JP2013227973A5 - - Google Patents

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Publication number
JP2013227973A5
JP2013227973A5 JP2013087923A JP2013087923A JP2013227973A5 JP 2013227973 A5 JP2013227973 A5 JP 2013227973A5 JP 2013087923 A JP2013087923 A JP 2013087923A JP 2013087923 A JP2013087923 A JP 2013087923A JP 2013227973 A5 JP2013227973 A5 JP 2013227973A5
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JP
Japan
Prior art keywords
transition
piece
transition piece
thin
ratio
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.)
Granted
Application number
JP2013087923A
Other languages
English (en)
Japanese (ja)
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JP2013227973A (ja
JP6130714B2 (ja
Filing date
Publication date
Priority claimed from US13/454,785 external-priority patent/US9109447B2/en
Application filed filed Critical
Publication of JP2013227973A publication Critical patent/JP2013227973A/ja
Publication of JP2013227973A5 publication Critical patent/JP2013227973A5/ja
Application granted granted Critical
Publication of JP6130714B2 publication Critical patent/JP6130714B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013087923A 2012-04-24 2013-04-19 遷移ピースを含む燃焼システムおよび鋳造超合金を使用した形成方法 Active JP6130714B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/454,785 US9109447B2 (en) 2012-04-24 2012-04-24 Combustion system including a transition piece and method of forming using a cast superalloy
US13/454,785 2012-04-24

Publications (3)

Publication Number Publication Date
JP2013227973A JP2013227973A (ja) 2013-11-07
JP2013227973A5 true JP2013227973A5 (enExample) 2016-06-09
JP6130714B2 JP6130714B2 (ja) 2017-05-17

Family

ID=48139842

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013087923A Active JP6130714B2 (ja) 2012-04-24 2013-04-19 遷移ピースを含む燃焼システムおよび鋳造超合金を使用した形成方法

Country Status (5)

Country Link
US (1) US9109447B2 (enExample)
EP (1) EP2657453B1 (enExample)
JP (1) JP6130714B2 (enExample)
CN (1) CN103375187B (enExample)
RU (1) RU2013118656A (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2915957A1 (en) * 2014-03-05 2015-09-09 Siemens Aktiengesellschaft Cast tubular duct for a gas turbine and manufacturing method thereof
US10830142B2 (en) * 2016-10-10 2020-11-10 General Electric Company Combustor aft frame cooling
CN107178792A (zh) * 2017-06-13 2017-09-19 东方电气集团东方汽轮机有限公司 一种燃气轮机及航空发动机燃烧器尾筒结构

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3527285A (en) 1967-11-07 1970-09-08 Gen Motors Corp Method and mold for casting thin wall cylinders
US3657882A (en) * 1970-11-13 1972-04-25 Westinghouse Electric Corp Combustion apparatus
US6416596B1 (en) 1974-07-17 2002-07-09 The General Electric Company Cast nickel-base alloy
US4236378A (en) 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4422288A (en) * 1981-03-02 1983-12-27 General Electric Company Aft mounting system for combustion transition duct members
US5335502A (en) 1992-09-09 1994-08-09 General Electric Company Arched combustor
US5414999A (en) 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
JP3756994B2 (ja) * 1995-07-11 2006-03-22 株式会社日立製作所 ガスタービン用燃焼器及びガスタービン並びにその部材
US5964091A (en) * 1995-07-11 1999-10-12 Hitachi, Ltd. Gas turbine combustor and gas turbine
JPH10226838A (ja) * 1997-02-19 1998-08-25 Hitachi Metals Ltd 燃焼器用鋳造部品およびその製造方法
JP4097233B2 (ja) * 1997-05-07 2008-06-11 株式会社東芝 X線管の収容容器およびその製造方法、並びにx線管装置
WO1999006771A1 (en) 1997-07-31 1999-02-11 Alliedsignal Inc. Rib turbulators for combustor external cooling
US6553767B2 (en) 2001-06-11 2003-04-29 General Electric Company Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form
US6851263B2 (en) 2002-10-29 2005-02-08 General Electric Company Liner for a gas turbine engine combustor having trapped vortex cavity
US6890148B2 (en) * 2003-08-28 2005-05-10 Siemens Westinghouse Power Corporation Transition duct cooling system
US7373772B2 (en) 2004-03-17 2008-05-20 General Electric Company Turbine combustor transition piece having dilution holes
US7082766B1 (en) * 2005-03-02 2006-08-01 General Electric Company One-piece can combustor
US7377117B2 (en) 2005-08-09 2008-05-27 Turbine Services, Ltd. Transition piece for gas turbine
US7540156B2 (en) 2005-11-21 2009-06-02 General Electric Company Combustion liner for gas turbine formed of cast nickel-based superalloy
US7631504B2 (en) * 2006-02-21 2009-12-15 General Electric Company Methods and apparatus for assembling gas turbine engines
US7908867B2 (en) * 2007-09-14 2011-03-22 Siemens Energy, Inc. Wavy CMC wall hybrid ceramic apparatus
US20090249791A1 (en) * 2008-04-08 2009-10-08 General Electric Company Transition piece impingement sleeve and method of assembly
US8549861B2 (en) 2009-01-07 2013-10-08 General Electric Company Method and apparatus to enhance transition duct cooling in a gas turbine engine
US8397511B2 (en) * 2009-05-19 2013-03-19 General Electric Company System and method for cooling a wall of a gas turbine combustor
US8226886B2 (en) * 2009-08-31 2012-07-24 General Electric Company Nickel-based superalloys and articles

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