PL2331878T3 - Zespół komory spalania do silnika turbogazowego - Google Patents
Zespół komory spalania do silnika turbogazowegoInfo
- Publication number
- PL2331878T3 PL2331878T3 PL09788722T PL09788722T PL2331878T3 PL 2331878 T3 PL2331878 T3 PL 2331878T3 PL 09788722 T PL09788722 T PL 09788722T PL 09788722 T PL09788722 T PL 09788722T PL 2331878 T3 PL2331878 T3 PL 2331878T3
- Authority
- PL
- Poland
- Prior art keywords
- gas turbine
- turbine engine
- combustor assembly
- combustor
- assembly
- Prior art date
Links
Classifications
-
- 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
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- 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
- F23R3/10—Air inlet arrangements for primary air
-
- 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
- F23R3/26—Controlling the air flow
-
- 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
- F23R3/54—Reverse-flow combustion chambers
-
- 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
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00012—Details of sealing devices
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00017—Assembling combustion chamber liners or subparts
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/210,363 US8490400B2 (en) | 2008-09-15 | 2008-09-15 | Combustor assembly comprising a combustor device, a transition duct and a flow conditioner |
PCT/US2009/001257 WO2010030309A2 (en) | 2008-09-15 | 2009-02-27 | Combustor assembly comprising a combustor device, a transition duct and a flow conditioner |
EP20090788722 EP2331878B1 (en) | 2008-09-15 | 2009-02-27 | Combustor assembly for a gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2331878T3 true PL2331878T3 (pl) | 2015-09-30 |
Family
ID=40674046
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL09788722T PL2331878T3 (pl) | 2008-09-15 | 2009-02-27 | Zespół komory spalania do silnika turbogazowego |
Country Status (5)
Country | Link |
---|---|
US (1) | US8490400B2 (pl) |
EP (1) | EP2331878B1 (pl) |
ES (1) | ES2536367T3 (pl) |
PL (1) | PL2331878T3 (pl) |
WO (1) | WO2010030309A2 (pl) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5535036B2 (ja) * | 2010-11-01 | 2014-07-02 | 川崎重工業株式会社 | ガスタービン燃焼器 |
US8448450B2 (en) * | 2011-07-05 | 2013-05-28 | General Electric Company | Support assembly for transition duct in turbine system |
US8978389B2 (en) * | 2011-12-15 | 2015-03-17 | Siemens Energy, Inc. | Radial inflow gas turbine engine with advanced transition duct |
US9003803B2 (en) * | 2012-08-03 | 2015-04-14 | General Electric Company | Combustor cap assembly |
US20140208756A1 (en) * | 2013-01-30 | 2014-07-31 | Alstom Technology Ltd. | System For Reducing Combustion Noise And Improving Cooling |
US9163837B2 (en) * | 2013-02-27 | 2015-10-20 | Siemens Aktiengesellschaft | Flow conditioner in a combustor of a gas turbine engine |
US9416969B2 (en) | 2013-03-14 | 2016-08-16 | Siemens Aktiengesellschaft | Gas turbine transition inlet ring adapter |
US9303871B2 (en) * | 2013-06-26 | 2016-04-05 | Siemens Aktiengesellschaft | Combustor assembly including a transition inlet cone in a gas turbine engine |
US9759427B2 (en) * | 2013-11-01 | 2017-09-12 | General Electric Company | Interface assembly for a combustor |
EP2927591A1 (de) * | 2014-03-31 | 2015-10-07 | Siemens Aktiengesellschaft | Kühlring und Gasturbinenbrenner mit einem solchen Kühlring |
US9803864B2 (en) * | 2014-06-24 | 2017-10-31 | General Electric Company | Turbine air flow conditioner |
