DE59603160D1 - Hitzeschild-anordnung für eine gasturbinen-brennkammer - Google Patents
Hitzeschild-anordnung für eine gasturbinen-brennkammerInfo
- Publication number
- DE59603160D1 DE59603160D1 DE59603160T DE59603160T DE59603160D1 DE 59603160 D1 DE59603160 D1 DE 59603160D1 DE 59603160 T DE59603160 T DE 59603160T DE 59603160 T DE59603160 T DE 59603160T DE 59603160 D1 DE59603160 D1 DE 59603160D1
- Authority
- DE
- Germany
- Prior art keywords
- combustion chamber
- gas turbine
- heat shield
- turbine combustion
- shield arrangement
- 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.)
- Expired - Fee Related
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
- Spray-Type Burners (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19508111A DE19508111A1 (de) | 1995-03-08 | 1995-03-08 | Hitzeschild-Anordnung für eine Gasturbinen-Brennkammer |
PCT/EP1996/000860 WO1996027765A1 (de) | 1995-03-08 | 1996-03-01 | Hitzeschild-anordnung für eine gasturbinen-brennkammer |
Publications (1)
Publication Number | Publication Date |
---|---|
DE59603160D1 true DE59603160D1 (de) | 1999-10-28 |
Family
ID=7755962
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19508111A Withdrawn DE19508111A1 (de) | 1995-03-08 | 1995-03-08 | Hitzeschild-Anordnung für eine Gasturbinen-Brennkammer |
DE59603160T Expired - Fee Related DE59603160D1 (de) | 1995-03-08 | 1996-03-01 | Hitzeschild-anordnung für eine gasturbinen-brennkammer |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19508111A Withdrawn DE19508111A1 (de) | 1995-03-08 | 1995-03-08 | Hitzeschild-Anordnung für eine Gasturbinen-Brennkammer |
Country Status (5)
Country | Link |
---|---|
US (1) | US5894732A (de) |
EP (1) | EP0813669B1 (de) |
CA (1) | CA2214691A1 (de) |
DE (2) | DE19508111A1 (de) |
WO (1) | WO1996027765A1 (de) |
Families Citing this family (61)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19643028A1 (de) * | 1996-10-18 | 1998-04-23 | Bmw Rolls Royce Gmbh | Brennkammer einer Gasturbine mit einem ringförmigen Kopfabschnitt |
GB9623195D0 (en) * | 1996-11-07 | 1997-01-08 | Rolls Royce Plc | Gas turbine engine combustor |
US6546732B1 (en) * | 2001-04-27 | 2003-04-15 | General Electric Company | Methods and apparatus for cooling gas turbine engine combustors |
US6530227B1 (en) * | 2001-04-27 | 2003-03-11 | General Electric Co. | Methods and apparatus for cooling gas turbine engine combustors |
US6497105B1 (en) | 2001-06-04 | 2002-12-24 | Pratt & Whitney Canada Corp. | Low cost combustor burner collar |
US6546733B2 (en) * | 2001-06-28 | 2003-04-15 | General Electric Company | Methods and systems for cooling gas turbine engine combustors |
DE10214573A1 (de) * | 2002-04-02 | 2003-10-16 | Rolls Royce Deutschland | Brennkammer einer Gasturbine mit Starterfilmkühlung |
US6751961B2 (en) * | 2002-05-14 | 2004-06-22 | United Technologies Corporation | Bulkhead panel for use in a combustion chamber of a gas turbine engine |
US6792757B2 (en) | 2002-11-05 | 2004-09-21 | Honeywell International Inc. | Gas turbine combustor heat shield impingement cooling baffle |
US6871501B2 (en) * | 2002-12-03 | 2005-03-29 | General Electric Company | Method and apparatus to decrease gas turbine engine combustor emissions |
US6904676B2 (en) | 2002-12-04 | 2005-06-14 | General Electric Company | Methods for replacing a portion of a combustor liner |
US8021784B2 (en) * | 2004-03-23 | 2011-09-20 | Hammond Group, Inc. | Cureless battery paste and method for producing battery plates |
US7140185B2 (en) * | 2004-07-12 | 2006-11-28 | United Technologies Corporation | Heatshielded article |
US7140189B2 (en) * | 2004-08-24 | 2006-11-28 | Pratt & Whitney Canada Corp. | Gas turbine floating collar |
US7134286B2 (en) * | 2004-08-24 | 2006-11-14 | Pratt & Whitney Canada Corp. | Gas turbine floating collar arrangement |
EP1767855A1 (de) * | 2005-09-27 | 2007-03-28 | Siemens Aktiengesellschaft | Brennkammer und Gasturbinenanlage |
FR2893390B1 (fr) * | 2005-11-15 | 2011-04-01 | Snecma | Fond de chambre de combustion avec ventilation |
