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특허 상세정보

Annular combustor for use with an energy system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F23R-00350   
미국특허분류(USC) 060/804; 060/732; 060/749
출원번호 US-0275049 (2001-05-01)
국제출원번호 PCT/US01/14115 (2002-10-31)
§371/§102 date 20021031 (20021031)
국제공개번호 WO01/83963 (2001-11-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Webb Ziesenheim Logsdon Orkin &
인용정보 피인용 횟수 : 15  인용 특허 : 69
초록

An annular combustor has an annular inner shell, an annular outer shell and a dome end wall connecting the inner shell with the outer shell. A dam is positioned between the dome end wall and the exit end and extends radially from at least one of the inner shell and the outer shell to provide a reduced flow area passageway within the combustion chamber.

대표
청구항

1. An annular combustor comprising:a) an annular inner shell having an inner surface and an outer surface; b) a coaxial annular outer shell having an inner surface and an outer surface; c) a dome end wall connecting the inner shell and outer shell, wherein the inner shell, the outer shell and the dome end wall define an annular combustion chamber having a chamber width between the inner surface of the outer shell and the outer surface of the inner shell, wherein the chamber extends along a longitudinal axis and has an exit end opposite the dome end wall;...

이 특허에 인용된 특허 (69)

  1. Shekleton Jack R. (San Diego CA) Sledd Michael W. (Vista CA). Air blast fuel injecton system. USP1994015277022.
  2. Shekleton Jack R. (San Diego CA) Treece William D. (La Mesa CA). Annular combustor. USP1994115363644.
  3. Shah Nipulkumar (San Diego CA) Shekleton Jack R. (San Diego CA). Annular combustor for a turbine engine with tangential passages sized to provide only combustion air. USP1994045303543.
  4. Shekleton Jack R. (San Diego CA) Lafferty Melvin K. (San Diego CA). Annular combustor for a turbine engine without film cooling. USP1992045101620.
  5. Shekleton Jack R. (San Diego CA) Rodgers Colin (San Diego CA) Archibald John P. (LaJolla CA). Annular combustor with tangential cooling air injection. USP1990054928479.
  6. Shekleton Jack R. (San Diego CA) Rodgers Colin (San Diego CA) Archibald John P. (LaJolla CA) Smith Robert W. (Lakeside CA). Annular combustor with tangential cooling air injection. USP199506RE34962.
  7. Melconian Jerry O. (Reading MA). Annular vortex combustor. USP1991065025622.
  8. Melconian Jerry O. (Reading MA). Annular vortex slinger combustor. USP1991034996838.
  9. Shekleton Jack R. (San Diego CA). Coanda phenomena combustor for a turbine engine. USP1992025085039.
  10. Schulte-Werning Burkhard,CHX. Combustion chamber. USP1998045735126.
  11. Dubell Thomas L. (Palm Beach Gardens FL) Shadowen James H. (Riviera Beach FL). Combustor. USP1994035297385.
  12. Shekleton Jack R. (San Diego CA). Combustor with enhanced turbine nozzle cooling. USP1989054825640.
  13. DuBell Thomas L.. Combustor with first and second zones. USP1998055749219.
  14. Shekleton Jack R. (San Diego CA) Lafferty Melvin K. (San Diego CA). Compact gas turbine engine. USP1991075033263.
  15. Shekleton Jack R. (San Diego CA) Lafferty Melvin K. (San Diego CA). Compact gas turbine engine. USP1996115577380.
  16. Shekleton Jack R. (San Diego CA). Cooling of turbine nozzle containment ring. USP1992075129224.
  17. Shekleton Jack R. (San Diego CA) Johnson Douglas C. (Rockford IL). Cooling of turbine nozzles. USP1991115062262.
  18. Jorgensen Robert A. (Clifton Park NY) Farrell Roger A. (Schenectady NY) Gerhold Bruce W. (Rexford NY). Dual stage-dual mode low emission gas turbine combustion system. USP1983124420929.
  19. Wilkes Colin (Scotia NY) Hilt Milton B. (Sloansville NY). Dual stage-dual mode low nox combustor. USP1981104292801.
  20. Shekleton Jack R. (San Diego CA). Dual zone combustor fuel injection. USP1992115163284.
  21. Shekleton Jack R. (San Diego CA). Dual zone single manifold fuel injection system. USP1993015177955.
  22. Kawaguchi Katsuyuki (Nagasaki JA). Fuel combustion apparatus. USP1977104054028.
  23. Shekleton Jack R. (San Diego CA). Gas turbine annular combustor. USP1992055113647.
  24. Shekelton Jack R. (San Diego CA) Johnson Douglas C. (Corona CA). Gas turbine annular combustor with radial dilution air injection. USP1991105058375.
  25. Heitmann Arnold M. (Swampscott MA) Brassert Walter L. (Belmont MA) Chouinard Donald N. (Peabody MA). Gas turbine combustion chamber arrangement. USP1977084040251.
  26. Shekleton Jack R. (San Diego CA) Lafferty Melvin K. (San Diego CA). Gas turbine engine with fuel mainfold system. USP1992085140808.
  27. Melconian Jerry O. (South Hamilton MA) Watkins Sidney C. (Bloomfield CT). Gas turbine engines with toroidal combustors. USP1979054151709.
  28. Shekleton Jack R. (San Diego CA) Sachrison Steven A. (San Diego CA). High altitude starting two-stage fuel injection apparatus. USP1993115261224.
  29. Schelp Helmut R. (Pacific Palisades CA). High temperature gas turbine. USP1977084041699.
  30. Taylor Jack R. (Cincinnati OH). Low NOx combustor. USP1987104698963.
  31. Moreno Frederick E. (Los Altos CA). Low NOx staged combustor with swirl suppression. USP1988114784600.
  32. Shekleton Jack R. (San Diego CA) Johnson Douglas C. (San Diego CA) Lafferty Melvin K. (San Diego CA). Low cost annular combustor. USP1989014794754.
  33. Willis Jeffrey W. ; Pont Guillermo ; Alder ; Jr. Bruce L.. Low emissions combustion system for a gas turbine engine. USP1998125850732.
