ATE510108T1 - Übergangsstück einer gasturbinenbrennkammer - Google Patents

Übergangsstück einer gasturbinenbrennkammer

Info

Publication number
ATE510108T1
ATE510108T1 AT05077569T AT05077569T ATE510108T1 AT E510108 T1 ATE510108 T1 AT E510108T1 AT 05077569 T AT05077569 T AT 05077569T AT 05077569 T AT05077569 T AT 05077569T AT E510108 T1 ATE510108 T1 AT E510108T1
Authority
AT
Austria
Prior art keywords
gas turbine
transition piece
outlet
combustion chamber
turbine combustion
Prior art date
Application number
AT05077569T
Other languages
English (en)
Inventor
Vincent T Riggi Jr
Ronald A Riggi
Warren Peck
Martin Haar
Original Assignee
Turbine Services 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 Turbine Services Ltd filed Critical Turbine Services Ltd
Application granted granted Critical
Publication of ATE510108T1 publication Critical patent/ATE510108T1/de

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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • 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
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Connection Of Plates (AREA)
AT05077569T 2005-08-09 2005-11-10 Übergangsstück einer gasturbinenbrennkammer ATE510108T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/200,382 US7377117B2 (en) 2005-08-09 2005-08-09 Transition piece for gas turbine

Publications (1)

Publication Number Publication Date
ATE510108T1 true ATE510108T1 (de) 2011-06-15

Family

ID=36121287

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05077569T ATE510108T1 (de) 2005-08-09 2005-11-10 Übergangsstück einer gasturbinenbrennkammer

Country Status (4)

Country Link
US (1) US7377117B2 (de)
EP (1) EP1752612B1 (de)
AT (1) ATE510108T1 (de)
CA (1) CA2525643C (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8001787B2 (en) 2007-02-27 2011-08-23 Siemens Energy, Inc. Transition support system for combustion transition ducts for turbine engines
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
KR100962129B1 (ko) 2007-12-28 2010-06-10 한전케이피에스 주식회사 트랜지션피스 얼라인먼트 장치 및 트랜지션피스 얼라인먼트 방법
US8418474B2 (en) * 2008-01-29 2013-04-16 Alstom Technology Ltd. Altering a natural frequency of a gas turbine transition duct
US7762086B2 (en) * 2008-03-12 2010-07-27 United Technologies Corporation Nozzle extension assembly for ground and flight testing
US8245515B2 (en) * 2008-08-06 2012-08-21 General Electric Company Transition duct aft end frame cooling and related method
US8091365B2 (en) * 2008-08-12 2012-01-10 Siemens Energy, Inc. Canted outlet for transition in a gas turbine engine
US8113003B2 (en) * 2008-08-12 2012-02-14 Siemens Energy, Inc. Transition with a linear flow path for use in a gas turbine engine
US9284887B2 (en) 2009-12-31 2016-03-15 Rolls-Royce North American Technologies, Inc. Gas turbine engine and frame
US9255484B2 (en) * 2011-03-16 2016-02-09 General Electric Company Aft frame and method for cooling aft frame
US8997501B2 (en) * 2011-06-02 2015-04-07 General Electric Company System for mounting combustor transition piece to frame of gas turbine engine
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
US20170145839A1 (en) * 2014-06-17 2017-05-25 Siemens Energy, Inc. Transition duct system with a robust converging flow joint at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine
US9702258B2 (en) 2014-07-01 2017-07-11 Siemens Energy, Inc. Adjustable transition support and method of using the same
EP2990615A1 (de) 2014-08-26 2016-03-02 Siemens Aktiengesellschaft Vorrichtung mit Lastarm zum Ein- und Ausbauen eines Bauteils einer Gasturbine
US11156112B2 (en) * 2018-11-02 2021-10-26 Chromalloy Gas Turbine Llc Method and apparatus for mounting a transition duct in a gas turbine engine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5554636A (en) 1978-10-16 1980-04-22 Hitachi Ltd Combustor of gas turbine
US4422288A (en) 1981-03-02 1983-12-27 General Electric Company Aft mounting system for combustion transition duct members
GB2115877B (en) * 1982-03-04 1985-05-01 Gen Electric Aft mounting system for gas turbine combustion transition duct members
US5414999A (en) 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
EP0718468B1 (de) 1994-12-20 2001-10-31 General Electric Company Verstärkungrahmen für Gasturbinenbrennkammerendstück
US6442946B1 (en) * 2000-11-14 2002-09-03 Power Systems Mfg., Llc Three degrees of freedom aft mounting system for gas turbine transition duct
JP2002243154A (ja) 2001-02-16 2002-08-28 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器
US6619915B1 (en) 2002-08-06 2003-09-16 Power Systems Mfg, Llc Thermally free aft frame for a transition duct
US6662567B1 (en) 2002-08-14 2003-12-16 Power Systems Mfg, Llc Transition duct mounting system
US6675584B1 (en) 2002-08-15 2004-01-13 Power Systems Mfg, Llc Coated seal article used in turbine engines
US6834507B2 (en) 2002-08-15 2004-12-28 Power Systems Mfg., Llc Convoluted seal with enhanced wear capability
US6890148B2 (en) 2003-08-28 2005-05-10 Siemens Westinghouse Power Corporation Transition duct cooling system

Also Published As

Publication number Publication date
US7377117B2 (en) 2008-05-27
EP1752612A1 (de) 2007-02-14
EP1752612B1 (de) 2011-05-18
CA2525643C (en) 2013-03-26
US20070033941A1 (en) 2007-02-15
CA2525643A1 (en) 2007-02-09

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