimir; Shalaev, Ivan; Maslov, Anatoly; Soloviev, Victor, Surface plasma discharge for controlling forebody vortex asymmetry.
  28. Malmuth, Norman; Fedorov, Alexander, Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow.
  29. Corke, Thomas; Thomas, Flint; Shatzman, David; Wood, Tommie, System and method for aerodynamic flow control.
  30. Drouin, Jr., Donald V.; Schwimley, Scott Lee, Systems and methods for alleviating aircraft loads with plasma actuators.
  31. Silkey, Joseph S.; Smereczniak, Philip, Systems and methods for controlling flows with pulsed discharges.
  32. Minick,Alan B.; Goldberg,Benjamin; Knauer,Larry, Wing enhancement through ion entrainment of media.
  33. Roy, Subrata, Wingless hovering of micro air vehicle.
  34. Roy, Subrata, Wingless hovering of micro air vehicle.
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