ATE146872T1 - Brennkammer und verfahren dafür - Google Patents
Brennkammer und verfahren dafürInfo
- Publication number
- ATE146872T1 ATE146872T1 AT93914042T AT93914042T ATE146872T1 AT E146872 T1 ATE146872 T1 AT E146872T1 AT 93914042 T AT93914042 T AT 93914042T AT 93914042 T AT93914042 T AT 93914042T AT E146872 T1 ATE146872 T1 AT E146872T1
- Authority
- AT
- Austria
- Prior art keywords
- combustion chamber
- zone
- pilot zone
- pilot
- divergent
- 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
- F23R3/42—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
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/08—Purpose of the control system to produce clean exhaust gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/08—Purpose of the control system to produce clean exhaust gases
- F05D2270/082—Purpose of the control system to produce clean exhaust gases with as little NOx as possible
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Auxiliary Devices For And Details Of Packaging Control (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/898,053 US5406799A (en) | 1992-06-12 | 1992-06-12 | Combustion chamber |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE146872T1 true ATE146872T1 (de) | 1997-01-15 |
Family
ID=25408862
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT93914042T ATE146872T1 (de) | 1992-06-12 | 1993-05-20 | Brennkammer und verfahren dafür |
Country Status (8)
Country | Link |
---|---|
US (2) | US5406799A (de) |
EP (1) | EP0644994B1 (de) |
JP (1) | JPH07507862A (de) |
AT (1) | ATE146872T1 (de) |
DE (2) | DE69306950T2 (de) |
ES (1) | ES2078888T3 (de) |
GR (1) | GR950300068T1 (de) |
WO (1) | WO1993025851A1 (de) |
Families Citing this family (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5402634A (en) * | 1993-10-22 | 1995-04-04 | United Technologies Corporation | Fuel supply system for a staged combustor |
JP3464487B2 (ja) * | 1994-07-13 | 2003-11-10 | ボルボ エアロ コーポレイション | ガスタービンエンジン用低排気ガス燃焼器 |
FR2727193B1 (fr) * | 1994-11-23 | 1996-12-20 | Snecma | Chambre de combustion a deux tetes fonctionnant du ralenti au plein gaz |
US6058710A (en) * | 1995-03-08 | 2000-05-09 | Bmw Rolls-Royce Gmbh | Axially staged annular combustion chamber of a gas turbine |
DE19615910B4 (de) * | 1996-04-22 | 2006-09-14 | Alstom | Brenneranordnung |
JPH11257664A (ja) | 1997-12-30 | 1999-09-21 | United Technol Corp <Utc> | ガスタ―ビンエンジンの燃料噴射ノズル/ガイドアセンブリ |
US6240731B1 (en) | 1997-12-31 | 2001-06-05 | United Technologies Corporation | Low NOx combustor for gas turbine engine |
US6530223B1 (en) * | 1998-10-09 | 2003-03-11 | General Electric Company | Multi-stage radial axial gas turbine engine combustor |
US6412272B1 (en) * | 1998-12-29 | 2002-07-02 | United Technologies Corporation | Fuel nozzle guide for gas turbine engine and method of assembly/disassembly |
DE10020598A1 (de) * | 2000-04-27 | 2002-03-07 | Rolls Royce Deutschland | Gasturbinenbrennkammer mit Zuleitungsöffnungen |
WO2008070210A2 (en) * | 2006-06-15 | 2008-06-12 | Indiana University Research And Technology Corporation | Pilot fuel injection for a wave rotor engine |
US7631500B2 (en) * | 2006-09-29 | 2009-12-15 | General Electric Company | Methods and apparatus to facilitate decreasing combustor acoustics |
JP5147938B2 (ja) * | 2007-07-02 | 2013-02-20 | シーメンス アクチエンゲゼルシヤフト | バーナおよびバーナの運転方法 |
