JPS6242214B2 - - Google Patents

Info

Publication number
JPS6242214B2
JPS6242214B2 JP57031871A JP3187182A JPS6242214B2 JP S6242214 B2 JPS6242214 B2 JP S6242214B2 JP 57031871 A JP57031871 A JP 57031871A JP 3187182 A JP3187182 A JP 3187182A JP S6242214 B2 JPS6242214 B2 JP S6242214B2
Authority
JP
Japan
Prior art keywords
bracket
support device
transition duct
boss
support
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
Application number
JP57031871A
Other languages
English (en)
Japanese (ja)
Other versions
JPS57168024A (en
Inventor
Ebuan Suteeberu Chaarusu
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 Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JPS57168024A publication Critical patent/JPS57168024A/ja
Publication of JPS6242214B2 publication Critical patent/JPS6242214B2/ja
Granted 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
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L3/00—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets
    • F16L3/16—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets with special provision allowing movement of the pipe
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Flanged Joints, Insulating Joints, And Other Joints (AREA)
JP57031871A 1981-03-02 1982-03-02 Rear attachment system for combustion shift duct Granted JPS57168024A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/239,437 US4422288A (en) 1981-03-02 1981-03-02 Aft mounting system for combustion transition duct members

Publications (2)

Publication Number Publication Date
JPS57168024A JPS57168024A (en) 1982-10-16
JPS6242214B2 true JPS6242214B2 (US07923587-20110412-C00001.png) 1987-09-07

Family

ID=22902123

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57031871A Granted JPS57168024A (en) 1981-03-02 1982-03-02 Rear attachment system for combustion shift duct

Country Status (4)

Country Link
US (1) US4422288A (US07923587-20110412-C00001.png)
JP (1) JPS57168024A (US07923587-20110412-C00001.png)
CA (1) CA1168457A (US07923587-20110412-C00001.png)
FR (1) FR2500905B1 (US07923587-20110412-C00001.png)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02113313U (US07923587-20110412-C00001.png) * 1989-02-23 1990-09-11

