AU2001257482A1 - Annular combustor for use with an energy system - Google Patents
Annular combustor for use with an energy systemInfo
- Publication number
- AU2001257482A1 AU2001257482A1 AU2001257482A AU5748201A AU2001257482A1 AU 2001257482 A1 AU2001257482 A1 AU 2001257482A1 AU 2001257482 A AU2001257482 A AU 2001257482A AU 5748201 A AU5748201 A AU 5748201A AU 2001257482 A1 AU2001257482 A1 AU 2001257482A1
- Authority
- AU
- Australia
- Prior art keywords
- energy system
- annular combustor
- combustor
- annular
- energy
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
- F02C3/085—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage the turbine being of the radial-flow type (radial-radial)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M9/00—Baffles or deflectors for air or combustion products; Flame shields
- F23M9/06—Baffles or deflectors for air or combustion products; Flame shields in fire-boxes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Supply (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US20094600P | 2000-05-01 | 2000-05-01 | |
| US60200946 | 2000-05-01 | ||
| PCT/US2001/014115 WO2001083963A1 (en) | 2000-05-01 | 2001-05-01 | Annular combustor for use with an energy system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AU2001257482A1 true AU2001257482A1 (en) | 2001-11-12 |
Family
ID=22743841
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU2001257482A Abandoned AU2001257482A1 (en) | 2000-05-01 | 2001-05-01 | Annular combustor for use with an energy system |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US6845621B2 (en) |
| EP (1) | EP1295018A4 (en) |
| JP (1) | JP4851674B2 (en) |
| KR (1) | KR20030036174A (en) |
| CN (1) | CN1502007A (en) |
| AU (1) | AU2001257482A1 (en) |
| CA (1) | CA2407717A1 (en) |
| WO (1) | WO2001083963A1 (en) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6644916B1 (en) * | 2002-06-10 | 2003-11-11 | Elliott Energy Systems, Inc | Vane and method of construction thereof |
| US7950233B2 (en) * | 2006-03-31 | 2011-05-31 | Pratt & Whitney Canada Corp. | Combustor |
| US8701416B2 (en) * | 2006-06-26 | 2014-04-22 | Joseph Michael Teets | Radially staged RQL combustor with tangential fuel-air premixers |
| US9038392B2 (en) * | 2006-10-20 | 2015-05-26 | Ihi Corporation | Gas turbine combustor |
| US20090211260A1 (en) * | 2007-05-03 | 2009-08-27 | Brayton Energy, Llc | Multi-Spool Intercooled Recuperated Gas Turbine |
| US8065881B2 (en) * | 2008-08-12 | 2011-11-29 | Siemens Energy, Inc. | Transition with a linear flow path with exhaust mouths for use in a gas turbine engine |
| US8091365B2 (en) * | 2008-08-12 | 2012-01-10 | Siemens Energy, Inc. | Canted outlet for transition in a gas turbine engine |
| US8113003B2 (en) * | 2008-08-12 | 2012-02-14 | Siemens Energy, Inc. | Transition with a linear flow path for use in a gas turbine engine |
| US8616007B2 (en) * | 2009-01-22 | 2013-12-31 | Siemens Energy, Inc. | Structural attachment system for transition duct outlet |
| EP2430292A1 (en) | 2009-05-12 | 2012-03-21 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
| WO2011109514A1 (en) * | 2010-03-02 | 2011-09-09 | Icr Turbine Engine Corporatin | Dispatchable power from a renewable energy facility |
| US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
| CA2813680A1 (en) | 2010-09-03 | 2012-03-08 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
| US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
| US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
| KR101265883B1 (en) * | 2012-11-22 | 2013-05-20 | 에스티엑스중공업 주식회사 | Micro gas turbine including ignitor combination structure and method for assembling the same |
