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특허 상세정보

System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/38   
미국특허분류(USC) 244/130 ; 322/02A ; 244/204 ; 244/205
출원번호 US-0625914 (1996-04-01)
발명자 / 주소
대리인 / 주소
    Papageorge
인용정보 피인용 횟수 : 38  인용 특허 : 0
초록

The system includes radiation generation and transmission components which radiate tuned microwave electromagnetic energy outwardly from a vehicle through an antenna into a fluid medium through which the vehicle is moving. The microwave radiation is at the frequency of harmonic resonance electromagnetic excitation of the molecules of the medium which produces efficient heating and ionizing of the fluid resulting in a reduction of the mass density thereof. This reduction decreases the drag forces acting on the vehicle resulting in a greatly enhanced aerod...

대표
청구항

[ What is claimed is:] [1.] A system for increasing the dynamic efficiency of a vehicle in a fluid medium, comprising:a source of electromagnetic radiation;means for transmitting electromagnetic radiation from said source to desired surface portions of the vehicle, said surface portions including leading edges, said means for transmitting receiving the radiation from said source;means for emitting a beam of the radiation outwardly and away from the desired surface portions, the leading edges and the vehicle in order to heat the fluid medium thereby reduc...

이 특허를 인용한 특허 피인용횟수: 38

  1. Bonutti, Peter M.. Active drag and thrust modulation system and method. USP2004096793177.
  2. Bonutti, Peter M.. Active drag and thrust modulation system and methods. USP2005126978767.
  3. Bonutti, Peter M.. Active drag modulation system and method. USP2004116824108.
  4. DiCocco, Jack; Prince, Troy; Patel, Mehul; Ng, Tsun Ming Terry. Aircraft and missile afterbody flow control device and method of controlling flow. USP2017059637223.
  5. Bonutti, Peter M.. Drag modification system. USP2013078482436.
  6. Lugg, Richard H.. Hypersonic aircraft. USP20190310232937.
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  10. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  11. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  12. Kremeyer, Kevin. Laser-based flow modification to remotely control air vehicle flight path. USP2014098827211.
  13. Kremeyer, Kevin. Laser-based flow modification to remotely control air vehicle flight path. USP20181110124883.
  14. Kremeyer, Kevin. Laser-based flow modification to remotely control air vehicle flight path. USP2017019533753.
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  19. Teter, Roger D.; Dunn, Steven A.; Meyer, J. William. Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy. USP2010057721997.
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  21. Miller, Paul A.; Aragon, Ben P.. Method for generating surface plasma. USP2003056570333.
  22. Lewis, Blair J.. Method, apparatus, and system for deflecting air approaching a wing. USP2012058181910.
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  27. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  28. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
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  32. Meyer,J. W.. System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping. USP2007077237752.
  33. Drouin, Jr., Donald V.; Schwimley, Scott Lee. Systems and methods for alleviating aircraft loads with plasma actuators. USP2016099446840.
  34. Silkey, Joseph S.; Smereczniak, Philip. Systems and methods for controlling flows with pulsed discharges. USP2014058727286.
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