Families Citing this family (88)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4793768A (en) * 1985-12-27 1988-12-27 Sundstrand Corporation Seal and turbine mount
FR2623249A1 (fr) * 1987-11-12 1989-05-19 Snecma Ensemble constitue de deux pieces en materiaux ayant des coefficients de dilatation differents, reliees entre elles et methode d'assemblage
US5081833A (en) * 1988-04-21 1992-01-21 Nuovopignone-Industrie Meccaniche E Fonderia S.P.A. Device for keeping the annular outlet mouth of the gas volute always centered about the nozzle assembly in a gas turbine
US5265412A (en) * 1992-07-28 1993-11-30 General Electric Company Self-accommodating brush seal for gas turbine combustor
US5400586A (en) * 1992-07-28 1995-03-28 General Electric Co. 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
US5749584A (en) 1992-11-19 1998-05-12 General Electric Company Combined brush seal and labyrinth seal segment for rotary machines
US5474306A (en) * 1992-11-19 1995-12-12 General Electric Co. Woven seal and hybrid cloth-brush seals for turbine applications
US5480162A (en) * 1993-09-08 1996-01-02 United Technologies Corporation Axial load carrying brush seal
US5414999A (en) * 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
DE4340530A1 (de) * 1993-11-29 1995-06-01 Abb Management Ag Vorrichtung zur Abstützung dünner Liner
EP0718468B1 (en) * 1994-12-20 2001-10-31 General Electric Company Transition piece frame support
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
GB9813972D0 (en) * 1998-06-30 1998-08-26 Rolls Royce Plc A combustion chamber
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
US6412268B1 (en) 2000-04-06 2002-07-02 General Electric Company Cooling air recycling for gas turbine transition duct end frame and related method
US6442946B1 (en) * 2000-11-14 2002-09-03 Power Systems Mfg., Llc Three degrees of freedom aft mounting system for gas turbine transition duct
US6450762B1 (en) * 2001-01-31 2002-09-17 General Electric Company Integral aft seal for turbine applications
US6662567B1 (en) 2002-08-14 2003-12-16 Power Systems Mfg, Llc Transition duct mounting system
US6860108B2 (en) * 2003-01-22 2005-03-01 Mitsubishi Heavy Industries, Ltd. Gas turbine tail tube seal and gas turbine using the same
US6904756B2 (en) * 2003-02-28 2005-06-14 Power Systems Mfg, Llc Transition duct support bracket wear cover
US7178341B2 (en) * 2004-06-17 2007-02-20 Siemens Power Generation, Inc. Multi-zone tubing assembly for a transition piece of a gas turbine
US7354244B2 (en) 2004-09-01 2008-04-08 Aos Holding Company Blower and method of conveying fluids
US8015818B2 (en) * 2005-02-22 2011-09-13 Siemens Energy, Inc. Cooled transition duct for a gas turbine engine
US7721547B2 (en) * 2005-06-27 2010-05-25 Siemens Energy, Inc. Combustion transition duct providing stage 1 tangential turning for turbine engines
US7377117B2 (en) * 2005-08-09 2008-05-27 Turbine Services, Ltd. Transition piece for gas turbine
US8038351B2 (en) * 2007-03-30 2011-10-18 Roller Bearing Company Of America, Inc. Self-lubricated bearing assembly
US8240045B2 (en) * 2007-05-22 2012-08-14 Siemens Energy, Inc. Gas turbine transition duct coupling apparatus
US8151570B2 (en) * 2007-12-06 2012-04-10 Alstom Technology Ltd Transition duct cooling feed tubes
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
US7918433B2 (en) * 2008-06-25 2011-04-05 General Electric Company Transition piece mounting bracket and related method
US8549861B2 (en) * 2009-01-07 2013-10-08 General Electric Company Method and apparatus to enhance transition duct cooling in a gas turbine engine
US8215115B2 (en) * 2009-09-28 2012-07-10 Hamilton Sundstrand Corporation Combustor interface sealing arrangement
US8448444B2 (en) * 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
US8997501B2 (en) * 2011-06-02 2015-04-07 General Electric Company System for mounting combustor transition piece to frame of gas turbine engine
US8978388B2 (en) 2011-06-03 2015-03-17 General Electric Company Load member for transition duct in turbine system
US8448450B2 (en) 2011-07-05 2013-05-28 General Electric Company Support assembly for transition duct in turbine system
US8650852B2 (en) 2011-07-05 2014-02-18 General Electric Company Support assembly for transition duct in turbine system
US8974179B2 (en) 2011-11-09 2015-03-10 General Electric Company Convolution seal for transition duct in turbine system
US8701415B2 (en) 2011-11-09 2014-04-22 General Electric Company Flexible metallic seal for transition duct in turbine system
US8459041B2 (en) 2011-11-09 2013-06-11 General Electric Company Leaf seal for transition duct in turbine system
US9109447B2 (en) * 2012-04-24 2015-08-18 General Electric Company Combustion system including a transition piece and method of forming using a cast superalloy
US9038394B2 (en) 2012-04-30 2015-05-26 General Electric Company Convolution seal for transition duct in turbine system