| WO2015199694A1 (en) | 2014-06-26 | 2015-12-30 | Siemens Energy, Inc. | Converging flow joint insert system at an intersection between adjacent transitions duct bodies |
| EP3161266A1 (en) | 2014-06-26 | 2017-05-03 | Siemens Energy, Inc. | Converging flow joint insert system at an intersection between adjacent transition duct bodljs |
| US10557358B2 (en) * | 2015-02-06 | 2020-02-11 | United Technologies Corporation | Gas turbine engine containment structures |
| US20230296250A1 (en) * | 2022-03-21 | 2023-09-21 | General Electric Company | Turbine engine combustor and combustor liner |
| US11788724B1 (en) * | 2022-09-02 | 2023-10-17 | General Electric Company | Acoustic damper for combustor |
Family Cites Families (74)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2856755A (en) * | 1953-10-19 | 1958-10-21 | Szydlowski Joseph | Combustion chamber with diverse combustion and diluent air paths |
| GB1104599A (en) | 1966-12-16 | 1968-02-28 | Rolls Royce | Gas turbine engine combustion chamber |
| US3645095A (en) | 1970-11-25 | 1972-02-29 | Avco Corp | Annualr combustor |
| US3738106A (en) | 1971-10-26 | 1973-06-12 | Avco Corp | Variable geometry combustors |
| US3745766A (en) | 1971-10-26 | 1973-07-17 | Avco Corp | Variable geometry for controlling the flow of air to a combustor |
| GB1424197A (en) * | 1972-06-09 | 1976-02-11 | Lucas Industries Ltd | Combustion chambers for gas turbine engines |
| JPS5129726A (en) | 1974-09-06 | 1976-03-13 | Mitsubishi Heavy Ind Ltd | |
| US4013088A (en) | 1975-05-19 | 1977-03-22 | Braukmann Armaturen Ag | Valve structure |
| US4040251A (en) * | 1975-06-04 | 1977-08-09 | Northern Research And Engineering Corporation | Gas turbine combustion chamber arrangement |
| US4151709A (en) | 1975-09-19 | 1979-05-01 | Avco Corporation | Gas turbine engines with toroidal combustors |
| US4041699A (en) | 1975-12-29 | 1977-08-16 | The Garrett Corporation | High temperature gas turbine |
| US4721454A (en) | 1977-05-25 | 1988-01-26 | Phillips Petroleum Company | Method and apparatus for burning nitrogen-containing fuels |
| US4285193A (en) | 1977-08-16 | 1981-08-25 | Exxon Research & Engineering Co. | Minimizing NOx production in operation of gas turbine combustors |
| US4420929A (en) | 1979-01-12 | 1983-12-20 | General Electric Company | Dual stage-dual mode low emission gas turbine combustion system |
| US4292801A (en) | 1979-07-11 | 1981-10-06 | General Electric Company | Dual stage-dual mode low nox combustor |
| US4698963A (en) | 1981-04-22 | 1987-10-13 | The United States Of America As Represented By The Department Of Energy | Low NOx combustor |
| US4787208A (en) | 1982-03-08 | 1988-11-29 | Westinghouse Electric Corp. | Low-nox, rich-lean combustor |
| US4819438A (en) | 1982-12-23 | 1989-04-11 | United States Of America | Steam cooled rich-burn combustor liner |
| DE3545524C2 (en) | 1985-12-20 | 1996-02-29 | Siemens Ag | Multi-stage combustion chamber for the combustion of nitrogenous gas with reduced NO¶x¶ emission and method for its operation |
| US4702073A (en) | 1986-03-10 | 1987-10-27 | Melconian Jerry O | Variable residence time vortex combustor |
| US4784600A (en) | 1986-10-08 | 1988-11-15 | Prutech Ii | Low NOx staged combustor with swirl suppression |
| US4982570A (en) | 1986-11-25 | 1991-01-08 | General Electric Company | Premixed pilot nozzle for dry low Nox combustor |
| US4825640A (en) | 1987-06-22 | 1989-05-02 | Sundstrand Corporation | Combustor with enhanced turbine nozzle cooling |
| US4794754A (en) | 1987-06-22 | 1989-01-03 | Sundstrand Corporation | Low cost annular combustor |
