JPS4864310A - - Google Patents

Info

Publication number
JPS4864310A
JPS4864310A JP47121235A JP12123572A JPS4864310A JP S4864310 A JPS4864310 A JP S4864310A JP 47121235 A JP47121235 A JP 47121235A JP 12123572 A JP12123572 A JP 12123572A JP S4864310 A JPS4864310 A JP S4864310A
Authority
JP
Japan
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
JP47121235A
Other languages
Japanese (ja)
Other versions
JPS5112763B2 (enrdf_load_stackoverflow
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 filed Critical
Publication of JPS4864310A publication Critical patent/JPS4864310A/ja
Publication of JPS5112763B2 publication Critical patent/JPS5112763B2/ja
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP47121235A 1971-12-09 1972-12-05 Expired JPS5112763B2 (enrdf_load_stackoverflow)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US20643371A 1971-12-09 1971-12-09

Publications (2)

Publication Number Publication Date
JPS4864310A true JPS4864310A (enrdf_load_stackoverflow) 1973-09-06
JPS5112763B2 JPS5112763B2 (enrdf_load_stackoverflow) 1976-04-22

Family

ID=22766359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP47121235A Expired JPS5112763B2 (enrdf_load_stackoverflow) 1971-12-09 1972-12-05

Country Status (6)

Country Link
US (1) US3759038A (enrdf_load_stackoverflow)
JP (1) JPS5112763B2 (enrdf_load_stackoverflow)
CA (1) CA961654A (enrdf_load_stackoverflow)
CH (1) CH561358A5 (enrdf_load_stackoverflow)
DE (1) DE2258719A1 (enrdf_load_stackoverflow)
GB (1) GB1355728A (enrdf_load_stackoverflow)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5447917A (en) * 1977-09-26 1979-04-16 Hitachi Ltd Flame cross-ignition tube for gas turbine
JP2010276018A (ja) * 2009-05-28 2010-12-09 General Electric Co <Ge> 拡大フラ・シール
JP2011058496A (ja) * 2009-09-11 2011-03-24 General Electric Co <Ge> タービンエンジンのための円周方向自己膨張式支持体
JP2015036548A (ja) * 2013-08-14 2015-02-23 ゼネラル・エレクトリック・カンパニイ ガスターボ機械用の、ディフューザが一体化された内部筒部材

Families Citing this family (76)

