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특허 상세정보

Rotary valve multiple combustor pulse detonation engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-005/02   
미국특허분류(USC) 60/3938 ; 60/3939 ; 60/3976 ; 60/3978
출원번호 US-0045771 (1993-04-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 54  인용 특허 : 0
초록

A pulse detonation engine is provided with several detonation combustors selectively coupled to an air inlet and fuel source by a rotary valve. The rotary valve isolates the steady operation of the air inlet and fuel system from the unsteady nature of the detonation process, and allows the fueling of some of the detonation chambers while detonation occurs in other detonation chambers. The fuel system may use a solid fueled gas generator.

대표
청구항

A rotary valve multiple combustor pulse detonation engine comprising: at least two detonation chambers, each having an inlet end and an outlet end; a fuel manifold for supplying fuel from a fuel source to said at least two detonation chambers at said inlet ends; an inlet air duct manifold for supplying air to said at least two detonation chambers at said inlet ends; means for initiating a pulsed supersonic shock wave-triggered detonation combustion wave for initiating detonation in said at least two detonation chambers; and a rotor disk valve having at l...

이 특허를 인용한 특허 피인용횟수: 54

  1. Louis G. Hunter, Jr. ; Kent W. Benner. Annular liquid fueled pulse detonation engine. USP2002026349538.
  2. Buchheim, Robert K.. Apparatus comprising a rotary-acting pilot valve. USP2005116962323.
  3. Louis G. Hunter ; Billy D. Couch ; Paul E. Hagseth. Combined cycle pulse combustion/gas turbine engine. USP2002116477829.
  4. Tangirala, Venkat Eswarlu; Janssen, Jonathan Sebastian; Dean, Anthony John. Compact, low pressure-drop shock-driven combustor and rocket booster, pulse detonation based supersonic propulsion system employing the same. USP2010037669406.
  5. Highsmith, Thomas K.; Blair, Michael D.; Wassom, Steven R.; Starrett, William D.; Dever, Joel. Digital solid rocket motor and gas generator. USP2004036705075.
  6. Lewis Brian F.. Direct fired compressor and method of producing compressed air. USP2001046212875.
  7. Uhm, Jong Ho; Johnson, Thomas Edward. Fuel nozzle assembly for use in turbine engines and methods of assembling same. USP2015028943832.
  8. Janssen, Jonathan Sebastian; Tangirala, Venkat Eswarlu; Dean, Anthony John; Wiedenhoefer, James Fredric. Inlet airflow management system for a pulse detonation engine for supersonic applications. USP2011027891164.
  9. Venkataramani, Kattalaicheri Srinivasan; Butler, Lawrence; Lee, Ching Pang; Maclin, Harvey Michael. Integral pulse detonation system for a gas turbine engine. USP2005066904750.
  10. Eidelman, Shmuel; Charov, Dmitri. Method and apparatus for improving the efficiency of pulsed detonation engines. USP2003126662550.
  11. Henry,John Leslie. Methods and apparatus for generating gas turbine engine thrust using a pulse detonator. USP2007067228683.
  12. Nalim, Razi; Akbari, Pezhman. Pilot fuel injection for a wave rotor engine. USP2013058443583.
  13. Baker, Von David. Propulsion module. USP2003076584764.
  14. Rasheed, Adam; Dean, Anthony John; Vandervort, Christian Lee. Pulse detonation assembly and hybrid engine. USP2010107818956.
  15. Baker, Von David; Rezy, Bernie Joseph. Pulse detonation bypass engine propulsion pod. USP2003126668542.
  16. Bussing Thomas R. A.. Pulse detonation electrical power generation apparatus with water injection. USP2000056062018.
  17. Tew, David E.; Anderson, Torger J.; Guile, Roy N.; Sobel, David R.; Twelves, Jr., Wendell V.; Jones, Gary D.. Pulse detonation engine having an aerodynamic valve. USP2003076584765.
  18. Tew, David E.; Twelves, Jr., Wendell V.. Pulse detonation engine having an aerodynamic valve. USP2005046883543.
  19. Brzek, Brian Gene; Rasheed, Adam; Joshi, Narendra Digamber. Pulse detonation system. USP2015028955303.
  20. Butler, Lawrence; Venkataramani, Kattalaicheri Srinivasan; Murrow, Kurt David; Leyva, Ivett Alejandra. Pulse detonation system for a gas turbine engine. USP2005056889505.
  21. Venkataramani, Kattalaicheri Srinivasan; Butler, Lawrence; Bailey, William Andrew. Pulse detonation system for a gas turbine engine. USP2005086928804.