US8176739B2 (en) * | 2008-07-17 | 2012-05-15 | General Electric Company | Coanda injection system for axially staged low emission combustors |
US8220269B2 (en) * | 2008-09-30 | 2012-07-17 | Alstom Technology Ltd. | Combustor for a gas turbine engine with effusion cooled baffle |
US8220271B2 (en) * | 2008-09-30 | 2012-07-17 | Alstom Technology Ltd. | Fuel lance for a gas turbine engine including outer helical grooves |
WO2010096817A2 (en) | 2009-02-23 | 2010-08-26 | Williams International Co., L.L.C. | Combustion system |
JP4797079B2 (ja) * | 2009-03-13 | 2011-10-19 | 川崎重工業株式会社 | ガスタービン燃焼器 |
US20100242483A1 (en) * | 2009-03-30 | 2010-09-30 | United Technologies Corporation | Combustor for gas turbine engine |
RU2534189C2 (ru) * | 2010-02-16 | 2014-11-27 | Дженерал Электрик Компани | Камера сгорания для газовой турбины(варианты) и способ эксплуатации газовой турбины |
EP2434222B1 (de) * | 2010-09-24 | 2019-02-27 | Ansaldo Energia IP UK Limited | Verfahren zum betrieb einer verbrennungskammer |
US9068748B2 (en) * | 2011-01-24 | 2015-06-30 | United Technologies Corporation | Axial stage combustor for gas turbine engines |
US9958162B2 (en) | 2011-01-24 | 2018-05-01 | United Technologies Corporation | Combustor assembly for a turbine engine |
US8479492B2 (en) * | 2011-03-25 | 2013-07-09 | Pratt & Whitney Canada Corp. | Hybrid slinger combustion system |
US9057523B2 (en) * | 2011-07-29 | 2015-06-16 | United Technologies Corporation | Microcircuit cooling for gas turbine engine combustor |
CH707282B1 (de) * | 2011-09-22 | 2015-12-15 | Gen Electric | Brenner und Verfahren zur Brennstoffzufuhr zu einem Brenner. |
US9194586B2 (en) | 2011-12-07 | 2015-11-24 | Pratt & Whitney Canada Corp. | Two-stage combustor for gas turbine engine |
US9243802B2 (en) | 2011-12-07 | 2016-01-26 | Pratt & Whitney Canada Corp. | Two-stage combustor for gas turbine engine |
US9416972B2 (en) | 2011-12-07 | 2016-08-16 | Pratt & Whitney Canada Corp. | Two-stage combustor for gas turbine engine |
JP6028578B2 (ja) * | 2013-01-15 | 2016-11-16 | 株式会社Ihi | 燃焼器 |
EP2971649A4 (de) * | 2013-03-14 | 2016-03-16 | United Technologies Corp | Gasturbinenmotorarchitektur mit verschachtelter konzentrischer brennkammer |
WO2014201135A1 (en) | 2013-06-11 | 2014-12-18 | United Technologies Corporation | Combustor with axial staging for a gas turbine engine |
WO2015031796A1 (en) | 2013-08-29 | 2015-03-05 | United Technologies Corporation | Hybrid diffuser case for a gas turbine engine combustor |
US20150107255A1 (en) * | 2013-10-18 | 2015-04-23 | General Electric Company | Turbomachine combustor having an externally fueled late lean injection (lli) system |
RU2561754C1 (ru) * | 2014-02-12 | 2015-09-10 | Открытое акционерное общество "Газпром" | Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации |
US9803555B2 (en) * | 2014-04-23 | 2017-10-31 | General Electric Company | Fuel delivery system with moveably attached fuel tube |
US9976743B2 (en) * | 2014-07-03 | 2018-05-22 | United Technologies Corporation | Dilution hole assembly |
US10378773B2 (en) | 2014-09-19 | 2019-08-13 | United Technologies Corporation | Turbine engine diffuser assembly with airflow mixer |
FR3037384B1 (fr) * | 2015-06-11 | 2017-06-23 | Turbomeca | Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion |
RU2624682C1 (ru) * | 2016-07-05 | 2017-07-05 | Новиков Илья Николаевич | Кольцевая камера сгорания газотурбинного двигателя и способ осуществления рабочего процесса |