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US3824030A (en) * 1973-07-30 1974-07-16 Curtiss Wright Corp Diaphragm and labyrinth seal assembly for gas turbines
US4016718A (en) * 1975-07-21 1977-04-12 United Technologies Corporation Gas turbine engine having an improved transition duct support
US4009569A (en) * 1975-07-21 1977-03-01 United Technologies Corporation Diffuser-burner casing for a gas turbine engine
FR2465080A1 (fr) * 1979-09-17 1981-03-20 Snecma Dispositif de suspension aval de chambre de combustion pour turbomachines
US4422288A (en) * 1981-03-02 1983-12-27 General Electric Company Aft mounting system for combustion transition duct members
US4413470A (en) * 1981-03-05 1983-11-08 Electric Power Research Institute, Inc. Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element
US4790137A (en) * 1987-07-17 1988-12-13 The United States Of America As Represented By The Secretary Of The Air Force Aircraft engine outer duct mounting device
US4921401A (en) * 1989-02-23 1990-05-01 United Technologies Corporation Casting for a rotary machine
GB2247521A (en) * 1990-09-01 1992-03-04 Rolls Royce Plc A combustion chamber assembly
US5400586A (en) * 1992-07-28 1995-03-28 General Electric Co. Self-accommodating brush seal for gas turbine combustor
US5265412A (en) * 1992-07-28 1993-11-30 General Electric Company Self-accommodating brush seal for gas turbine combustor
US6131910A (en) * 1992-11-19 2000-10-17 General Electric Co. Brush seals and combined labyrinth and brush seals for rotary machines
US5474306A (en) * 1992-11-19 1995-12-12 General Electric Co. Woven seal and hybrid cloth-brush seals for turbine applications
US5749584A (en) 1992-11-19 1998-05-12 General Electric Company Combined brush seal and labyrinth seal segment for rotary machines
US5414999A (en) * 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
US5394687A (en) * 1993-12-03 1995-03-07 The United States Of America As Represented By The Department Of Energy Gas turbine vane cooling system
US5749218A (en) * 1993-12-17 1998-05-12 General Electric Co. Wear reduction kit for gas turbine combustors
DE69523545T2 (de) * 1994-12-20 2002-05-29 General Electric Co., Schenectady Verstärkungrahmen für Gasturbinenbrennkammerendstück
JPH09195799A (ja) * 1996-01-17 1997-07-29 Mitsubishi Heavy Ind Ltd 燃焼器のスプリングシール装置
JP3652780B2 (ja) * 1996-04-08 2005-05-25 三菱重工業株式会社 タービン冷却装置
WO1998016764A1 (en) * 1996-10-16 1998-04-23 Siemens Westinghouse Power Corporation Brush seal for gas turbine combustor-transition interface
US5983641A (en) * 1997-04-30 1999-11-16 Mitsubishi Heavy Industries, Ltd. Tail pipe of gas turbine combustor and gas turbine combustor having the same tail pipe
US6006523A (en) * 1997-04-30 1999-12-28 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor with angled tube section
US6027121A (en) * 1997-10-23 2000-02-22 General Electric Co. Combined brush/labyrinth seal for rotary machines
US6045134A (en) * 1998-02-04 2000-04-04 General Electric Co. Combined labyrinth and brush seals for rotary machines
US6139018A (en) * 1998-03-25 2000-10-31 General Electric Co. Positive pressure-actuated brush seal
US6168162B1 (en) 1998-08-05 2001-01-02 General Electric Co. Self-centering brush seal
US6250640B1 (en) 1998-08-17 2001-06-26 General Electric Co. Brush seals for steam turbine applications
US6290232B1 (en) 1999-11-16 2001-09-18 General Electric Co. Rub-tolerant brush seal for turbine rotors and methods of installation
US6331006B1 (en) 2000-01-25 2001-12-18 General Electric Company Brush seal mounting in supporting groove using flat spring with bifurcated end
US6345494B1 (en) * 2000-09-20 2002-02-12 Siemens Westinghouse Power Corporation Side seal for combustor transitions
US7093837B2 (en) 2002-09-26 2006-08-22 Siemens Westinghouse Power Corporation Turbine spring clip seal
US6869082B2 (en) * 2003-06-12 2005-03-22 Siemens Westinghouse Power Corporation Turbine spring clip seal
DE102004010422A1 (de) * 2004-03-01 2005-09-22 Alstom Technology Ltd Dichtungskörper
US7596954B2 (en) * 2004-07-09 2009-10-06 United Technologies Corporation Blade clearance control
US7229249B2 (en) * 2004-08-27 2007-06-12 Pratt & Whitney Canada Corp. Lightweight annular interturbine duct
US7246995B2 (en) * 2004-12-10 2007-07-24 Siemens Power Generation, Inc. Seal usable between a transition and a turbine vane assembly in a turbine engine
US7377116B2 (en) * 2005-04-28 2008-05-27 Siemens Power Generation, Inc. Gas turbine combustor barrier structures for spring clips
US7909569B2 (en) * 2005-06-09 2011-03-22 Pratt & Whitney Canada Corp. Turbine support case and method of manufacturing
US7421842B2 (en) * 2005-07-18 2008-09-09 Siemens Power Generation, Inc. Turbine spring clip seal
US8038389B2 (en) * 2006-01-04 2011-10-18 General Electric Company Method and apparatus for assembling turbine nozzle assembly
WO2007104587A2 (de) * 2006-03-15 2007-09-20 Siemens Aktiengesellschaft Verfahren zur montage eines mischgehäuses in einer gasturbine sowie verstellvorrichtung hierfür
US8499565B2 (en) * 2006-03-17 2013-08-06 Siemens Energy, Inc. Axial diffusor for a turbine engine
US20070214792A1 (en) * 2006-03-17 2007-09-20 Siemens Power Generation, Inc. Axial diffusor for a turbine engine
FR2899271B1 (fr) * 2006-03-29 2008-05-30 Snecma Sa Ensemble d'une aube et d'une chemise de refroidissement, distributeur de turbomachine comportant l'ensemble, turbomachine, procede de montage et de reparation de l'ensemble
US7909570B2 (en) * 2006-08-25 2011-03-22 Pratt & Whitney Canada Corp. Interturbine duct with integrated baffle and seal
US8769963B2 (en) * 2007-01-30 2014-07-08 Siemens Energy, Inc. Low leakage spring clip/ring combinations for gas turbine engine
US7930891B1 (en) * 2007-05-10 2011-04-26 Florida Turbine Technologies, Inc. Transition duct with integral guide vanes
US7909300B2 (en) * 2007-10-18 2011-03-22 General Electric Company Combustor bracket assembly
US8051663B2 (en) 2007-11-09 2011-11-08 United Technologies Corp. Gas turbine engine systems involving cooling of combustion section liners
US8322146B2 (en) * 2007-12-10 2012-12-04 Alstom Technology Ltd Transition duct assembly
US8418474B2 (en) * 2008-01-29 2013-04-16 Alstom Technology Ltd. Altering a natural frequency of a gas turbine transition duct
EP2247830B1 (en) * 2008-02-27 2019-04-10 General Electric Company Flexible seal for a turbine and corresponding turbine
FR2927951B1 (fr) * 2008-02-27 2011-08-19 Snecma Ensemble diffuseur-redresseur pour une turbomachine
FR2931872B1 (fr) * 2008-05-28 2010-08-20 Snecma Turbine haute pression d'une turbomachine avec montage ameliore du boitier de pilotage des jeux radiaux d'aubes mobiles.
US8091365B2 (en) * 2008-08-12 2012-01-10 Siemens Energy, Inc. Canted outlet for transition in a gas turbine engine
US8065881B2 (en) * 2008-08-12 2011-11-29 Siemens Energy, Inc. Transition with a linear flow path with exhaust mouths for use in a gas turbine engine
US20120036857A1 (en) * 2010-08-10 2012-02-16 General Electric Company Combustion liner stop blocks having insertable wear features and related methods
US20120180500A1 (en) * 2011-01-13 2012-07-19 General Electric Company System for damping vibration in a gas turbine engine
US8448444B2 (en) * 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
US8978388B2 (en) * 2011-06-03 2015-03-17 General Electric Company Load member for transition duct in turbine system
US8888445B2 (en) 2011-08-19 2014-11-18 General Electric Company Turbomachine seal assembly
US9897317B2 (en) * 2012-10-01 2018-02-20 Ansaldo Energia Ip Uk Limited Thermally free liner retention mechanism
US10378456B2 (en) 2012-10-01 2019-08-13 Ansaldo Energia Switzerland AG Method of operating a multi-stage flamesheet combustor
US9347669B2 (en) 2012-10-01 2016-05-24 Alstom Technology Ltd. Variable length combustor dome extension for improved operability
US10060630B2 (en) 2012-10-01 2018-08-28 Ansaldo Energia Ip Uk Limited Flamesheet combustor contoured liner
US9416969B2 (en) 2013-03-14 2016-08-16 Siemens Aktiengesellschaft Gas turbine transition inlet ring adapter
DE102013007443A1 (de) * 2013-04-30 2014-10-30 Rolls-Royce Deutschland Ltd & Co Kg Brennerdichtung für Gasturbinen-Brennkammerkopf und Hitzeschild
US11732892B2 (en) 2013-08-14 2023-08-22 General Electric Company Gas turbomachine diffuser assembly with radial flow splitters
US9470422B2 (en) 2013-10-22 2016-10-18 Siemens Energy, Inc. Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier
US9328664B2 (en) 2013-11-08 2016-05-03 Siemens Energy, Inc. Transition support system for combustion transition ducts for turbine engines
EP3783200B1 (en) 2014-12-11 2024-03-06 Siemens Energy Global GmbH & Co. KG Transition duct for a gas turbine engine
US10066837B2 (en) 2015-02-20 2018-09-04 General Electric Company Combustor aft mount assembly
CN109154202A (zh) * 2016-03-25 2019-01-04 西门子股份公司 燃气涡轮发动机、相应的密封部段和整合出口件
US11021977B2 (en) * 2018-11-02 2021-06-01 Chromalloy Gas Turbine Llc Diffuser guide vane with deflector panel having curved profile
KR102156416B1 (ko) * 2019-03-12 2020-09-16 두산중공업 주식회사 트랜지션 피스 조립체와 트랜지션 피스 모듈 및 상기 트랜지션 피스 조립체를 포함하는 연소기 및 가스 터빈

