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특허 상세정보

Shock suppression supersonic aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/04    B64C-003/28   
미국특허분류(USC) 244/01N ; 244/034R ; 244/045R ; 244/130
출원번호 US-0785684 (1997-01-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Schruhl
인용정보 피인용 횟수 : 21  인용 특허 : 11
초록

The invention is a supersonic aircraft. In detail, the aircraft is in the form of a flying wing having a generally flat upper surface, a generally cosine shaped lower surface and a swept back leading edge. A propulsion system is mounted in the aircraft for providing forward thrust and is adapted to provide a source of pressurized air. A plenum is mounted under and behind the leading edge of the flying wing in a spaced relationship thereto, the plenum having a swept back leading edge and a length substantially equal to the length of the flying wing and a ...

대표
청구항

[ We claim:] [1.] A supersonic aircraft comprising:the aircraft in the form of a flying wing having a generally flat upper surface, a generally cosine shaped lower surface and a swept back leading edge;a propulsion system mounted in the aircraft for providing forward thrust, said propulsion system adapted to provide a source of pressurized air;a plenum mounted under and behind the leading edge of said flying wing in a spaced relationship thereto, having a swept back leading edge and a length substantially equal to the length of said flying wing and a tra...

이 특허를 인용한 특허 피인용횟수: 21

  1. Harbeck, Michael W.; Quayle, Brian. Aircraft fuselage drag reduction blivet. USP2014078783617.
  2. Franklin, III, Walter M.; Morgenstern, John M.; Lee, Howard; Quayle, Brian; Hajic, Ken; Scarcello, John; Arslan, Alan E.. Aircraft tail configuration for sonic boom reduction. USP2004116824092.
  3. Warnica, David; Koning, Albert J.; Franceschini, Michael; Woloshyn, Jennifer. Apparatus for stabilization and deceleration of supersonic flow incorporating a diverging nozzle and perforated plate. USP2012058176941.
  4. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  5. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  6. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  7. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  8. Lebas, Guillaume. Jet engine nacelle for a supersonic aircraft. USP2009127631836.
  9. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  10. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  11. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  12. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  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. USP2015049016632.
  14. Hartmann, Tom. Passive aerodynamic sonic boom suppression for supersonic aircraft. USP2003076588703.
  15. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  16. Chang, Ming; Meza, Victor; Morgenstern, John M.; Arslan, Alan E.. Supersonic aircraft with channel relief control. USP2005076921045.
  17. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  18. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  19. Crosta, Franck; Prat, Damien. Turboshaft engine that reduces rear noise emissions. USP2010027654363.
  20. Ronald G. Meschino CA. Wing combination for drag reduction, aircraft including such a wing, and a method of reducing the drag of an existing aircraft. USP2002016340134.
  21. Quayle,Brian; Morgenstern,John M.; Arslan,Alan E.. Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction. USP2007057216830.