JP5543132B2 - 部品配置構造、燃焼器装置およびガスタービン - Google Patents

部品配置構造、燃焼器装置およびガスタービン Download PDF

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Publication number
JP5543132B2
JP5543132B2 JP2009125611A JP2009125611A JP5543132B2 JP 5543132 B2 JP5543132 B2 JP 5543132B2 JP 2009125611 A JP2009125611 A JP 2009125611A JP 2009125611 A JP2009125611 A JP 2009125611A JP 5543132 B2 JP5543132 B2 JP 5543132B2
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JP
Japan
Prior art keywords
groove
flame tube
side wall
wall surface
component 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
JP2009125611A
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English (en)
Japanese (ja)
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JP2009287559A (ja
JP2009287559A6 (ja
JP2009287559A5 (enExample
Inventor
ツェルナイ クリストフ
チルレン シュテファン
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.)
Siemens AG
Original Assignee
Siemens AG
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Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Publication of JP2009287559A publication Critical patent/JP2009287559A/ja
Publication of JP2009287559A6 publication Critical patent/JP2009287559A6/ja
Publication of JP2009287559A5 publication Critical patent/JP2009287559A5/ja
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Expired - Fee Related legal-status Critical Current
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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
    • F23R3/60—Support structures; Attaching or mounting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05002—Means for accommodate thermal expansion of the wall liner
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05005—Sealing means between wall tiles or panels
    • 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)
  • Sealing Devices (AREA)
JP2009125611A 2008-05-26 2009-05-25 部品配置構造、燃焼器装置およびガスタービン Expired - Fee Related JP5543132B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP08009563A EP2128524A1 (de) 2008-05-26 2008-05-26 Bauteilanordnung, Brennkammeranordnung und Gasturbine
EP08009563.1 2008-05-26

Publications (4)

Publication Number Publication Date
JP2009287559A JP2009287559A (ja) 2009-12-10
JP2009287559A6 JP2009287559A6 (ja) 2010-02-18
JP2009287559A5 JP2009287559A5 (enExample) 2012-06-07
JP5543132B2 true JP5543132B2 (ja) 2014-07-09

Family

ID=40351740

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2009125611A Expired - Fee Related JP5543132B2 (ja) 2008-05-26 2009-05-25 部品配置構造、燃焼器装置およびガスタービン

Country Status (3)

Country Link
US (1) US20090288422A1 (enExample)
EP (1) EP2128524A1 (enExample)
JP (1) JP5543132B2 (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008061870B4 (de) * 2008-12-15 2015-10-22 Carl Freudenberg Kg Dichtring, Dichtungsanordnung mit einem Dichtring und Verwendung einer Dichtungsanordnung und eines Dichtrings
US8490981B2 (en) * 2010-02-23 2013-07-23 General Electric Company Brush seal
US8955331B2 (en) * 2011-05-20 2015-02-17 Siemens Energy, Inc. Turbine combustion system coupling with adjustable wear pad
US8650852B2 (en) * 2011-07-05 2014-02-18 General Electric Company Support assembly for transition duct in turbine system
DE102011108273A1 (de) * 2011-07-21 2013-01-24 Howaldtswerke-Deutsche Werft Gmbh Dichtungsanordung
US9297536B2 (en) * 2012-05-01 2016-03-29 United Technologies Corporation Gas turbine engine combustor surge retention
US8707673B1 (en) * 2013-01-04 2014-04-29 General Electric Company Articulated transition duct in turbomachine
WO2014143325A1 (en) * 2013-03-15 2014-09-18 Copeland Andrew D Seal assembly for a gas turbine engine and method of forming a turbine engine component
WO2014179328A1 (en) * 2013-04-29 2014-11-06 United Technologies Corporation Joint for sealing a gap between casing segments of an industrial gas turbine engine combustor
JP6170341B2 (ja) 2013-05-21 2017-07-26 三菱日立パワーシステムズ株式会社 再生型ガスタービン燃焼器
US9759427B2 (en) * 2013-11-01 2017-09-12 General Electric Company Interface assembly for a combustor
CN104196637A (zh) * 2014-08-15 2014-12-10 江苏透平密封高科技有限公司 一种新型燃气轮机尾筒气封及其制造方法
US10533750B2 (en) 2014-09-05 2020-01-14 Siemens Aktiengesellschaft Cross ignition flame duct
US20170241277A1 (en) * 2016-02-23 2017-08-24 Siemens Energy, Inc. Movable interface for gas turbine engine
EP3306199B1 (en) * 2016-10-06 2020-12-30 Ansaldo Energia Switzerland AG Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device
KR101850922B1 (ko) * 2016-10-07 2018-04-20 두산중공업 주식회사 가스터빈용 연소 덕트 조립체
US20180306120A1 (en) 2017-04-21 2018-10-25 General Electric Company Pressure regulated piston seal for a gas turbine combustor liner
GB201814674D0 (en) * 2018-09-10 2018-10-24 Rolls Royce Plc Radially dispaceable brush seal
GB201814673D0 (en) * 2018-09-10 2018-10-24 Rolls Royce Plc Radially displaceable brush seal
US12420941B2 (en) * 2022-12-01 2025-09-23 Pratt & Whitney Canada Corp. Aircraft engine with exhaust having removable deflector
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 (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5265412A (en) * 1992-07-28 1993-11-30 General Electric Company Self-accommodating brush seal for gas turbine combustor
JPH0658171A (ja) * 1992-08-07 1994-03-01 Toyota Motor Corp シールリング
JPH08338538A (ja) * 1995-06-09 1996-12-24 Honda Motor Co Ltd 油圧シール装置
WO1998016764A1 (en) * 1996-10-16 1998-04-23 Siemens Westinghouse Power Corporation Brush seal for gas turbine combustor-transition interface
JP4686809B2 (ja) * 2000-04-13 2011-05-25 Ｎｏｋ株式会社 シールリング
JP2001330154A (ja) * 2000-05-24 2001-11-30 Nichias Corp 膨張黒鉛製リングパッキンおよびその製造方法
JP2001349544A (ja) * 2000-06-06 2001-12-21 Hitachi Ltd ガスタービン設備及びその燃焼器におけるトランジションピースの額縁構造
JP2002081552A (ja) * 2000-09-04 2002-03-22 Toshiba Corp ブラシシール装置
JP2003004145A (ja) * 2001-06-20 2003-01-08 Mitsubishi Heavy Ind Ltd 回転軸用シール
DE10163804B4 (de) * 2001-12-22 2005-07-07 Mtu Aero Engines Gmbh Bürstendichtung
US20040256807A1 (en) * 2003-06-23 2004-12-23 Nitin Bhate Retrofittable non-metallic brush seal assembly
DE502005001634D1 (de) * 2004-05-05 2007-11-15 Alstom Technology Ltd Brennkammer für gasturbine
JP4736394B2 (ja) * 2004-10-15 2011-07-27 Ｎｏｋ株式会社 シールリング
GB0423923D0 (en) * 2004-10-28 2004-12-01 Rolls Royce Plc Segmented annular seal for a gas turbine engine
US7413194B2 (en) * 2004-10-28 2008-08-19 Rolls-Royce Plc Pressure balanced annular seal
US7527469B2 (en) * 2004-12-10 2009-05-05 Siemens Energy, Inc. Transition-to-turbine seal apparatus and kit for transition/turbine junction of a gas turbine engine

Also Published As

Publication number Publication date
EP2128524A1 (de) 2009-12-02
JP2009287559A (ja) 2009-12-10
US20090288422A1 (en) 2009-11-26

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