FR2894327B1 (fr) * | 2005-12-05 | 2008-05-16 | Snecma Sa | Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif |
GB2434199B (en) * | 2006-01-14 | 2011-01-05 | Alstom Technology Ltd | Combustor liner with heat shield |
US7596949B2 (en) * | 2006-02-23 | 2009-10-06 | General Electric Company | Method and apparatus for heat shielding gas turbine engines |
FR2903172B1 (fr) * | 2006-06-29 | 2008-10-17 | Snecma Sa | Agencement pour chambre de combustion de turbomachine ayant un defecteur a collerette |
FR2903171B1 (fr) * | 2006-06-29 | 2008-10-17 | Snecma Sa | Agencement a liaison par crabot pour chambre de combustion de turbomachine |
US7827800B2 (en) * | 2006-10-19 | 2010-11-09 | Pratt & Whitney Canada Corp. | Combustor heat shield |
US7721548B2 (en) * | 2006-11-17 | 2010-05-25 | Pratt & Whitney Canada Corp. | Combustor liner and heat shield assembly |
US7681398B2 (en) * | 2006-11-17 | 2010-03-23 | Pratt & Whitney Canada Corp. | Combustor liner and heat shield assembly |
US7748221B2 (en) * | 2006-11-17 | 2010-07-06 | Pratt & Whitney Canada Corp. | Combustor heat shield with variable cooling |
US7861530B2 (en) * | 2007-03-30 | 2011-01-04 | Pratt & Whitney Canada Corp. | Combustor floating collar with louver |
US7926280B2 (en) * | 2007-05-16 | 2011-04-19 | Pratt & Whitney Canada Corp. | Interface between a combustor and fuel nozzle |
FR2918443B1 (fr) * | 2007-07-04 | 2009-10-30 | Snecma Sa | Chambre de combustion comportant des deflecteurs de protection thermique de fond de chambre et moteur a turbine a gaz en etant equipe |
GB2460403B (en) * | 2008-05-28 | 2010-11-17 | Rolls Royce Plc | Combustor Wall with Improved Cooling |
US20100089020A1 (en) * | 2008-10-14 | 2010-04-15 | General Electric Company | Metering of diluent flow in combustor |
US8567199B2 (en) * | 2008-10-14 | 2013-10-29 | General Electric Company | Method and apparatus of introducing diluent flow into a combustor |
US9121609B2 (en) * | 2008-10-14 | 2015-09-01 | General Electric Company | Method and apparatus for introducing diluent flow into a combustor |
US20100089022A1 (en) * | 2008-10-14 | 2010-04-15 | General Electric Company | Method and apparatus of fuel nozzle diluent introduction |
US8448416B2 (en) * | 2009-03-30 | 2013-05-28 | General Electric Company | Combustor liner |
US8695322B2 (en) * | 2009-03-30 | 2014-04-15 | General Electric Company | Thermally decoupled can-annular transition piece |
US8863527B2 (en) * | 2009-04-30 | 2014-10-21 | Rolls-Royce Corporation | Combustor liner |
JP4838888B2 (ja) * | 2009-05-27 | 2011-12-14 | 川崎重工業株式会社 | ガスタービン燃焼器 |
DE102009033592A1 (de) | 2009-07-17 | 2011-01-20 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit Starterfilm zur Kühlung der Brennkammerwand |
EP2530383B1 (de) * | 2010-01-28 | 2019-09-18 | Kawasaki Jukogyo Kabushiki Kaisha | Gasturbinenbrennkammer |
GB201107095D0 (en) | 2011-04-28 | 2011-06-08 | Rolls Royce Plc | A head part of an annular combustion chamber |
GB201107090D0 (en) * | 2011-04-28 | 2011-06-08 | Rolls Royce Plc | A head part of an annular combustion chamber |
JP5924618B2 (ja) * | 2012-06-07 | 2016-05-25 | 川崎重工業株式会社 | 燃料噴射装置 |
WO2014163669A1 (en) | 2013-03-13 | 2014-10-09 | Rolls-Royce Corporation | Combustor assembly for a gas turbine engine |
DE102013007443A1 (de) * | 2013-04-30 | 2014-10-30 | Rolls-Royce Deutschland Ltd & Co Kg | Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild |
FR3019216B1 (fr) * | 2014-03-31 | 2018-08-10 | Safran Aircraft Engines | Deflecteur de fond de chambre de combustion d'une turbomachine comportant des rainures sur le pourtour d'une ouverture centrale |
US20160116169A1 (en) * | 2014-09-29 | 2016-04-28 | United Technologies Corporation | Mixer retention |
FR3026827B1 (fr) * | 2014-10-01 | 2019-06-07 | Safran Aircraft Engines | Chambre de combustion de turbomachine |
US9933161B1 (en) * | 2015-02-12 | 2018-04-03 | Pratt & Whitney Canada Corp. | Combustor dome heat shield |
US9746184B2 (en) * | 2015-04-13 | 2017-08-29 | Pratt & Whitney Canada Corp. | Combustor dome heat shield |
