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특허 상세정보

Single dielectric barrier aerodynamic plasma actuation

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/02    B64C-013/00   
미국특허분류(USC) 244/175; 244/205; 244/198; 244/130
출원번호 US-0994029 (2004-11-16)
등록번호 US-7380756 (2008-06-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    AFMCLO/JAZ
인용정보 피인용 횟수 : 45  인용 특허 : 22
초록

A single dielectric barrier aerodynamic plasma actuator apparatus based on the dielectric barrier discharge phenomenon is disclosed and suggested for application to aerodynamic uses for drag reduction, stall elimination and airfoil efficiency improvement. In the plasma actuator apparatus non-uniform in time and space, partially ionized gasses are generated by one or more electrode pairs each having one electrically encapsulated electrode and one air stream exposed electrode and energization by a high-voltage alternating current waveform. The influence of...

대표
청구항

We claim: 1. Air vehicle dielectric barrier aerodynamic plasma actuator apparatus comprising the combination of: an aerodynamic vehicle having a vehicle airfoil component disposed in a moving air location thereof; a first dielectric barrier discharge electrical conductor element surrounded by an electrically insulating dielectric barrier enclosure member and disposed in a selected position on said aerodynamic vehicle component in said moving air location; a second dielectric barrier discharge electrical conductor element located proximate said electrica...

이 특허에 인용된 특허 (22)

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이 특허를 인용한 특허 피인용횟수: 45

  1. Khozikov, Vyacheslav; Liu, Shengyi; Roe, George M.. Active directional control of airflows over rotorcraft blades using plasma actuating cascade arrays. USP2012048157528.
  2. Khozikov, Vyacheslav; Liu, Shengyi; Roe, George M.. Active directional control of airflows over wind turbine blades using plasma actuating cascade arrays. USP2012048162610.
  3. DiCocco, Jack; Prince, Troy; Patel, Mehul; Ng, Tsun Ming Terry. Aircraft and missile afterbody flow control device and method of controlling flow. USP2017059637223.
  4. Matsuda, Hisashi; Yamazaki, Kenichi; Tanaka, Motofumi; Shimura, Naohiko; Asayama, Masahiro; Osako, Toshiki. Airflow generation device and wind power generation system. USP2017079709032.
  5. Wiebe, David J.; Montgomery, Matthew D.. Control of blade tip-to-shroud leakage in a turbine engine by directed plasma flow. USP2013118585356.
  6. Murray, Robert Carl; Gupta, Anurag; Saddoughi, Seyed Gholamali; Wadia, Aspi Rustom. Control of shockwave-boundarylayer-interaction using MEMS plasma devices. USP2012068196871.
  7. Bedel, Laurent; Jouve, Michel. Device for treating gases using surface plasma. USP2015038974741.
  8. Khozikov, Vyacheslav; Liu, Shengyi. Disbanded cascaded array for generating and moving plasma clusters for active airflow control. USP2012088251318.
  9. Hansen, Craig M.; McClure, Paul D.; Macheret, Sergey. Dynamically controlled cross flow instability inhibiting assembly. USP2014018636254.
  10. Silkey, Joseph S.; Wilson, Christopher D.; Dyer, Richard S.. Inlet distortion and recovery control system. USP2009127637455.
  11. Silkey, Joseph Steven; Suiter, David James; Osborne, Bradley Alan. Laminated plasma actuator. USP2018059975625.
  12. Roy, Subrata. Method and apparatus for providing high control authority atmospheric plasma. USP2017119820369.
  13. Patel, Mehul; Corke, Thomas C.. Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2012098267355.
  14. Patel, Mehul; Corke, Tom. Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2009127624941.
  15. Patel, Mehul; Corke, Tom. Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators. USP2017129834301.
  16. Vuillemin, Alexandre Alfred Gaston. Method of processing acoustic waves emitted at the outlet of a turbo engine of an aircraft with a dielectric-barrier discharge device and aircraft comprising such a device. USP2016069361876.
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  20. Domel, Neal D.; Baruzzini, Dan J.; Miller, Daniel N.. Passive robust flow control micro device. USP2013038403271.
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