US9133722B2 (en) 2012-04-30 2015-09-15 General Electric Company Transition duct with late injection in turbine system
US8707673B1 (en) 2013-01-04 2014-04-29 General Electric Company Articulated transition duct in turbomachine
US9080447B2 (en) 2013-03-21 2015-07-14 General Electric Company Transition duct with divided upstream and downstream portions
US20150040394A1 (en) * 2013-08-07 2015-02-12 General Electric Company Remote turbine component replacement apparatus and method of remotely replacing a turbine component
US9458732B2 (en) 2013-10-25 2016-10-04 General Electric Company Transition duct assembly with modified trailing edge in turbine system
WO2015119754A1 (en) * 2014-02-04 2015-08-13 United Technologies Corporation Brackets for gas turbine engine components
US9702258B2 (en) 2014-07-01 2017-07-11 Siemens Energy, Inc. Adjustable transition support and method of using the same
US20160047313A1 (en) * 2014-08-15 2016-02-18 General Electric Company Bushing for joining turbomachine components
US11118465B2 (en) * 2014-08-19 2021-09-14 Mitsubishi Power, Ltd. Gas turbine combustor transition piece including inclined surface at downstream end portions for reducing pressure fluctuations
US9574460B2 (en) * 2014-10-30 2017-02-21 Siemens Energy, Inc. Support arrangement for a transition piece of a gas turbine engine
JP6490222B2 (ja) 2014-12-11 2019-03-27 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ 移行ダクト支持および支持剛性の調整レベルを提供する方法
US10520193B2 (en) 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
US10227883B2 (en) 2016-03-24 2019-03-12 General Electric Company Transition duct assembly
US10260360B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly
US10260752B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10260424B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10145251B2 (en) 2016-03-24 2018-12-04 General Electric Company Transition duct assembly
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
US10584876B2 (en) 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US11002190B2 (en) 2016-03-25 2021-05-11 General Electric Company Segmented annular combustion system
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
JP6650849B2 (ja) * 2016-08-25 2020-02-19 三菱日立パワーシステムズ株式会社 ガスタービン
JP6619307B2 (ja) * 2016-09-05 2019-12-11 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US10865660B2 (en) * 2017-09-12 2020-12-15 DOOSAN Heavy Industries Construction Co., LTD Transition piece support structure, gas turbine combustor including same, and method of installing same
DE102020111200A1 (de) 2020-04-24 2021-10-28 Man Energy Solutions Se Befestigungseinrichtung zur elastischen Aufhängung eines Übergangskanals an einem Leitschaufelträger einer Gasturbine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511432A (en) * 1945-02-20 1950-06-13 Power Jets Res & Dev Ltd Support for multiple flame tubes
US2529958A (en) * 1945-10-09 1950-11-14 Bristol Aeroplane Co Ltd Means for supporting gas-turbine power plants
US2509503A (en) * 1946-02-12 1950-05-30 Lucas Ltd Joseph Combustion chamber for prime movers
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner
GB743205A (en) * 1953-03-04 1956-01-11 Rolls Royce Improvements in or relating to power-plant installations for aircraft
FR1160619A (fr) * 1956-11-22 1958-07-22 Lucas Industries Ltd Chambre de combustion pour combustibles liquides
US3007312A (en) * 1959-11-23 1961-11-07 Gen Motors Corp Combustion liner locater
US3232054A (en) * 1964-02-20 1966-02-01 Lucas Industries Ltd Liquid fuel combustion apparatus, for jet-propulsion engines, gas turbines, or other prime movers
US3481146A (en) * 1967-12-28 1969-12-02 Lucas Industries Ltd Combustion apparatus for gas turbine engines
FR1551357A (US07923587-20110412-C00001.png) * 1967-12-28 1968-12-27
US3572029A (en) * 1969-09-04 1971-03-23 Us Air Force Rocket engine thrust chamber attachment means
US3609968A (en) * 1970-04-29 1971-10-05 Westinghouse Electric Corp Self-adjusting seal structure
US3741678A (en) * 1971-04-28 1973-06-26 Westinghouse Electric Corp Cooling air profiling structures for a gas turbine
US3750398A (en) * 1971-05-17 1973-08-07 Westinghouse Electric Corp Static seal structure
US3759038A (en) * 1971-12-09 1973-09-18 Westinghouse Electric Corp Self aligning combustor and transition structure for a gas turbine
US4016718A (en) * 1975-07-21 1977-04-12 United Technologies Corporation Gas turbine engine having an improved transition duct support
US3999784A (en) * 1975-09-18 1976-12-28 Caterpillar Tractor Co. Tube clamp mounting
JPS5554636A (en) * 1978-10-16 1980-04-22 Hitachi Ltd Combustor of gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02113313U (US07923587-20110412-C00001.png) * 1989-02-23 1990-09-11

Also Published As

Publication number Publication date
US4422288A (en) 1983-12-27
FR2500905A1 (fr) 1982-09-03
CA1168457A (en) 1984-06-05
JPS57168024A (en) 1982-10-16
FR2500905B1 (fr) 1985-08-09

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