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특허 상세정보

Relating to air-breathing flight vehicles

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 244/207; 244/035A; 244/053B
출원번호 US-0640579 (2009-12-17)
등록번호 US-8662453 (2014-03-04)
우선권정보 EP-08253441 (2008-10-23); GB-0819473.0 (2008-10-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Buchanan Ingersoll & Rooney PC
인용정보 피인용 횟수 : 2  인용 특허 : 12

An air intake for a supersonic air-breathing flight vehicle introduces or injects fluid in order to create predetermined regions of separated flow and an attendant fluid shear layer. This shear layer forms an aerodynamic boundary for the capture flow with a profile determined and optimised by appropriate injection of fluid. The aerodynamic boundary so generated replaces mechanically moveable solid surfaces used to vary the geometry of prior-art intakes. Use of an introduced or injected fluid can provide an advantage of a variable geometry, but with reduc...


1. A method of controlling a location of shock waves generated at a leading edge of an engine intake of an engine in a powerplant of a supersonic vehicle, the engine intake comprising a surface providing the leading edge and a cowl having a cowl lip downstream of the leading edge, so that the shock wave extends in an optimum orientation relative to the cowl lip, the method comprising: downstream of the leading edge and upstream of the cowl lip, injecting air into an air flow captured by the air-intake, the air being injected through or adjacent the surfa...

이 특허에 인용된 특허 (12)

  1. Romey Russell P. (Jacksonville FL) Greer Lonny R. (Jacksonville FL). Adjustable non-piloted air blast fuel nozzle. USP1989064835971.
  2. Armanios Erian A. ; Dancila D. Stefan. Apparatus and method for aerodynamic blowing control using smart materials. USP2000116142425.
  3. Tindell Runyon H. (Old Bethpage NY). Blown boundary layer control system for a jet aircraft. USP1995095447283.
  4. Hartman Neil W. (Tucson AZ). Gas compressor for jet engine. USP1990064930309.
  5. Stebbings,David W.. Gas heat engine. USP2006097111449.
  6. Smereczniak Philip (St. Peters MO) Spetnagel David R. (St. Charles MO). Method and apparatus for controlling the throat area, expansion ratio and thrust vector angle of an aircraft turbine eng. USP1997125694766.
  7. Kutschenreuter ; Jr. Paul H. (Loveland OH) Blanton John C. (West Chester OH). Method of operating a scramjet including integrated inlet and combustor. USP1993105255513.
  8. Guile Roy N. (Wethersfield CT) Peschke William T. (Manchester CT). Piloting igniter for supersonic combustor. USP1989044821512.
  9. Harshman Daniel L. (Forest Park OH). Scramjet combustor. USP1991125072581.
  10. Kutschenreuter ; Jr. Paul H. (Loveland OH) Blanton John C. (West Chester OH). Scramjet including integrated inlet and combustor. USP1992025085048.
  11. Moorhouse, David J.. Structure and method for controlling inlet shock position of a hypersonic vehicle. USP2005046880342.
  12. Gupta, Anurag; Graziosi, Paolo; Mani, Ramani. System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine. USP2003126655632.