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특허 상세정보

Pulse detonation engine system for driving turbine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/22    F02C-007/26   
미국특허분류(USC) 060/776; 060/039.38
출원번호 US-0511906 (2004-02-10)
등록번호 US-7367194 (2008-05-06)
우선권정보 JP-2003-033253(2003-02-12); JP-2003-033301(2003-02-12); JP-2003-144087(2003-05-21); JP-2003-424454(2003-12-22)
국제출원번호 PCT/JP04/001426 (2004-02-10)
§371/§102 date 20041020 (20041020)
국제공개번호 WO04/072451 (2004-08-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Oblon, Spivak, McClelland, Maier & Neustadt, P.C.
인용정보 피인용 횟수 : 6  인용 특허 : 15
초록

A pulse detonation engine system (1) for driving a turbine is comprises a detonation generator section (5) including a detonation tube (7) having a tubular hollow section for permitting detonation to be generated therein during combustion stage of a mixture gas combined with a gas and a fuel, a gas supply section (17) for feeding the gas into the tubular hollow section of the detonation tube (7) at given time intervals, a fuel valve (19) for feeding the fuel into the tubular hollow section of the detonation tube (7) at the given time intervals, and an ig...

대표
청구항

The invention claimed is: 1. A pulse detonation engine system, comprising: a pulse detonation generator including a detonation tube having a tubular hollow section configured to generate a detonation wave therein during a combustion process of a mixture gas combined with a gas and a fuel, a gas supply section configured to feed the gas into the tubular hollow section of the detonation tube at a given time interval, a fuel supply section configured to feed the fuel into the tubular hollow section of the detonation tube at a given time interval, and an ig...

이 특허에 인용된 특허 (15)

  1. Goldmeer,Jeffrey S.; Girodet,William H.. Closed-loop cooling system for a hydrogen/oxygen based combustor. USP2007027178339.
  2. Butler, Lawrence; Johnson, James Edward; Dunbar, Lawrence Wayne. Combined cycle pulse detonation turbine engine. USP2003126666018.
  3. Nordeen,Craig A.; Norris,James W.; Twelves, Jr.,Wendell V.. Combustion ignition. USP2006057047724.
  4. Orlando,Robert Joseph; Venkataramani,Kattalaicheri Srinivasan; Lee,Ching Pang. Gas turbine engine having improved core system. USP2006087093446.
  5. Anderson J. Hilbert. High pressure gas cycle and powder plant. USP2001016167693.
  6. Schick,Louis Andrew; Dean,Anthony John. Hybrid fuel cell-pulse detonation power system. USP2006127150143.
  7. Baycura Orestes M. (2238 Central Park Dr. Campbell CA 95008). Low noise gas turbine. USP1979114175380.
  8. Hunter, Jr., Louis G.. MAPP gas fuel for flight vehicles having pulse detonation engines and method of use. USP2003076584761.
  9. Kraft,Robert Eugene. Methods and apparatus for operating gas turbine engines. USP2006037007455.
  10. Dean,Anthony John; McManus,Keith Robert; Tangirala,Venkat Eswarlu. Multiple detonation initiator for frequency multiplied pulsed detonation combustion. USP2006117131260.
  11. Bussing Thomas R. A.. Pulse detonation electrical power generation apparatus with water injection. USP2000056062018.
  12. Norris, James W.; Twelves, Jr., Wendell V.. Pulsed combustion engine. USP2005056886325.
  13. Sammann,Bradley C.; Twelves, Jr.,Wendell V.; Jones,Gary D.; Norris,James W.; Klein,Harvey L.; Jones,James E.; Kramer,Stephen K.; Thonebe,Douglas A.. Pulsed combustion engine. USP2006097100360.
  14. Venkataramani,Kattalaicheri Srinivasan; Butler,Lawrence; Lee,Ching Pang. Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine. USP2006107124573.
  15. Bussing Thomas R. A. (Issaquah WA). Rotary valve multiple combustor pulse detonation engine. USP1996055513489.