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특허 상세정보

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Systems and methods for alleviating aircraft loads with plasma actuators

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G06F-017/00    B64C-021/00    B64C-023/00    H05H-001/24   
출원번호 US-0166199 (2008-07-01)
등록번호 US-9446840 (2016-09-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 1  인용 특허 : 46
초록
▼

Systems and methods for alleviating aircraft loads with plasma actuators are disclosed. A method for operating an aircraft in accordance with a particular embodiment includes receiving an input corresponding to an aircraft component structural response to an aerodynamic load. The method can further include, based at least in part on the input corresponding to the aircraft component's structural response, reducing the structural response to the aerodynamic load by activating at least one plasma actuator carried by the aircraft, in accordance with one or m...

대표
청구항
▼

1. A method for establishing operational parameters for an aircraft, comprising: receiving a baseline structural response profile corresponding to expected total flight time of the aircraft as a function of flight condition, the profile including an expected structural response level at a first corresponding total flight time value;selecting activation parameters for one or more plasma actuators carried by the aircraft based on an effect of the parameters to shift the total flight time value at which the expected structural response level occurs from the...

이 특허에 인용된 특허 (46)

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  2. Maestrello Lucio (Newport News VA). Active control of boundary layer transition and turbulence. USP1990064932610.
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  4. Bonutti, Peter M.. Active drag and thrust modulation system and methods. USP2005126978767.
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  7. Osborne, Bradley Alan; Wilson, Christopher Daniel. Airfoil trailing edge plasma flow control apparatus and method. USP2011087988101.
  8. Ball William H. (Mercer Island WA) Syberg Jan (Kent WA). Apparatus for re-energizing boundary layer air. USP1988064749151.
  9. Herr Jan E. (6250½Stanley Ave. San Diego CA 92115). Apparatus for transmitting electric current by concentric channels of ionized gas. USP1984064453196.
  10. Rethorst Scott Carson (South Pasadena CA). Compression energy transformation system for a supersonic wing. USP1977024008866.
  11. Smereczniak, Philip. Directed energy off-body heating for supersonic vehicle shockwave and sonic boom control. USP2010017641153.
  12. Schoenbach, Karl H.; Byszewski, Wojciech W.; Peterkin, Frank E.; Dharami, Amin N.. Discharge device having cathode with micro hollow array. USP2003026518692.
  13. Edelman Seymour (9115 Glenridge Rd. Silver Spring MD 20910). Drag modification piezoelectric panels. USP1982124363991.
  14. Van de Walle Christian Gilbert. Dual polarization quantum well laser in the 200 to 600 nanometers range. USP1998105828684.
  15. Nosenchuck, Daniel M.; Brown, Garry L.. Electromagnetic device and method for boundary layer control. USP1994065320309.
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  17. Chen, Jyh-Hong Eric; Lin, Tyau-Jeen. Hollow cathode array for plasma generation. USP2003036528947.
  18. Hagseth, Paul E.; McClure, Paul D.. Inlet electromagnetic flow control. USP2011017870720.
  19. Saeks Richard E ; Kunhardt Erich E ; Carlton Lindley A ; Pap Robert M. Ion doping apparatus and method for aerodynamic flow control. USP2001066247671.
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  21. Keefe Laurence R.. Method and apparatus for reducing the drag of flows over surfaces. USP1998095803409.
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  23. Miller, Paul A.; Aragon, Ben P.. Method for generating surface plasma. USP2003056570333.
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  25. Patel, Mehul; Corke, Tom. Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2009127624941.
  26. Corke, Thomas C.; Spivey, Richard. Methods and apparatus for reducing drag via a plasma actuator. USP2012018091950.
  27. Meng James C. S.. Micro-electrode and magnet array for microturbulence control. USP1999085934622.
  28. Nosenchuck Daniel M. (Mercerville NJ) Brown Garry L. (Princeton NJ). Multiple electromagnetic tiles for boundary layer control. USP1995085437421.
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  30. McClure, Paul D.; Chase, Charles J.. Over-wing traveling-wave axial flow plasma accelerator. USP2011088006939.
  31. Sherman Daniel M. ; Wilkinson Stephen P. ; Roth J. Reece. Paraelectric gas flow accelerator. USP2001036200539.
  32. Jacob, Jamey D.. Plasma actuator. USP2010047703479.
  33. Schwimley, Scott L.; Drouin, Jr., Donald V.. Plasma actuator system and method for use with a weapons bay on a high speed mobile platform. USP2011098016246.
  34. 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. USP2012118308112.
  35. Scholl Richard A. ; Christie David J.. Pulsed direct current power supply configurations for generating plasmas. USP1999065917286.
  36. Minick, Alan B.. Rotary wing system with ion field flow control. USP2012018091836.
  37. Silfvast William T. (Holmdel NJ) Szeto Leo H. (Howell NJ) Wood ; II Obert R. (New York NY). Segmented plasma excitation-recombination light source. USP1983074395770.
  38. Kremeyer, Kevin. Shock wave modification method, apparatus, and system. USP2003036527221.
  39. Enloe,Carl L.; McLaughlin,Thomas E.; Jumper,Eric J.; Corke,Thomas C.. Single dielectric barrier aerodynamic plasma actuation. USP2008067380756.
  40. Nosenchuck Daniel M.. Staggered actuation of electromagnetic tiles for boundary layer control. USP1999105964433.
  41. Malmuth, Norman; Fedorov, Alexander. Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow. USP2004106805325.
  42. Tsunoda Stanley I.. System and method for controlling the flow of a conductive fluid over a surface. USP2000066079345.
  43. Blackburn Ronald F. ; Warmkessel Barry M. ; Kawamoto Sonja M.. System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion. USP1998085797563.
  44. Miles, Richard B.; Macheret, Sergey O.; Shneider, Mikhail; Likhanskii, Alexandre; Silkey, Joseph Steven. Systems and methods for controlling flows with electrical pulses. USP2010067744039.
  45. Scott,Simon J; Johnson,Graham A; Thornton,Edward. Turbulent flow drag reduction. USP2006067066431.
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이 특허를 인용한 특허 피인용횟수: 1

  1. Han, Taeyoung; Khalighi, Bahram; Chen, Kuo-huey. Plasma actuator for vehicle aerodynamic drag reduction. USP2017119821862.

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