US11073286B2 (en) | 2017-09-20 | 2021-07-27 | General Electric Company | Trapped vortex combustor and method for operating the same |
US10976052B2 (en) * | 2017-10-25 | 2021-04-13 | General Electric Company | Volute trapped vortex combustor assembly |
US10989411B2 (en) * | 2019-01-03 | 2021-04-27 | General Electric Company | Heat exchanger for turbo machine |
GB202019219D0 (en) * | 2020-12-07 | 2021-01-20 | Rolls Royce Plc | Lean burn combustor |
GB202019222D0 (en) | 2020-12-07 | 2021-01-20 | Rolls Royce Plc | Lean burn combustor |
Family Cites Families (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3016705A (en) * | 1960-08-04 | 1962-01-16 | Avco Corp | Self-purging starting fuel nozzles for gas turbine engines |
GB1150344A (en) * | 1965-08-05 | 1969-04-30 | Lucas Industries Ltd | Combustion Apparatus for Gas Turbine Engines |
US3792582A (en) * | 1970-10-26 | 1974-02-19 | United Aircraft Corp | Combustion chamber for dissimilar fluids in swirling flow relationship |
US3701255A (en) * | 1970-10-26 | 1972-10-31 | United Aircraft Corp | Shortened afterburner construction for turbine engine |
US3788065A (en) * | 1970-10-26 | 1974-01-29 | United Aircraft Corp | Annular combustion chamber for dissimilar fluids in swirling flow relationship |
US3811277A (en) * | 1970-10-26 | 1974-05-21 | United Aircraft Corp | Annular combustion chamber for dissimilar fluids in swirling flow relationship |
US3747345A (en) * | 1972-07-24 | 1973-07-24 | United Aircraft Corp | Shortened afterburner construction for turbine engine |
GB1421399A (en) * | 1972-11-13 | 1976-01-14 | Snecma | Fuel injectors |
US3919840A (en) * | 1973-04-18 | 1975-11-18 | United Technologies Corp | Combustion chamber for dissimilar fluids in swirling flow relationship |
FR2235274B1 (de) * | 1973-06-28 | 1976-09-17 | Snecma | |
US3872664A (en) * | 1973-10-15 | 1975-03-25 | United Aircraft Corp | Swirl combustor with vortex burning and mixing |
US3979939A (en) * | 1974-05-21 | 1976-09-14 | G. Schwartz & Co. | Apparatus for the mounting and removal of the rollers of a roll stand |
US3974646A (en) * | 1974-06-11 | 1976-08-17 | United Technologies Corporation | Turbofan engine with augmented combustion chamber using vorbix principle |
US3930370A (en) * | 1974-06-11 | 1976-01-06 | United Technologies Corporation | Turbofan engine with augmented combustion chamber using vorbix principle |
US3973395A (en) * | 1974-12-18 | 1976-08-10 | United Technologies Corporation | Low emission combustion chamber |
US4045956A (en) * | 1974-12-18 | 1977-09-06 | United Technologies Corporation | Low emission combustion chamber |
US4058977A (en) * | 1974-12-18 | 1977-11-22 | United Technologies Corporation | Low emission combustion chamber |
US3937008A (en) * | 1974-12-18 | 1976-02-10 | United Technologies Corporation | Low emission combustion chamber |
US4365577A (en) * | 1977-08-26 | 1982-12-28 | Heinrich Edgar W | Float module combination |
FR2402068A1 (fr) * | 1977-09-02 | 1979-03-30 | Snecma | Chambre de combustion anti-pollution |
US4194359A (en) * | 1977-12-12 | 1980-03-25 | United Technologies Corporation | Means for improving the performance of burner shroud diffusers |
US4194358A (en) * | 1977-12-15 | 1980-03-25 | General Electric Company | Double annular combustor configuration |
US4145878A (en) * | 1977-12-15 | 1979-03-27 | United Technologies Corp. | Vorbix augmenter configuration |