| US4912931A (en) | 1987-10-16 | 1990-04-03 | Prutech Ii | Staged low NOx gas turbine combustor |
| US4891936A (en) | 1987-12-28 | 1990-01-09 | Sundstrand Corporation | Turbine combustor with tangential fuel injection and bender jets |
| US4928479A (en) | 1987-12-28 | 1990-05-29 | Sundstrand Corporation | Annular combustor with tangential cooling air injection |
| US5297385A (en) | 1988-05-31 | 1994-03-29 | United Technologies Corporation | Combustor |
| US4910957A (en) | 1988-07-13 | 1990-03-27 | Prutech Ii | Staged lean premix low nox hot wall gas turbine combustor with improved turndown capability |
| US5025622A (en) | 1988-08-26 | 1991-06-25 | Sol-3- Resources, Inc. | Annular vortex combustor |
| US4996838A (en) * | 1988-10-27 | 1991-03-05 | Sol-3 Resources, Inc. | Annular vortex slinger combustor |
| US4967562A (en) | 1988-12-12 | 1990-11-06 | Sundstrand Corporation | Turbine engine with high efficiency fuel atomization |
| US4989404A (en) | 1988-12-12 | 1991-02-05 | Sundstrand Corporation | Turbine engine with high efficiency fuel atomization |
| US4949545A (en) | 1988-12-12 | 1990-08-21 | Sundstrand Corporation | Turbine wheel and nozzle cooling |
| US5058375A (en) | 1988-12-28 | 1991-10-22 | Sundstrand Corporation | Gas turbine annular combustor with radial dilution air injection |
| US5027603A (en) | 1988-12-28 | 1991-07-02 | Sundstrand Corporation | Turbine engine with start injector |
| US5101620A (en) | 1988-12-28 | 1992-04-07 | Sundstrand Corporation | Annular combustor for a turbine engine without film cooling |
| US5062262A (en) | 1988-12-28 | 1991-11-05 | Sundstrand Corporation | Cooling of turbine nozzles |
| US5033263A (en) | 1989-03-17 | 1991-07-23 | Sundstrand Corporation | Compact gas turbine engine |
| US5577380A (en) | 1989-03-17 | 1996-11-26 | Sundstrand Corporation | Compact gas turbine engine |
| US5140808A (en) | 1989-03-17 | 1992-08-25 | Sundstrand Corporation | Gas turbine engine with fuel mainfold system |
| US5331803A (en) | 1989-07-24 | 1994-07-26 | Sundstrand Corporation | Method of obtaining a desired temperature profile in a turbine engine and turbine engine incorporating the same |
| US5749219A (en) | 1989-11-30 | 1998-05-12 | United Technologies Corporation | Combustor with first and second zones |
| US5085039A (en) | 1989-12-07 | 1992-02-04 | Sundstrand Corporation | Coanda phenomena combustor for a turbine engine |
| US5129224A (en) | 1989-12-08 | 1992-07-14 | Sundstrand Corporation | Cooling of turbine nozzle containment ring |
| US5263316A (en) | 1989-12-21 | 1993-11-23 | Sundstrand Corporation | Turbine engine with airblast injection |
| US5261224A (en) | 1989-12-21 | 1993-11-16 | Sundstrand Corporation | High altitude starting two-stage fuel injection apparatus |
| US5150570A (en) | 1989-12-21 | 1992-09-29 | Sundstrand Corporation | Unitized fuel manifold and injector for a turbine engine |
| US5363644A (en) | 1989-12-21 | 1994-11-15 | Sundstrand Corporation | Annular combustor |
| US5113647A (en) | 1989-12-22 | 1992-05-19 | Sundstrand Corporation | Gas turbine annular combustor |
| US5285628A (en) | 1990-01-18 | 1994-02-15 | Donlee Technologies, Inc. | Method of combustion and combustion apparatus to minimize Nox and CO emissions from a gas turbine |
| US5303543A (en) | 1990-02-08 | 1994-04-19 | Sundstrand Corporation | Annular combustor for a turbine engine with tangential passages sized to provide only combustion air |
| US5127221A (en) | 1990-05-03 | 1992-07-07 | General Electric Company | Transpiration cooled throat section for low nox combustor and related process |
