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특허 상세정보

Annular vortex slinger combustor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/00    F23R-003/12   
미국특허분류(USC) 60/3936 ; 60/732 ; 60/755
출원번호 US-0559423 (1991-07-26)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 31  인용 특허 : 3
초록

A circumferentially stirred variable residence time vortex slinger combuster, includes a primary combustion chamber for containing an annular combustion vortex and a first group of louvres peripherally disposed about the primary combustion chamber and distributed along its primary axis. The louvres are 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 combustor vortex in a helical path, and to feed combustion in the pri...

대표
청구항

A circumferentially stirred variable residence time vortex slinger combustor comprising: a primary annular combustion chamber including inner primary and outer primary walls for containing an annular combustion vortex, one of said inner primary walls and said outer primary walls defining a first group of louvres peripherally disposed about said primary combustion chamber and longitudinally distributed along its primary axis, said louvres inclined to impel air circumferentially about the primary axis within said primary combustion chamber to cool its inte...

이 특허를 인용한 특허 피인용횟수: 31

  1. Wagner, Joel H.; Lutjen, Paul M.. 3D non-axisymmetric combustor liner. USP2014048707708.
  2. Teets, J. Michael. Annular combustor for use with an energy system. USP2005016845621.
  3. Condevaux, Jamey J.; Simpkins, Lisa M.; Sordyl, John. Combustion system. USP2016059328924.
  4. Condevaux, Jamey J.; Simpkins, Lisa M.; Sordyl, John. Combustion system. USP2014028640464.
  5. Critchley, Ian L.; Yankowich, Paul R.; Tyrer, Kenneth R.. Combustion systems with rotary fuel slingers. USP2010077762072.
  6. Stastny,Honza; Sze,Robert. Combustor exit duct. USP2007097269958.
  7. Morenko, Oleg. Combustor for gas turbine engine. USP2017019541292.
  8. Prociw, Lev Alexander; Hu, Tin Cheung John. Combustor for gas turbine engine. USP2018059958161.
  9. Prociw, Lev Alexander; Zabeti, Parham. Combustor for gas turbine engine. USP2016019228747.
  10. Prociw, Lev Alexander; Zabeti, Parham; Hu, Tin Cheung John. Combustor for gas turbine engine. USP2015099127843.
  11. Hawie, Eduardo; Sze, Robert. Combustor with chamfered dome. USP2012058171736.
  12. Oechsle, Victor L.. Gas turbine engine and combustor. USP2014078776525.
  13. Bunker, Ronald Scott. Gas turbine engine and method of operating thereof. USP2016059328663.
  14. Willis, Jeffrey W.; Pont, Guillermo; Toby, Benjamin E.; McKeirnan, Jr., Robert D.. Gas turbine engine having a multi-stage multi-plane combustion system. USP2004026684642.
  15. Patel, Bhawan B.; Morenko, Oleg. Hybrid slinger combustion system. USP2018019874148.
  16. Patel, Bhawan B.; Morenko, Oleg. Hybrid slinger combustion system. USP2013078479492.
  17. Patel, Bhawan B.; Morenko, Oleg. Hybrid slinger combustion system. USP2014038677731.
  18. Willis Jeffrey W. ; Pont Guillermo ; Alder ; Jr. Bruce L.. Low emissions combustion system for a gas turbine engine. USP1998125850732.
  19. Jeffery W. Willis ; Guillermo Pont ; Benjamin E. Toby ; Robert D. McKeirnan, Jr.. Multi-stage multi-plane combustion system for a gas turbine engine. USP2002096453658.
  20. Teets, Joseph Michael. Radially staged RQL combustor with tangential fuel-air premixers. USP2014048701416.
  21. Harris, Mark M.. Rotary cup fuel injector. USP2010037685822.
  22. Lawlor, Shawn P.; Steele, Robert C.; Kendrick, Donald. Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall. USP2004026694743.
  23. Patel, Bhawan B.; Morenko, Oleg. Slinger combustor. USP2016069366187.
  24. Harris, Mark M.; Brown, Wesley D.; Garcia, Angel M.. Small gas turbine engine with multiple burn zones. USP2009087568343.
  25. Harris, Mark M.; Brown, Wesley D.; Garcie, Angel M.. Small gas turbine engine with multiple burn zones. USP2012068196407.
  26. Wiebe, David J.. Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine. USP2017119810434.
  27. Kendrick,Donald; Lawlor,Shawn P.; Steele,Robert C.. Trapped vortex combustor. USP2006027003961.
  28. Callas, James J.; White, David J.. Turbine engine having folded annular jet combustor. USP2011098015814.
  29. Buret, Michel Roger; Cazalens, Michel Pierre; Hernandez, Didier Hippolyte. Turbomachine with angular air delivery. USP2009067549294.
  30. 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.
  31. 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.