US4145879A (en) * | 1977-12-15 | 1979-03-27 | United Technologies Corp. | Modified vorbix burner concept |
US4145880A (en) * | 1977-12-15 | 1979-03-27 | United Technologies Corp. | Vorbix augmenter configuration with diffuser and vorbix swirler |
US4260367A (en) * | 1978-12-11 | 1981-04-07 | United Technologies Corporation | Fuel nozzle for burner construction |
US4265615A (en) * | 1978-12-11 | 1981-05-05 | United Technologies Corporation | Fuel injection system for low emission burners |
US4389848A (en) * | 1981-01-12 | 1983-06-28 | United Technologies Corporation | Burner construction for gas turbines |
US4474014A (en) * | 1981-09-17 | 1984-10-02 | United Technologies Corporation | Partially unshrouded swirler for combustion chambers |
US4527386A (en) * | 1983-02-28 | 1985-07-09 | United Technologies Corporation | Diffuser for gas turbine engine |
DE3663189D1 (en) * | 1985-03-04 | 1989-06-08 | Siemens Ag | Burner disposition for combustion installations, especially for combustion chambers of gas turbine installations, and method for its operation |
US5036657A (en) * | 1987-06-25 | 1991-08-06 | General Electric Company | Dual manifold fuel system |
US5044559A (en) * | 1988-11-02 | 1991-09-03 | United Technologies Corporation | Gas assisted liquid atomizer |
US4977740A (en) * | 1989-06-07 | 1990-12-18 | United Technologies Corporation | Dual fuel injector |
US5099644A (en) * | 1990-04-04 | 1992-03-31 | General Electric Company | Lean staged combustion assembly |
US5197289A (en) * | 1990-11-26 | 1993-03-30 | General Electric Company | Double dome combustor |
US5197278A (en) * | 1990-12-17 | 1993-03-30 | General Electric Company | Double dome combustor and method of operation |
US5220795A (en) * | 1991-04-16 | 1993-06-22 | General Electric Company | Method and apparatus for injecting dilution air |
CA2089302C (en) * | 1992-03-30 | 2004-07-06 | Joseph Frank Savelli | Double annular combustor |
-
1992
- 1992-06-12 US US07/898,053 patent/US5406799A/en not_active Expired - Lifetime
-
1993
- 1993-05-20 ES ES93914042T patent/ES2078888T3/es not_active Expired - Lifetime
- 1993-05-20 DE DE69306950T patent/DE69306950T2/de not_active Expired - Fee Related
- 1993-05-20 AT AT93914042T patent/ATE146872T1/de not_active IP Right Cessation
- 1993-05-20 DE DE0644994T patent/DE644994T1/de active Pending
- 1993-05-20 WO PCT/US1993/004819 patent/WO1993025851A1/en active IP Right Grant
- 1993-05-20 JP JP6500940A patent/JPH07507862A/ja active Pending
- 1993-05-20 EP EP93914042A patent/EP0644994B1/de not_active Expired - Lifetime
-
1994
- 1994-07-26 US US08/280,630 patent/US5490380A/en not_active Expired - Lifetime
-
1996
- 1996-01-31 GR GR950300068T patent/GR950300068T1/el unknown
Also Published As
Publication number | Publication date |
---|---|
DE644994T1 (de) | 1996-06-27 |
ES2078888T3 (es) | 1997-04-16 |
EP0644994B1 (de) | 1996-12-27 |
US5490380A (en) | 1996-02-13 |
JPH07507862A (ja) | 1995-08-31 |
ES2078888T1 (es) | 1996-01-01 |
EP0644994A1 (de) | 1995-03-29 |
DE69306950T2 (de) | 1997-05-07 |
US5406799A (en) | 1995-04-18 |
GR950300068T1 (en) | 1996-01-31 |
DE69306950D1 (de) | 1997-02-06 |
WO1993025851A1 (en) | 1993-12-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
UEP | Publication of translation of european patent specification | ||
REN | Ceased due to non-payment of the annual fee |