| US5277022A (en) | 1990-06-22 | 1994-01-11 | Sundstrand Corporation | Air blast fuel injecton system |
| GB9023004D0 (en) | 1990-10-23 | 1990-12-05 | Rolls Royce Plc | A gas turbine engine combustion chamber and a method of operating a gas turbine engine combustion chamber |
| US5207055A (en) | 1990-11-19 | 1993-05-04 | Sundstrand Corporation | Volume enhanced turbine engine combustion zone |
| US5172546A (en) | 1990-11-19 | 1992-12-22 | Sundstrand Corporation | Volume enhanced turbine engine combustion zone |
| US5177956A (en) | 1991-02-06 | 1993-01-12 | Sundstrand Corporation | Ultra high altitude starting compact combustor |
| US5163284A (en) | 1991-02-07 | 1992-11-17 | Sundstrand Corporation | Dual zone combustor fuel injection |
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| US5277021A (en) | 1991-05-13 | 1994-01-11 | Sundstrand Corporation | Very high altitude turbine combustor |
| US5207053A (en) | 1991-05-15 | 1993-05-04 | United Technologies Corporation | Method and system for staged rich/lean combustion |
| US5235804A (en) | 1991-05-15 | 1993-08-17 | United Technologies Corporation | Method and system for combusting hydrocarbon fuels with low pollutant emissions by controllably extracting heat from the catalytic oxidation stage |
| FR2683891B1 (en) | 1991-11-20 | 1995-03-24 | Snecma | TURBOMACHINE COMPRISING A DEVICE FOR REDUCING THE EMISSION OF NITROGEN OXIDES. |
| US5317864A (en) * | 1992-09-30 | 1994-06-07 | Sundstrand Corporation | Tangentially directed air assisted fuel injection and small annular combustors for turbines |
| US5323604A (en) | 1992-11-16 | 1994-06-28 | General Electric Company | Triple annular combustor for gas turbine engine |
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| AU5662296A (en) | 1995-03-24 | 1996-10-16 | Ultimate Power Engineering Group, Inc. | High vanadium content fuel combustor and system |
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| US5950417A (en) | 1996-07-19 | 1999-09-14 | Foster Wheeler Energy International Inc. | Topping combustor for low oxygen vitiated air streams |
| US5850732A (en) | 1997-05-13 | 1998-12-22 | Capstone Turbine Corporation | Low emissions combustion system for a gas turbine engine |
| US5996351A (en) | 1997-07-07 | 1999-12-07 | General Electric Company | Rapid-quench axially staged combustor |
| US6453658B1 (en) * | 2000-02-24 | 2002-09-24 | Capstone Turbine Corporation | Multi-stage multi-plane combustion system for a gas turbine engine |
-
2001
- 2001-05-01 AU AU2001257482A patent/AU2001257482A1/en not_active Abandoned
- 2001-05-01 CA CA002407717A patent/CA2407717A1/en not_active Abandoned
- 2001-05-01 US US10/275,049 patent/US6845621B2/en not_active Expired - Fee Related
- 2001-05-01 JP JP2001580556A patent/JP4851674B2/en not_active Expired - Lifetime
- 2001-05-01 EP EP01931001A patent/EP1295018A4/en not_active Withdrawn
- 2001-05-01 WO PCT/US2001/014115 patent/WO2001083963A1/en not_active Application Discontinuation
- 2001-05-01 CN CNA018121799A patent/CN1502007A/en active Pending
- 2001-05-01 KR KR1020027014598A patent/KR20030036174A/en not_active Application Discontinuation
Also Published As
| Publication number | Publication date |
|---|---|
| US6845621B2 (en) | 2005-01-25 |
| US20030205050A1 (en) | 2003-11-06 |
| EP1295018A1 (en) | 2003-03-26 |
| CN1502007A (en) | 2004-06-02 |
| WO2001083963A1 (en) | 2001-11-08 |
| CA2407717A1 (en) | 2001-11-08 |
| JP4851674B2 (en) | 2012-01-11 |
| EP1295018A4 (en) | 2004-06-02 |
| KR20030036174A (en) | 2003-05-09 |
| JP2004507700A (en) | 2004-03-11 |
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