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특허 상세정보

Annular pulse detonation apparatus and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-007/02   
미국특허분류(USC) 60/204 ; 60/247 ; 60/3978
출원번호 US-0265384 (1994-06-24)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 28  인용 특허 : 0
초록

A pulse detonation apparatus utilizes a rotatable core feed cylinder. The core feed cylinder is carried within a inner sidewall of a stationary annular detonation chamber. The core feed cylinder has ports in the sidewall that will register with ports in the inner sidewall of the annular detonation chamber at least once each revolution. A fuel valve means mounted to the outer sidewall of the annular detonation chamber supplies pulses of gaseous fuel. The oxygen content at the forward end of the detonation chamber is richer than toward the rearward end. Th...

대표
청구항

A method of creating a high pressure discharge, comprising: (a) providing a core feed cylinder having a longitudinal axis, a forward end, a rearward end, a sidewall, an inlet port extending through the forward end, and an outlet port in the sidewall, (b) mounting the core feed cylinder within an annular detonation chamber having an inner sidewall that sealingly and rotatably receives the core feed cylinder, an outer sidewall spaced radially outward from the inner sidewall, a closed forward end and an open rearward end, defining an annular detonation cavi...

이 특허를 인용한 특허 피인용횟수: 28

  1. Louis G. Hunter, Jr. ; Kent W. Benner. Annular liquid fueled pulse detonation engine. USP2002026349538.
  2. Louis G. Hunter ; Billy D. Couch ; Paul E. Hagseth. Combined cycle pulse combustion/gas turbine engine. USP2002116477829.
  3. Nordeen,Craig A.; Norris,James W.; Twelves, Jr.,Wendell V.. Combustion ignition. USP2006057047724.
  4. Highsmith, Thomas K.; Blair, Michael D.; Wassom, Steven R.; Starrett, William D.; Dever, Joel. Digital solid rocket motor and gas generator. USP2004036705075.
  5. Hunter, Jr., Louis G.. MAPP gas fuel for flight vehicles having pulse detonation engines and method of use. USP2003076584761.
  6. Gregory Vincent Meholic ; William Randolph Stowell. Magnetohydrodynamic flow control for pulse detonation engines. USP2002116484492.
  7. Edelman, Raymond B.; Lander, Herbert R.; Hunt, Jeffrey H.. Method to initiate multiple chamber detonation wave combustors. USP2012018091336.
  8. Don D. Winfree ; Louis G. Hunter, Jr. ; Billy D. Couch. Pulse detonation cluster engine. USP2002086439503.
  9. Winfree Don D. ; Hunter ; Jr. Louis G.. Pulse detonation igniter for pulse detonation chambers. USP1999085937635.
  10. Norris, James W.; Twelves, Jr., Wendell V.. Pulsed combustion engine. USP2005056886325.
  11. 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.
  12. Sammann, Bradley C.; Twelves, Jr., Wendell V.; Jones, Gary D.. Pulsed combustion turbine engine. USP2005066901738.
  13. Thomas A. Kaemming ; Paul G. Willhite. Pulsed detonation engine with backpressure. USP2002126494034.
  14. Thomas A. Kaemming ; Paul G. Willhite ; Richard S. Dyer ; Michael A. Guntorius. Pulsed detonation engine with divergent inflow transition section. USP2002096446428.
  15. Thomas A. Kaemming ; Paul G. Willhite ; Richard S. Dyer ; Michael A. Guntorius. Pulsed detonation engine with ejector bypass. USP2002026347509.
  16. Sanders, Bobby W.; Weir, Lois J.. Rotary inlet flow controller for pulse detonation combustion engines. USP2003106637187.
  17. Fullerton, Larry W; Teel, James L; Thompson, Jr., Herman M. System and method for accelerating a mass using a pressure produced by a detonation. USP2017029581704.
  18. Fullerton, Larry W.. System and method for generating and controlling conducted acoustic waves for geophysical exploration. USP2012108292022.
  19. Fullerton, Larry W.. System and method for generating and controlling conducted acoustic waves for geophysical exploration. USP2012118302730.
  20. Fullerton, Larry W.. System and method for generating and directing very loud sounds. USP2012058172034.
  21. Fullerton, Larry W.. System and method for generating and directing very loud sounds. USP2011027882926.
  22. Fullerton, Larry W.. System and method for ignition of a gaseous or dispersed fuel-oxidant mixture. USP2012038136624.
  23. Fullerton, Larry W.. System and method for ignition of a gaseous or dispersed fuel-oxidant mixture. USP2011027886866.
  24. Fullerton, Larry W.; Teel, James L.; Thompson, Jr., Herman M.. System for coupling an overpressure wave to a target media. USP2014128905186.
  25. Hunter, Louis G.; Miller, Daniel N.; Hagseth, Paul E.. System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans. USP2004076758032.
  26. Ouellette, Richard P.; Kutzmann, Aaron J.. Vertical takeoff and landing aircraft. USP2004116824097.
  27. Ouellette, Richard P.; Kutzmann, Aaron J.. Vertical takeoff and landing aircraft. USP2005126976654.
  28. Ouellette, Richard P.; Kutzmann, Aaron J.. Vertical takeoff and landing aircraft. USP2005086926231.