EP1384950A2 - Chambre de combustion annulaire pour une turbine à gaz - Google Patents

Chambre de combustion annulaire pour une turbine à gaz Download PDF

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Publication number
EP1384950A2
EP1384950A2 EP03405504A EP03405504A EP1384950A2 EP 1384950 A2 EP1384950 A2 EP 1384950A2 EP 03405504 A EP03405504 A EP 03405504A EP 03405504 A EP03405504 A EP 03405504A EP 1384950 A2 EP1384950 A2 EP 1384950A2
Authority
EP
European Patent Office
Prior art keywords
combustion chamber
lining segments
segments
chamber according
divided
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.)
Granted
Application number
EP03405504A
Other languages
German (de)
English (en)
Other versions
EP1384950A3 (fr
EP1384950B1 (fr
Inventor
Peter Graf
Stefan Tschirren
Helmar Wunderle
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.)
General Electric Technology GmbH
Original Assignee
Alstom Technology AG
Alstom Schweiz AG
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 Alstom Technology AG, Alstom Schweiz AG filed Critical Alstom Technology AG
Publication of EP1384950A2 publication Critical patent/EP1384950A2/fr
Publication of EP1384950A3 publication Critical patent/EP1384950A3/fr
Application granted granted Critical
Publication of EP1384950B1 publication Critical patent/EP1384950B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50Combustion 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)
  • Turbine Rotor Nozzle Sealing (AREA)
EP03405504A 2002-07-25 2003-07-07 Chambre de combustion annulaire pour une turbine à gaz Expired - Lifetime EP1384950B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10233805A DE10233805B4 (de) 2002-07-25 2002-07-25 Ringförmige Brennkammer für eine Gasturbine
DE10233805 2002-07-25

Publications (3)

Publication Number Publication Date
EP1384950A2 true EP1384950A2 (fr) 2004-01-28
EP1384950A3 EP1384950A3 (fr) 2007-04-04
EP1384950B1 EP1384950B1 (fr) 2012-10-17

Family

ID=29796562

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03405504A Expired - Lifetime EP1384950B1 (fr) 2002-07-25 2003-07-07 Chambre de combustion annulaire pour une turbine à gaz

Country Status (3)

Country Link
US (1) US7350360B2 (fr)
EP (1) EP1384950B1 (fr)
DE (1) DE10233805B4 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2282124A1 (fr) * 2009-08-03 2011-02-09 Alstom Technology Ltd Procédé de modification d'une chambre à combustion d'une turbine à gaz
US9255484B2 (en) * 2011-03-16 2016-02-09 General Electric Company Aft frame and method for cooling aft frame
US9612017B2 (en) 2014-06-05 2017-04-04 Rolls-Royce North American Technologies, Inc. Combustor with tiled liner
US10465907B2 (en) 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
US10598380B2 (en) 2017-09-21 2020-03-24 General Electric Company Canted combustor for gas turbine engine
US11047575B2 (en) 2019-04-15 2021-06-29 Raytheon Technologies Corporation Combustor heat shield panel

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4446693A (en) 1980-11-08 1984-05-08 Rolls-Royce Limited Wall structure for a combustion chamber
EP0321809A1 (fr) 1987-12-21 1989-06-28 BBC Brown Boveri AG Procédé pour la combustion de combustible liquide dans un brûleur
US5363643A (en) 1993-02-08 1994-11-15 General Electric Company Segmented combustor
EP1363075A2 (fr) 2002-05-16 2003-11-19 United Technologies Corporation Panneaux de protection thermique pour une chambre de combustion de turbine à gaz

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH257279A (de) 1946-01-14 1948-09-30 Hunziker Reinhold Fangvorrichtung für Kleintiere wie Mäuse.
CH428324A (de) * 1964-05-21 1967-01-15 Prvni Brnenska Strojirna Brennkammer
US4567730A (en) * 1983-10-03 1986-02-04 General Electric Company Shielded combustor
US4628694A (en) * 1983-12-19 1986-12-16 General Electric Company Fabricated liner article and method
US5435127A (en) * 1993-11-15 1995-07-25 General Electric Company Method and apparatus for boosting ram airflow to an ejection nozzle
GB2298267B (en) * 1995-02-23 1999-01-13 Rolls Royce Plc An arrangement of heat resistant tiles for a gas turbine engine combustor
US6301877B1 (en) * 1995-11-13 2001-10-16 United Technologies Corporation Ejector extension cooling for exhaust nozzle
WO1998013645A1 (fr) * 1996-09-26 1998-04-02 Siemens Aktiengesellschaft Element a effet de bouclier thermique a recyclage du fluide de refroidissement et systeme de bouclier thermique pour element de guidage de gaz chauds
DE19727407A1 (de) * 1997-06-27 1999-01-07 Siemens Ag Hitzeschild
US6606861B2 (en) * 2001-02-26 2003-08-19 United Technologies Corporation Low emissions combustor for a gas turbine engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4446693A (en) 1980-11-08 1984-05-08 Rolls-Royce Limited Wall structure for a combustion chamber
EP0321809A1 (fr) 1987-12-21 1989-06-28 BBC Brown Boveri AG Procédé pour la combustion de combustible liquide dans un brûleur
US5363643A (en) 1993-02-08 1994-11-15 General Electric Company Segmented combustor
EP1363075A2 (fr) 2002-05-16 2003-11-19 United Technologies Corporation Panneaux de protection thermique pour une chambre de combustion de turbine à gaz

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
D. K. MUKHERJEE: "State-of-the-art gas turbines - a brief update", ABB REVIEW, vol. 2, 1997, pages 4 - 14

Also Published As

Publication number Publication date
DE10233805A1 (de) 2004-02-05
US20040154308A1 (en) 2004-08-12
US7350360B2 (en) 2008-04-01
DE10233805B4 (de) 2013-08-22
EP1384950A3 (fr) 2007-04-04
EP1384950B1 (fr) 2012-10-17

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