CN103291457B - 具有热护罩的过渡连接件后架组件 - Google Patents

具有热护罩的过渡连接件后架组件 Download PDF

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Publication number
CN103291457B
CN103291457B CN201310065321.5A CN201310065321A CN103291457B CN 103291457 B CN103291457 B CN 103291457B CN 201310065321 A CN201310065321 A CN 201310065321A CN 103291457 B CN103291457 B CN 103291457B
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China
Prior art keywords
transition piece
heat shield
dilution
aft frame
frame
Prior art date
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CN201310065321.5A
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English (en)
Chinese (zh)
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CN103291457A (zh
Inventor
C.P.威利斯
W.L.拜尔恩
D.W.奇拉
D.T.勒蒙
P.B.梅尔顿
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General Electric Company PLC
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General Electric Co
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Publication of CN103291457B publication Critical patent/CN103291457B/zh
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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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
CN201310065321.5A 2012-03-02 2013-03-01 具有热护罩的过渡连接件后架组件 Active CN103291457B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/410,417 2012-03-02
US13/410417 2012-03-02
US13/410,417 US9010127B2 (en) 2012-03-02 2012-03-02 Transition piece aft frame assembly having a heat shield

Publications (2)

Publication Number Publication Date
CN103291457A CN103291457A (zh) 2013-09-11
CN103291457B true CN103291457B (zh) 2017-03-01

Family

ID=47790067

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310065321.5A Active CN103291457B (zh) 2012-03-02 2013-03-01 具有热护罩的过渡连接件后架组件

Country Status (5)

Country Link
US (1) US9010127B2 (https=)
EP (1) EP2634372B1 (https=)
JP (1) JP6050702B2 (https=)
CN (1) CN103291457B (https=)
RU (1) RU2638416C2 (https=)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9115585B2 (en) * 2011-06-06 2015-08-25 General Electric Company Seal assembly for gas turbine
WO2016068857A1 (en) * 2014-10-28 2016-05-06 Siemens Aktiengesellschaft Seal assembly between a transition duct and the first row vane assembly for use in turbine engines
KR101686336B1 (ko) * 2015-07-03 2016-12-13 두산중공업 주식회사 가스터빈의 트랜지션피스 연결장치
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
GB201614711D0 (en) * 2016-08-31 2016-10-12 Rolls Royce Plc Axial flow machine
JP6966354B2 (ja) * 2018-02-28 2021-11-17 三菱パワー株式会社 ガスタービン燃焼器
US12595908B1 (en) * 2025-01-14 2026-04-07 Ge Infrastructure Technology Llc Combustor with additively manufactured combustor body having aft frame with heat transfer augmentation

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1143107A2 (en) * 2000-04-06 2001-10-10 General Electric Company Gas turbine transition duct end frame cooling
EP1731715A1 (de) * 2005-06-10 2006-12-13 Siemens Aktiengesellschaft Übergangsbereich zwischen einer Brennkammer und einer Turbineneinheit
CN101644191A (zh) * 2008-08-06 2010-02-10 通用电气公司 过渡管路后端构架的冷却及相关方法
CN101922353A (zh) * 2009-03-31 2010-12-22 通用电气公司 从密封槽供给薄膜冷却孔
EP2402659A1 (de) * 2010-07-01 2012-01-04 Siemens Aktiengesellschaft Brennkammeraußenschale

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4465284A (en) 1983-09-19 1984-08-14 General Electric Company Scalloped cooling of gas turbine transition piece frame
JP4031590B2 (ja) * 1999-03-08 2008-01-09 三菱重工業株式会社 燃焼器の尾筒シール構造及びその構造を用いたガスタービン
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
JP3993484B2 (ja) * 2002-07-15 2007-10-17 三菱重工業株式会社 燃焼器冷却構造
US6834507B2 (en) * 2002-08-15 2004-12-28 Power Systems Mfg., Llc Convoluted seal with enhanced wear capability
JP3795036B2 (ja) * 2003-03-14 2006-07-12 三菱重工業株式会社 タービン尾筒のシール構造およびシール装置
JP4191552B2 (ja) 2003-07-14 2008-12-03 三菱重工業株式会社 ガスタービン尾筒の冷却構造
FR2891300A1 (fr) * 2005-09-23 2007-03-30 Snecma Sa Dispositif de controle de jeu dans une turbine a gaz
US8001787B2 (en) * 2007-02-27 2011-08-23 Siemens Energy, Inc. Transition support system for combustion transition ducts for turbine engines
US8079219B2 (en) * 2008-09-30 2011-12-20 General Electric Company Impingement cooled combustor seal

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1143107A2 (en) * 2000-04-06 2001-10-10 General Electric Company Gas turbine transition duct end frame cooling
EP1731715A1 (de) * 2005-06-10 2006-12-13 Siemens Aktiengesellschaft Übergangsbereich zwischen einer Brennkammer und einer Turbineneinheit
CN101644191A (zh) * 2008-08-06 2010-02-10 通用电气公司 过渡管路后端构架的冷却及相关方法
CN101922353A (zh) * 2009-03-31 2010-12-22 通用电气公司 从密封槽供给薄膜冷却孔
EP2402659A1 (de) * 2010-07-01 2012-01-04 Siemens Aktiengesellschaft Brennkammeraußenschale

Also Published As

Publication number Publication date
JP2013181749A (ja) 2013-09-12
US20130227964A1 (en) 2013-09-05
RU2638416C2 (ru) 2017-12-13
CN103291457A (zh) 2013-09-11
RU2013108923A (ru) 2014-09-10
JP6050702B2 (ja) 2016-12-21
EP2634372A1 (en) 2013-09-04
US9010127B2 (en) 2015-04-21
EP2634372B1 (en) 2017-07-26

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Effective date of registration: 20231226

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Patentee after: GENERAL ELECTRIC CO. LTD.

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Patentee before: General Electric Co.