US10215418B2 (en) * | 2014-10-13 | 2019-02-26 | Ansaldo Energia Ip Uk Limited | Sealing device for a gas turbine combustor |
US9829199B2 (en) | 2014-10-30 | 2017-11-28 | Siemens Energy, Inc. | Flange with curved contact surface |
WO2016209222A1 (en) * | 2015-06-24 | 2016-12-29 | Siemens Aktiengesellschaft | Combustor basket cooling ring |
EP3144485A1 (en) * | 2015-09-16 | 2017-03-22 | Siemens Aktiengesellschaft | Turbomachine component with cooling features and a method for manufacturing such a turbomachine component |
US10677466B2 (en) | 2016-10-13 | 2020-06-09 | General Electric Company | Combustor inlet flow conditioner |
WO2018080474A1 (en) * | 2016-10-26 | 2018-05-03 | Siemens Aktiengesellschaft | Liner for a transition duct |
RU2761262C2 (ru) * | 2017-12-26 | 2021-12-06 | Ансальдо Энергия Свитзерленд Аг | Трубчатая камера сгорания для газовой турбины и газовая турбина, содержащая такую трубчатую камеру сгорания |
US11359815B2 (en) | 2020-03-10 | 2022-06-14 | General Electric Company | Sleeve assemblies and methods of fabricating same |
Family Cites Families (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR962862A (pl) * | 1946-10-26 | 1950-06-22 | ||
US3589128A (en) * | 1970-02-02 | 1971-06-29 | Avco Corp | Cooling arrangement for a reverse flow gas turbine combustor |
US3899882A (en) * | 1974-03-27 | 1975-08-19 | Westinghouse Electric Corp | Gas turbine combustor basket cooling |
US4192138A (en) * | 1977-08-29 | 1980-03-11 | Westinghouse Electric Corp. | Gas turbine combustor air inlet |
CH633347A5 (de) * | 1978-08-03 | 1982-11-30 | Bbc Brown Boveri & Cie | Gasturbine. |
JPS55164731A (en) | 1979-06-11 | 1980-12-22 | Hitachi Ltd | Gas-turbine combustor |
JPS5966619A (ja) * | 1982-10-06 | 1984-04-16 | Hitachi Ltd | ガスタ−ビン燃焼器 |
US4719748A (en) * | 1985-05-14 | 1988-01-19 | General Electric Company | Impingement cooled transition duct |
JP3054420B2 (ja) | 1989-05-26 | 2000-06-19 | 株式会社東芝 | ガスタービン燃焼器 |
US5474306A (en) * | 1992-11-19 | 1995-12-12 | General Electric Co. | Woven seal and hybrid cloth-brush seals for turbine applications |
US5309710A (en) * | 1992-11-20 | 1994-05-10 | General Electric Company | Gas turbine combustor having poppet valves for air distribution control |
EP0660046B1 (en) | 1993-12-22 | 1999-12-01 | Siemens Westinghouse Power Corporation | Combustor bybass system for a gas turbine |
US5737915A (en) * | 1996-02-09 | 1998-04-14 | General Electric Co. | Tri-passage diffuser for a gas turbine |
US5724816A (en) * | 1996-04-10 | 1998-03-10 | General Electric Company | Combustor for a gas turbine with cooling structure |
US5758504A (en) * | 1996-08-05 | 1998-06-02 | Solar Turbines Incorporated | Impingement/effusion cooled combustor liner |
GB2328011A (en) * | 1997-08-05 | 1999-02-10 | Europ Gas Turbines Ltd | Combustor for gas or liquid fuelled turbine |
JP4205231B2 (ja) * | 1998-02-10 | 2009-01-07 | ゼネラル・エレクトリック・カンパニイ | バーナ |
US6494044B1 (en) * | 1999-11-19 | 2002-12-17 | General Electric Company | Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method |
JP3478531B2 (ja) * | 2000-04-21 | 2003-12-15 | 川崎重工業株式会社 | ガスタービンのセラミック部品支持構造 |
US6460345B1 (en) * | 2000-11-14 | 2002-10-08 | General Electric Company | Catalytic combustor flow conditioner and method for providing uniform gasvelocity distribution |
US6832481B2 (en) * | 2002-09-26 | 2004-12-21 | Siemens Westinghouse Power Corporation | Turbine engine fuel nozzle |
US7249461B2 (en) * | 2003-08-22 | 2007-07-31 | Siemens Power Generation, Inc. | Turbine fuel ring assembly |
