JP6050702B2 - 熱シールドを有するトランジションピース後方フレーム組立体 - Google Patents

熱シールドを有するトランジションピース後方フレーム組立体 Download PDF

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Publication number
JP6050702B2
JP6050702B2 JP2013036591A JP2013036591A JP6050702B2 JP 6050702 B2 JP6050702 B2 JP 6050702B2 JP 2013036591 A JP2013036591 A JP 2013036591A JP 2013036591 A JP2013036591 A JP 2013036591A JP 6050702 B2 JP6050702 B2 JP 6050702B2
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JP
Japan
Prior art keywords
transition piece
heat shield
rear frame
frame assembly
air flow
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.)
Active
Application number
JP2013036591A
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English (en)
Japanese (ja)
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JP2013181749A5 (enExample
JP2013181749A (ja
Inventor
クリストファー・ポール・ウィリス
ウィリアム・ローレンス・バーン
デイビッド・ウィリアム・チラー
ドナルド・ティモシー・レモン
パトリック・ベネディクト・メルトン
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2013181749A publication Critical patent/JP2013181749A/ja
Publication of JP2013181749A5 publication Critical patent/JP2013181749A5/ja
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Publication of JP6050702B2 publication Critical patent/JP6050702B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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)
JP2013036591A 2012-03-02 2013-02-27 熱シールドを有するトランジションピース後方フレーム組立体 Active JP6050702B2 (ja)

Applications Claiming Priority (2)

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

Publications (3)

Publication Number Publication Date
JP2013181749A JP2013181749A (ja) 2013-09-12
JP2013181749A5 JP2013181749A5 (enExample) 2016-04-14
JP6050702B2 true JP6050702B2 (ja) 2016-12-21

Family

ID=47790067

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013036591A Active JP6050702B2 (ja) 2012-03-02 2013-02-27 熱シールドを有するトランジションピース後方フレーム組立体

Country Status (5)

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

Families Citing this family (6)

* 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

Family Cites Families (15)

* 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
US6412268B1 (en) * 2000-04-06 2002-07-02 General Electric Company Cooling air recycling for gas turbine transition duct end frame and related method
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
EP1731715A1 (de) 2005-06-10 2006-12-13 Siemens Aktiengesellschaft Übergangsbereich zwischen einer Brennkammer und einer Turbineneinheit
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
US8245515B2 (en) * 2008-08-06 2012-08-21 General Electric Company Transition duct aft end frame cooling and related method
US8079219B2 (en) * 2008-09-30 2011-12-20 General Electric Company Impingement cooled combustor seal
US8092159B2 (en) * 2009-03-31 2012-01-10 General Electric Company Feeding film cooling holes from seal slots
EP2402659A1 (de) 2010-07-01 2012-01-04 Siemens Aktiengesellschaft Brennkammeraußenschale

Also Published As

Publication number Publication date
CN103291457A (zh) 2013-09-11
EP2634372B1 (en) 2017-07-26
EP2634372A1 (en) 2013-09-04
RU2638416C2 (ru) 2017-12-13
JP2013181749A (ja) 2013-09-12
US9010127B2 (en) 2015-04-21
CN103291457B (zh) 2017-03-01
US20130227964A1 (en) 2013-09-05
RU2013108923A (ru) 2014-09-10

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