  34. DeCorso Serafino M. (Upper Providence Township ; Delaware County PA). Low-nox, rich-lean combustor. USP1988114787208.
  35. Schirmer Robert M. (Bartlesville OK) Alquist Henry E. (Bartlesville OK) Fromm Ellsworth H. (Bartlesville OK). Method and apparatus for burning nitrogen-containing fuels. USP1988014721454.
  36. Colket ; III Meredith B. (Simsbury CT) Kesten Arthur S. (West Hartford CT) Sangiovanni Joseph J. (West Suffield CT) Zabielski Martin F. (Manchester CT) Pandy Dennis R. (South Windsor CT) Seery Daniel. Method and system for combusting hydrocarbon fuels with low pollutant emissions by controllably extracting heat from the. USP1993085235804.
  37. Spadaccini Louis J. (Manchester CT) Rosfjord Thomas J. (South Windsor CT). Method and system for staged rich/lean combustion. USP1993055207053.
  38. Korenberg Jacob (York PA). Method of combustion and combustion apparatus to minimize Nox and CO emissions from a gas turbine. USP1994025285628.
  39. Shekleton Jack R. (San Diego CA). Method of obtaining a desired temperature profile in a turbine engine and turbine engine incorporating the same. USP1994075331803.
  40. Shaw Henry (Scotch Plains NJ) Skopp Alvin (Clark NJ). Minimizing NOx production in operation of gas turbine combustors. USP1981084285193.
  41. Becker Bernard (Lothringer Weg 2N ; D-4330 Mlheim/Ruhr DEX). Multi-stage combustion chamber for combustion of nitrogen-containing gas with reduced NOx emissions, and m. USP1991035002483.
  42. Becker Bernard (Mlheim/Ruhr DEX). Multi-stage combustion chamber for combustion of nitrogen-containing gas with reduced NOx emissions, and m. USP1991105052919.
  43. Jeffery W. Willis ; Guillermo Pont ; Benjamin E. Toby ; Robert D. McKeirnan, Jr.. Multi-stage multi-plane combustion system for a gas turbine engine. USP2002096453658.
  44. Waslo Jennifer (Scotia NY) Kuwata Masayoshi (Ballston Lake NY) Washam Roy M. (Schenectady NY). Premixed pilot nozzle for dry low Nox combustor. USP1991014982570.
  45. Feitelberg Alan S. ; Schmidt Mark Christopher ; Goebel Steven George. Rapid-quench axially staged combustor. USP1999125996351.
  46. Massarani Madhat. Rich-quench-lean combustor for use with a fuel having a high vanadium content and jet engine or gas turbine system havi. USP1998105819540.
  47. Toon, Ian J.; O'Dell, Stephen J.; Currin, John H.; Willis, Jeffrey D.. Staged gas turbine combustion chamber with counter swirling arrays of radial vanes having interjacent fuel injection. USP1994065319935.
  48. Moreno Frederick E. (Los Altos CA) Joshi Narendra D. (Phoenix AZ). Staged lean premix low nox hot wall gas turbine combustor with improved turndown capability. USP1990034910957.
  49. Joshi Narendra D. (Phoenix AZ) Moreno Frederick E. (Los Altos CA) Hartman Creighton D. (San Francisco CA). Staged low NOxgas turbine combustor. USP1990044912931.
  50. Schultz Donald F. (Middleburg Hts. OH). Steam cooled rich-burn combustor liner. USP1989044819438.
  51. Ansart Denis R. H. (Bois le Roi FRX) Bayle Laboure Grard J. P. (Avon FRX) Maunand Jacques L. M. (Saint Forget FRX) Sandelis Denis J. M. (Nangis FRX). System for reducing nitrogen-oxide emissions from a gas turbine engine. USP1994025285630.
  52. Shorb Linn C. (San Diego CA) Sledd Michael W. (San Diego CA) Shekleton Jack R. (San Diego CA). Tangentially directed air assisted fuel injection and small annular combustors for turbines. USP1994065317864.
  53. Robertson ; Jr. Arichbald Stuart ; Lu Chongqing ; Fan Zhen. Topping combustor for low oxygen vitiated air streams. USP1999095950417.
  54. Beebe Kenneth W. (Sartoga NY). Transpiration cooled throat section for low NOx combustor and related process. USP1992075127221.
  55. Ekstedt Edward E. (Montgomery OH) Joshi Narendra D. (Cincinnati OH) Ablett Adrian M. (Cincinnati OH) Gresla Timothy R. (Cincinnati OH) Koshoffer John M. (Cincinnati OH) Burke William F. (Marlborough . Triple annular combustor for gas turbine engine. USP1994065323604.
  56. Shekleton Jack R. (San Diego CA) LeCren Richard T. (San Diego CA). Turbine combustor with tangential fuel injection and bender jets. USP1990014891936.
  57. Shekleton Jack R. (San Diego CA). Turbine engine with airblast injection. USP1993115263316.
  58. Shekleton Jack R. (San Diego CA). Turbine engine with high efficiency fuel atomization. USP1991024989404.
  59. Shekleton Jack R. (San Diego CA). Turbine engine with high efficiency fuel atomization. USP1990114967562.
  60. Shekleton Jack R. (San Diego CA) Sachrison Steven A. (La Jolla CA) Sledd Michael W. (Vista CA). Turbine engine with start injector. USP1991075027603.
  61. Shekleton Jack R. ; Rodgers Colin. Turbine including a stored energy combustor. USP1999075927066.
  62. Shekleton Jack R. (San Diego CA). Turbine wheel and nozzle cooling. USP1990084949545.
  63. Shekleton Jack R. (San Diego CA). Ultra high altitude starting compact combustor. USP1993015177956.
  64. Shekleton Jack R. (San Diego CA). Unitized fuel manifold and injector for a turbine engine. USP1992095150570.
  65. Gocke Eberhard (Mosbach DT) Vollmer Rudolf (Mosbach DT). Valve structure. USP1977034013088.
  66. Melconian Jerry O. (76 Beaver Rd. Reading MA 01867). Variable residence time vortex combustor. USP1987104702073.
  67. Shekleton Jack R. (San Diego CA). Very high altitude turbine combustor. USP1995105456080.
  68. Shekleton Jack R. (San Diego CA) Rodgers Colin (San Diego CA). Volume enhanced turbine engine combustion zone. USP1992125172546.
  69. Shekleton Jack R. (San Diego CA) Rodgers Colin (San Diego CA). Volume enhanced turbine engine combustion zone. USP1993055207055.