US6923002B2 (en) | 2003-08-28 | 2005-08-02 | General Electric Company | Combustion liner cap assembly for combustion dynamics reduction |
US7284378B2 (en) * | 2004-06-04 | 2007-10-23 | General Electric Company | Methods and apparatus for low emission gas turbine energy generation |
US7197803B2 (en) * | 2003-10-08 | 2007-04-03 | Siemens Power Generation, Inc. | Fixture and method for aligning a transition |
US7574865B2 (en) * | 2004-11-18 | 2009-08-18 | Siemens Energy, Inc. | Combustor flow sleeve with optimized cooling and airflow distribution |
US7377116B2 (en) * | 2005-04-28 | 2008-05-27 | Siemens Power Generation, Inc. | Gas turbine combustor barrier structures for spring clips |
US7685823B2 (en) | 2005-10-28 | 2010-03-30 | Power Systems Mfg., Llc | Airflow distribution to a low emissions combustor |
US7805946B2 (en) * | 2005-12-08 | 2010-10-05 | Siemens Energy, Inc. | Combustor flow sleeve attachment system |
US7762074B2 (en) | 2006-04-04 | 2010-07-27 | Siemens Energy, Inc. | Air flow conditioner for a combustor can of a gas turbine engine |
US7784264B2 (en) * | 2006-08-03 | 2010-08-31 | Siemens Energy, Inc. | Slidable spring-loaded transition-to-turbine seal apparatus and heat-shielding system, comprising the seal, at transition/turbine junction of a gas turbine engine |
-
2008
- 2008-09-15 US US12/210,363 patent/US8490400B2/en not_active Expired - Fee Related
-
2009
- 2009-02-27 WO PCT/US2009/001257 patent/WO2010030309A2/en active Application Filing
- 2009-02-27 ES ES09788722.8T patent/ES2536367T3/es active Active
- 2009-02-27 PL PL09788722T patent/PL2331878T3/pl unknown
- 2009-02-27 EP EP20090788722 patent/EP2331878B1/en not_active Not-in-force
Also Published As
Publication number | Publication date |
---|---|
ES2536367T3 (es) | 2015-05-22 |
EP2331878A2 (en) | 2011-06-15 |
EP2331878B1 (en) | 2015-04-29 |
US20100064693A1 (en) | 2010-03-18 |
WO2010030309A3 (en) | 2012-04-26 |
WO2010030309A2 (en) | 2010-03-18 |
US8490400B2 (en) | 2013-07-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PL2331878T3 (pl) | Zespół komory spalania do silnika turbogazowego | |
GB0809336D0 (en) | A gas turbine engine arrangement | |
GB2438696B (en) | A gas turbine engine | |
GB2450139B (en) | An aerofoil for a gas turbine engine | |
GB0608859D0 (en) | A gas turbine engine | |
GB0920094D0 (en) | Reheat combustor for a gas turbine engine | |
GB2471171B (en) | Mechanical joint for a gas turbine engine | |
GB0822676D0 (en) | A gas turbine engine | |
GB0813820D0 (en) | A fan casing for a gas turbine engine | |
GB0813821D0 (en) | A fan casing for a gas turbine engine | |
EP2153051A4 (en) | MASKING ARRANGEMENT FOR GAS TURBINE ENGINE | |
GB0721577D0 (en) | A combustor for a gas-turbine engine | |
EP2187021A4 (en) | GAS TURBINE COMBUSTION CHAMBER | |
GB2467120B (en) | A gas Turbine engine | |
EP2136143A4 (en) | GAS TURBINE COMBUSTION CHAMBER | |
GB2467121B (en) | A gas turbine engine | |
GB0603285D0 (en) | A gas turbine engine | |
EP2182290A4 (en) | COMBUSTION CHAMBER FOR GAS TURBINE | |
EP2519729A4 (en) | EXHAUST FOR A GAS TURBINE ENGINE | |
EP2187127A4 (en) | GAS TURBINE COMBUSTION CHAMBER | |
GB0719786D0 (en) | A vane and a vane assembly for a gas turbine engine | |
GB0910752D0 (en) | An annulus filler for a gas turbine engine | |
GB0912166D0 (en) | A turbofan gas turbine engine | |
GB2462245B (en) | Gas turbine engine arrangement | |
EP2182195A4 (en) | COMBUSTION CHAMBER FOR GAS TURBINE |