DE59603160D1 - Hitzeschild-anordnung für eine gasturbinen-brennkammer - Google Patents

Hitzeschild-anordnung für eine gasturbinen-brennkammer

Info

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
Application number
DE59603160T
Other languages
English (en)
Inventor
William Kwan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
BMW Rolls Royce GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by BMW Rolls Royce GmbH filed Critical BMW Rolls Royce GmbH
Application granted granted Critical
Publication of DE59603160D1 publication Critical patent/DE59603160D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air 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)
DE59603160T 1995-03-08 1996-03-01 Hitzeschild-anordnung für eine gasturbinen-brennkammer Expired - Fee Related DE59603160D1 (de)

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)

* Cited by examiner, † Cited by third party
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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)

* Cited by examiner, † Cited by third party
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

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