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특허 상세정보

Annular vortex combustor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/14   
미국특허분류(USC) 60/39464 ; 60/732 ; 60/748 ; 60/755
출원번호 US-0550800 (1990-07-10)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 23  인용 특허 : 3
초록

A circumferentially stirred variable residence time vortex combustor including a primary combustion chamber for containing an annular combustion vortex and a first plurality of louvres peripherally disposed about the primary combuston chamber and longitudinally distributed along its primary axis, the louvres inclined to impel air circumferentially about the primary axis within the primary combustion chamber, to cool its interior surfaces, to impel air inwardly to assist in driving the annular combustion vortex in a helical path, and to feed combustion in...

대표
청구항

A circumferentially stirred variable residence time vortex combustor comprising: a toroidal shaped primary annular combustion chamber disposed around a primary axis in the X-direction including an inner primary wall and an outer primary wall for containing an annular combustion vortex, at least one of said inner primary and said outer primary walls defining a first plurality of louvres peripherally disposed about said primary combustion chamber and longitudinally distributed along its primary axis, said louvres inclined to impel air circumferentially abo...

이 특허를 인용한 특허 피인용횟수: 23

  1. De Sousa, Mario Cesar; Hernandez, Didier Hippolyte; Noel, Thomas Olivier Marie. Annular combustion chamber of a turbomachine. USP2010097788928.
  2. Teets, J. Michael. Annular combustor for use with an energy system. USP2005016845621.
  3. Spytek, Christopher J.. Apparatus and method for a gas turbine entrainment system. USP2011098015821.
  4. Craig Joe D. (P.O. Box 70 Tahoka TX 79373). Biomass gasification system and method. USP1997095666890.
  5. Popovic, Predrag; Hessler, William Kirk; Venkataraman, Krishna Kumar. Centerbody cap for a turbomachine combustor and method. USP2011098020385.
  6. Morenko, Oleg. Combustor for gas turbine engine. USP2017019541292.
  7. Prociw, Lev Alexander; Hu, Tin Cheung John. Combustor for gas turbine engine. USP2018059958161.
  8. Prociw, Lev Alexander; Zabeti, Parham. Combustor for gas turbine engine. USP20190210208956.
  9. Yuasa, Saburo; Sakurai, Takashi; Murayama, Motohide; Minakawa, Katsuhiro. Gas turbine combustor. USP2015059038392.
  10. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D.. Gas turbine engine having a multi-stage multi-plane combustion system. USP2004026684642.
  11. Haehnle, Hartmut; Jones, Russell Bond; Vogel, Gregory; Tschuor, Remigi. Gas turbine having an improved cooling architecture. USP2013048413449.
  12. Willis Jeffrey W. ; Pont Guillermo ; Alder ; Jr. Bruce L.. Low emissions combustion system for a gas turbine engine. USP1998125850732.
  13. Venkataraman, Krishna K.; Hessler, William Kirk; Popovic, Predrag. Low emissions gas turbine combustor. USP2011108028529.
  14. Ingram, Joe Britt. Microturbine with auxiliary air tubes for NOx emission reduction. USP2004056729141.
  15. Jeffery W. Willis ; Guillermo Pont ; Benjamin E. Toby ; Robert D. McKeirnan, Jr.. Multi-stage multi-plane combustion system for a gas turbine engine. USP2002096453658.
  16. Teets, Joseph Michael. Radially staged RQL combustor with tangential fuel-air premixers. USP2014048701416.
  17. Lawlor, Shawn P.; Steele, Robert C.; Kendrick, Donald. Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall. USP2004026694743.
  18. Monahan, Sarah Marie; Joshi, Narendra Digamber; Tangirala, Venkat Eswarlu; Masquelet, Matthieu Marc. Trapped vortex cavity staging in a combustor. USP20180910072846.
  19. Kendrick,Donald; Lawlor,Shawn P.; Steele,Robert C.. Trapped vortex combustor. USP2006027003961.
  20. Cameriano, Laurent Bernard; Cazalens, Michel Pierre; Duval, Sylvain; Lunel, Romain Nicolas. Turbomachine combustion chamber with helical air flow. USP2010037673456.
  21. Cazalens, Michel Pierre; Lunel, Romain Nicolas. Turbomachine combustion chamber with helical air flow. USP2009117614234.
  22. Steele, Robert C.; Edmonds, Ryan G.; Williams, Joseph T.; Baldwin, Stephen P.. Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel. USP2012118312725.
  23. Steele, Robert C.; Edmonds, Ryan G.; Williams, Joseph T.; Baldwin, Stephen P.. Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel. USP2009107603841.