Family Cites Families (5)

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GB584820A (en) * 1944-12-22 1947-01-23 Lucas Ltd Joseph Improvements relating to internal combustion prime movers
US2592060A (en) * 1946-03-25 1952-04-08 Rolls Royce Mounting of combustion chambers in jet-propulsion and gas-turbine power-units
US2748567A (en) * 1949-10-13 1956-06-05 Gen Motors Corp Gas turbine combustion chamber with telescoping casing and liner sections
US2774618A (en) * 1954-09-13 1956-12-18 Winston T Alderson Combination ball and slip joint for pipes
US3609968A (en) * 1970-04-29 1971-10-05 Westinghouse Electric Corp Self-adjusting seal structure

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5447917A (en) * 1977-09-26 1979-04-16 Hitachi Ltd Flame cross-ignition tube for gas turbine
JP2010276018A (ja) * 2009-05-28 2010-12-09 General Electric Co <Ge> 拡大フラ・シール
JP2011058496A (ja) * 2009-09-11 2011-03-24 General Electric Co <Ge> タービンエンジンのための円周方向自己膨張式支持体
JP2015036548A (ja) * 2013-08-14 2015-02-23 ゼネラル・エレクトリック・カンパニイ ガスターボ機械用の、ディフューザが一体化された内部筒部材

Also Published As

Publication number Publication date
JPS5112763B2 (enrdf_load_stackoverflow) 1976-04-22
GB1355728A (en) 1974-06-05
US3759038A (en) 1973-09-18
DE2258719A1 (de) 1973-06-14
CA961654A (en) 1975-01-28
CH561358A5 (enrdf_load_stackoverflow) 1975-04-30

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