이 특허를 인용한 특허 피인용횟수: 15

  1. Charron, Richard. Canted outlet for transition in a gas turbine engine. USP2012018091365.
  2. Kesseli, James B.; Nash, James S.. Ceramic-to-metal turbine shaft attachment. USP2015069051873.
  3. Baldwin, Matthew Stephen. Ceramic-to-metal turbine volute attachment for a gas turbine engine. USP20181010094288.
  4. Brooks, Robert T.. Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine. USP2017099771813.
  5. Wiebe, David J.; Carlson, Andrew; Stoker, Kyle C.. Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine. USP2017109803487.
  6. Donnelly, Frank Wegner; Dewis, David William. Dispatchable power from a renewable energy facility. USP2014108866334.
  7. Yuasa, Saburo; Sakurai, Takashi; Murayama, Motohide; Minakawa, Katsuhiro. Gas turbine combustor. USP2015059038392.
  8. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Upton, Timothy; Watson, John D.. Gas turbine energy storage and conversion system. USP2013088499874.
  9. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Watson, John D.. Gas turbine energy storage and conversion system. USP2014048708083.
  10. Donnelly, Frank Wegner; Dewis, David William. Gas turbine engine configurations. USP2014038669670.
  11. Kesseli, James B.; Baldwin, Matthew Stephen. Metallic ceramic spool for a gas turbine engine. USP2015038984895.
  12. Teets, Joseph Michael. Radially staged RQL combustor with tangential fuel-air premixers. USP2014048701416.
  13. Charron, Richard. Structural attachment system for transition duct outlet. USP2013128616007.
  14. Charron, Richard; Montgomery, Matthew; Snyder, Gary. Transition with a linear flow path for use in a gas turbine engine. USP2012028113003.
  15. Charron, Richard; Snyder, Gary. Transition with a linear flow path with exhaust mouths for use in a gas turbine engine. USP2011118065881.

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