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특허 상세정보

Pulse detonation cluster engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64B-001/24   
미국특허분류(USC) 244/053R; 60/247; 60/03978
출원번호 US-0612727 (2000-07-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bracewell & Patterson, L.L.P.
인용정보 피인용 횟수 : 14  인용 특허 : 7
초록

A pulse detonation cluster includes a cluster housing and a plurality of pulse detonation engines mounted within the housing. Each pulse detonation engine has an inner tubular housing rigidly and concentrically mounted within a cylindrical bore of an outer tubular housing. The inner housing has a plurality of inner housing ports, and the outer housing has a plurality of outer housing ports. A detonation chamber is formed in the annulus between the inner housing and the outer housing. An outer valve sleeve is rotatably mounted to the outer housing for sel...

대표
청구항

1. An aircraft having wings and a fuselage comprising:a pulse detonation cluster having a cluster housing and a plurality of pulse detonation engines mounted within the cluster housing, each engine having a detonation chamber and at least one valve for admitting air to the detonation chamber, the pulse detonation cluster also having a common drive member driven by an external drive system, the common drive member simultaneously moving the valves of the pulse detonation engines; a fuel injection system carried by the aircraft for delivering fuel to each o...

이 특허를 인용한 특허 피인용횟수: 14

  1. Leyva,Ivett Alejancra; Dean,Anthony John. Aircraft and detonative engine incorporating pulse detonation engines. USP2006087093794.
  2. Butler, Lawrence; Johnson, James Edward; Dunbar, Lawrence Wayne. Combined cycle pulse detonation turbine engine. USP2003126666018.
  3. Pinard,Pierre Francois; Dean,Anthony John; Rasheed,Adam. Detonation damper for pulse detonation engines. USP2006067055308.
  4. Guinan, Daniel P.; Gettinger, Christopher D.. Helical cross flow (HCF) pulse detonation engine. USP2017089726080.
  5. Pais,Salvatore. Laser augmented turbojet propulsion system. USP2006077080504.
  6. Ouellette,Richard P. Linear acoustic pulsejet. USP2008097427048.
  7. Edelman, Raymond B.; Lander, Herbert R.; Hunt, Jeffrey H.. Method to initiate multiple chamber detonation wave combustors. USP2012018091336.
  8. Kraft, Robert Eugene. Methods and apparatus for operating gas turbine engines. USP2004116813878.
  9. Kraft,Robert Eugene. Methods and apparatus for operating gas turbine engines. USP2006037007455.
  10. Kraft,Robert Eugene. Methods for operating gas turbine engines. USP2006097100377.
  11. Rasheed, Adam; Dean, Anthony John. Multiple tube pulse detonation engine turbine apparatus and system. USP2010087784265.
  12. Rasheed, Adam; Dean, Anthony John; Pinard, Peirre Francois; Vandervort, Christian Lee; Tangirala, Venkat Eswarlu. Pulse detonation engine bypass and cooling flow with downstream mixing volume. USP2010117841167.
  13. Boespflug, Matthew Patrick; Steenburgh, Dennis; Saddoughi, Seyed Gholami; Bennett, Grover Andrew. Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production. USP2012068205433.
  14. Knight,Andrew F.. Super-staged and continuously staged rocket. USP2006027000377.