ATE374908T1 - Brennkammer für gasturbine - Google Patents

Brennkammer für gasturbine

Info

Publication number
ATE374908T1
ATE374908T1 AT05736060T AT05736060T ATE374908T1 AT E374908 T1 ATE374908 T1 AT E374908T1 AT 05736060 T AT05736060 T AT 05736060T AT 05736060 T AT05736060 T AT 05736060T AT E374908 T1 ATE374908 T1 AT E374908T1
Authority
AT
Austria
Prior art keywords
combustion chamber
gas turbine
protective elements
thermal protective
cooling air
Prior art date
Application number
AT05736060T
Other languages
English (en)
Inventor
Ian William Boston
Stefan Gross
Jonas Hurter
Thomas Kueenzi
Original Assignee
Alstom Technology Ltd
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 Ltd filed Critical Alstom Technology Ltd
Application granted granted Critical
Publication of ATE374908T1 publication Critical patent/ATE374908T1/de

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
    • 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

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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
AT05736060T 2004-05-05 2005-04-22 Brennkammer für gasturbine ATE374908T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH7982004 2004-05-05

Publications (1)

Publication Number Publication Date
ATE374908T1 true ATE374908T1 (de) 2007-10-15

Family

ID=34965312

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05736060T ATE374908T1 (de) 2004-05-05 2005-04-22 Brennkammer für gasturbine

Country Status (7)

Country Link
US (1) US7752846B2 (de)
EP (1) EP1745245B1 (de)
CN (1) CN100510539C (de)
AT (1) ATE374908T1 (de)
DE (1) DE502005001634D1 (de)
ES (1) ES2296165T3 (de)
WO (1) WO2005108869A1 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2128524A1 (de) * 2008-05-26 2009-12-02 Siemens Aktiengesellschaft Bauteilanordnung, Brennkammeranordnung und Gasturbine
US9416970B2 (en) * 2009-11-30 2016-08-16 United Technologies Corporation Combustor heat panel arrangement having holes offset from seams of a radially opposing heat panel
GB201119526D0 (en) * 2011-11-14 2011-12-21 Rolls Royce Plc Leaf seal
FR2998039B1 (fr) * 2012-11-09 2014-11-14 Snecma Chambre de combustion pour une turbomachine
US20140144158A1 (en) * 2012-11-29 2014-05-29 General Electric Company Turbomachine component including a seal member
US9771818B2 (en) 2012-12-29 2017-09-26 United Technologies Corporation Seals for a circumferential stop ring in a turbine exhaust case
DE102014204466A1 (de) * 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine
US20180051880A1 (en) * 2016-08-18 2018-02-22 General Electric Company Combustor assembly for a turbine engine
US20180180289A1 (en) * 2016-12-23 2018-06-28 General Electric Company Turbine engine assembly including a rotating detonation combustor
FR3061761B1 (fr) * 2017-01-10 2021-01-01 Safran Aircraft Engines Chambre de combustion pour turbomachine
US11421877B2 (en) * 2017-08-29 2022-08-23 General Electric Company Vibration control for a gas turbine engine
JP7289752B2 (ja) * 2019-08-01 2023-06-12 三菱重工業株式会社 音響減衰器、筒アッセンブリ、燃焼器、ガスタービン及び筒アッセンブリの製造方法
DE102020203017A1 (de) * 2020-03-10 2021-09-16 Siemens Aktiengesellschaft Brennkammer mit keramischem Hitzeschild und Dichtung
CN112460630A (zh) * 2020-10-27 2021-03-09 中国船舶重工集团公司第七0三研究所 一种燃气轮机高温区间隙平面间密封组件
CN117090688B (zh) * 2023-08-29 2025-09-09 清航空天(北京)科技有限公司 一种浮动式爆震涡轮发动机

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5400586A (en) * 1992-07-28 1995-03-28 General Electric Co. Self-accommodating brush seal for gas turbine combustor
US5323604A (en) * 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
JP2904701B2 (ja) * 1993-12-15 1999-06-14 株式会社日立製作所 ガスタービン及びガスタービンの燃焼装置
WO1998016764A1 (en) * 1996-10-16 1998-04-23 Siemens Westinghouse Power Corporation Brush seal for gas turbine combustor-transition interface
US6186508B1 (en) * 1996-11-27 2001-02-13 United Technologies Corporation Wear resistant coating for brush seal applications
DE19712088C2 (de) * 1997-03-22 1999-06-24 Mtu Muenchen Gmbh Bürstendichtung mit in Umfangsrichtung schräg gestellten Borsten
DE19720649C2 (de) * 1997-05-16 2000-09-28 Mtu Muenchen Gmbh Bürstendichtung
GB2328011A (en) * 1997-08-05 1999-02-10 Europ Gas Turbines Ltd Combustor for gas or liquid fuelled turbine
US5961280A (en) * 1997-09-12 1999-10-05 General Elecgtric Company Anti-hysteresis brush seal
DE69922567T2 (de) * 1998-04-01 2005-12-08 Mitsubishi Heavy Industries, Ltd. Dichtungsanordnung für eine Gasturbine
EP0990851B1 (de) 1998-09-30 2003-07-23 ALSTOM (Switzerland) Ltd Brennkammer für eine Gasturbine
US6357752B1 (en) * 1999-10-15 2002-03-19 General Electric Company Brush seal
GB2361304A (en) * 2000-04-14 2001-10-17 Rolls Royce Plc Combustor wall tile
CN1246638C (zh) * 2001-04-27 2006-03-22 西门子公司 燃烧室、尤其是燃气轮机的燃烧室
EP1319896A3 (de) * 2001-12-14 2004-05-12 R. Jan Mowill Kraftstoff/Luft-Vormischeinrichtung mit veränderlicher Geometrie und Methode, die Ausströmgeschwindigkeit zu regeln

Also Published As

Publication number Publication date
DE502005001634D1 (de) 2007-11-15
WO2005108869A1 (de) 2005-11-17
EP1745245A1 (de) 2007-01-24
CN100510539C (zh) 2009-07-08
ES2296165T3 (es) 2008-04-16
US20080230997A1 (en) 2008-09-25
US7752846B2 (en) 2010-07-13
EP1745245B1 (de) 2007-10-03
CN1981159A (zh) 2007-06-13

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Legal Events

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REN Ceased due to non-payment of the annual fee