  22. Venkataramani,Kattalaicheri Srinivasan; Butler,Lawrence; Davidson,James Paul. Pulse detonation system for a gas turbine engine having multiple spools. USP2008027328570.
  23. Hinkey John B. ; Williams Joseph T. ; Bussing Thomas R.A.. Pulsed combustion acoustic wave generator. USP1999015864517.
  24. Thomas A. Kaemming ; Paul G. Willhite. Pulsed detonation engine with backpressure. USP2002126494034.
  25. Thomas A. Kaemming ; Paul G. Willhite ; Richard S. Dyer ; Michael A. Guntorius. Pulsed detonation engine with divergent inflow transition section. USP2002096446428.
  26. Thomas A. Kaemming ; Paul G. Willhite ; Richard S. Dyer ; Michael A. Guntorius. Pulsed detonation engine with ejector bypass. USP2002026347509.
  27. Bussing Thomas R. A. ; Bratkovich Thomas E.. Pulsed detonation rocket engine. USP1999025873240.
  28. DeRoche Mark. Repetitive detonation generator. USP1998095800153.
  29. Wiedenhoefer, James Fredric; Rasheed, Adam. Rotary air valve firing patterns for resonance detuning. USP2013018341932.
  30. Horn, Mark David; Havskjold, Glenn L.; Morrison, Jr., Calvin Q.. Rotary engine with exhaust gas supplemental compounding. USP2014048689764.
  31. Callas, James J.; Fiveland, Scott B.. Rotary pulse detonation engine. USP2004046725646.
  32. Venkataramani,Kattalaicheri Srinivasan; Butler,Lawrence; Lee,Ching Pang. Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine. USP2006107124573.
  33. Meholic, Gregory Vincent. Rotary valve for pulse detonation engines. USP2003016505462.
  34. Kutlucinar Isken. Rotary valve system. USP2001076257191.
  35. Kutlucinar Iskender. Rotary valve system. USP1999105967108.
  36. Venkataramani, Kattalaicheri Srinivasan; Butler, Lawrence; Lee, Ching-Pang; Maclin, Harvey Michael. Rotating pulse detonation system for a gas turbine engine. USP2005086931858.
  37. Johnson,Curtis William. Supersonic revolving nozzle. USP2006016981365.
  38. 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.
  39. Crothers, Sarah Lori; Stoia, Lucas John; Carnell, Jr., William Francis. System and method for control of combustion dynamics in combustion system. USP2017079709279.
  40. Crothers, Sarah Lori; Wilson, Charlotte Cole. System and method for control of combustion dynamics in combustion system. USP2017079709278.
  41. Ziminsky, Willy Steve; Crothers, Sarah Lori. System and method for control of combustion dynamics in combustion system. USP2017129845956.
  42. Fullerton, Larry W.. System and method for generating and controlling conducted acoustic waves for geophysical exploration. USP2012108292022.
  43. Fullerton, Larry W.. System and method for generating and controlling conducted acoustic waves for geophysical exploration. USP2012118302730.
  44. Fullerton, Larry W.. System and method for generating and directing very loud sounds. USP2012058172034.
  45. Fullerton, Larry W.. System and method for generating and directing very loud sounds. USP2011027882926.
  46. Fullerton, Larry W.. System and method for ignition of a gaseous or dispersed fuel-oxidant mixture. USP2012038136624.
  47. Fullerton, Larry W.. System and method for ignition of a gaseous or dispersed fuel-oxidant mixture. USP2011027886866.
  48. Pinard, Pierre Francois; Hinckley, Kevin Michael; Tangirala, Venkat Eswarlu; Rasheed, Adam; Chapin, David Michael; Dean, Anthony John. System and method for passive valving for pulse detonation combustors. USP2014058726630.
  49. Fullerton, Larry W.; Teel, James L.; Thompson, Jr., Herman M.. System for coupling an overpressure wave to a target media. USP2014128905186.
  50. Crothers, Sarah Lori; Flanagan, James Scott; Davis, Jr., Lewis Berkley. Systems and methods for a fuel pressure oscillation device for reduction of coherence. USP2017019551283.
  51. Stevenson, Christian Xavier; Crothers, Sarah Lori. Systems and methods for control of combustion dynamics and modal coupling in gas turbine engine. USP2017059644846.
  52. Crothers, Sarah Lori; Karim, Hasan; Hall, Joel Meador. Systems and methods for control of combustion dynamics in combustion system. USP20181010113747.
  53. Crothers, Sarah Lori; Citeno, Joseph Vincent; Stevenson, Christian Xavier. Systems and methods for variation of injectors for coherence reduction in combustion system. USP2017129845732.
  54. Johnson,Curtis William. Variable geometry nozzle with flexible side wall. USP2006067062901.