US10267521B2 (en) | 2015-04-13 | 2019-04-23 | Pratt & Whitney Canada Corp. | Combustor heat shield |
GB2543803B (en) * | 2015-10-29 | 2019-10-30 | Rolls Royce Plc | A combustion chamber assembly |
GB201701380D0 (en) | 2016-12-20 | 2017-03-15 | Rolls Royce Plc | A combustion chamber and a combustion chamber fuel injector seal |
GB201715366D0 (en) | 2017-09-22 | 2017-11-08 | Rolls Royce Plc | A combustion chamber |
US10330204B2 (en) | 2017-11-10 | 2019-06-25 | Rolls-Royce Deutschland Ltd & Co Kg | Burner seal of a gas turbine and method for manufacturing the same |
EP3483503B1 (de) * | 2017-11-10 | 2021-01-06 | Rolls-Royce Deutschland Ltd & Co KG | Brennerdichtung einer gasturbine und verfahren zu deren herstellung |
DE102018106051A1 (de) | 2018-03-15 | 2019-09-19 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammerbaugruppe mit Brennerdichtung und Düse sowie einer Leitströmungserzeugungseinrichtung |
FR3081974B1 (fr) * | 2018-06-04 | 2020-06-19 | Safran Aircraft Engines | Chambre de combustion d'une turbomachine |
FR3082284B1 (fr) * | 2018-06-07 | 2020-12-11 | Safran Aircraft Engines | Chambre de combustion pour une turbomachine |
DE102018125698A1 (de) | 2018-10-17 | 2020-04-23 | Man Energy Solutions Se | Gasturbinenbrennkammer |
US11892165B2 (en) | 2021-05-19 | 2024-02-06 | General Electric Company | Heat shield for fuel nozzle |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4180974A (en) * | 1977-10-31 | 1980-01-01 | General Electric Company | Combustor dome sleeve |
GB1594463A (en) * | 1978-02-07 | 1981-07-30 | Rolls Royce | Combustion equipment |
DE2949726A1 (de) * | 1979-12-11 | 1981-06-19 | Hochtemperatur-Reaktorbau GmbH, 5000 Köln | Von einem gas hohen druckes und hoher temperatur durchstroemter gaskanal grosser abmessungen |
US4322945A (en) * | 1980-04-02 | 1982-04-06 | United Technologies Corporation | Fuel nozzle guide heat shield for a gas turbine engine |
DE3131310A1 (de) * | 1981-08-07 | 1983-02-24 | Deutsche Babcock Bau GmbH, 4200 Oberhausen | Feuerungsraum fuer eine verbrennungsanlage |
EP0153842B1 (de) * | 1984-02-29 | 1988-07-27 | LUCAS INDUSTRIES public limited company | Brennkammer für Gasturbinen |
US4934145A (en) * | 1988-10-12 | 1990-06-19 | United Technologies Corporation | Combustor bulkhead heat shield assembly |
DE9000548U1 (de) * | 1990-01-19 | 1990-03-01 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Wärmeschutz-Vorrichtung |
US5142871A (en) * | 1991-01-22 | 1992-09-01 | General Electric Company | Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures |
GB9112324D0 (en) * | 1991-06-07 | 1991-07-24 | Rolls Royce Plc | Gas turbine engine combustor |
CA2070518C (en) * | 1991-07-01 | 2001-10-02 | Adrian Mark Ablett | Combustor dome assembly |
GB2287310B (en) * | 1994-03-01 | 1997-12-03 | Rolls Royce Plc | Gas turbine engine combustor heatshield |
US5623827A (en) * | 1995-01-26 | 1997-04-29 | General Electric Company | Regenerative cooled dome assembly for a gas turbine engine combustor |
-
1995
- 1995-03-08 DE DE19508111A patent/DE19508111A1/de not_active Withdrawn
-
1996
- 1996-03-01 CA CA002214691A patent/CA2214691A1/en not_active Abandoned
- 1996-03-01 US US08/913,122 patent/US5894732A/en not_active Expired - Fee Related
- 1996-03-01 EP EP96906722A patent/EP0813669B1/de not_active Expired - Lifetime
- 1996-03-01 DE DE59603160T patent/DE59603160D1/de not_active Expired - Fee Related
- 1996-03-01 WO PCT/EP1996/000860 patent/WO1996027765A1/de active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP0813669A1 (de) | 1997-12-29 |
WO1996027765A1 (de) | 1996-09-12 |
US5894732A (en) | 1999-04-20 |
CA2214691A1 (en) | 1996-09-12 |
EP0813669B1 (de) | 1999-09-22 |
DE19508111A1 (de) | 1996-09-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8327 | Change in the person/name/address of the patent owner |
Owner name: ROLLS-ROYCE DEUTSCHLAND GMBH, 61440 OBERURSEL, DE |
|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG, 15827 DAHLEWI |
|
8339 | Ceased/non-payment of the annual fee |