JP2011021601A5 - - Google Patents

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Publication number
JP2011021601A5
JP2011021601A5 JP2010152603A JP2010152603A JP2011021601A5 JP 2011021601 A5 JP2011021601 A5 JP 2011021601A5 JP 2010152603 A JP2010152603 A JP 2010152603A JP 2010152603 A JP2010152603 A JP 2010152603A JP 2011021601 A5 JP2011021601 A5 JP 2011021601A5
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JP
Japan
Prior art keywords
seal
circumferential seal
attaching
outer circumferential
inner circumferential
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
JP2010152603A
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English (en)
Japanese (ja)
Other versions
JP2011021601A (ja
JP5743442B2 (ja
Filing date
Publication date
Priority claimed from US12/505,778 external-priority patent/US8141879B2/en
Application filed filed Critical
Publication of JP2011021601A publication Critical patent/JP2011021601A/ja
Publication of JP2011021601A5 publication Critical patent/JP2011021601A5/ja
Application granted granted Critical
Publication of JP5743442B2 publication Critical patent/JP5743442B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2010152603A 2009-07-20 2010-07-05 タービンエンジン用のシール及びタービンエンジンを組立てる方法 Active JP5743442B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/505,778 US8141879B2 (en) 2009-07-20 2009-07-20 Seals for a turbine engine, and methods of assembling a turbine engine
US12/505,778 2009-07-20

Publications (3)

Publication Number Publication Date
JP2011021601A JP2011021601A (ja) 2011-02-03
JP2011021601A5 true JP2011021601A5 (enExample) 2013-08-15
JP5743442B2 JP5743442B2 (ja) 2015-07-01

Family

ID=43384155

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010152603A Active JP5743442B2 (ja) 2009-07-20 2010-07-05 タービンエンジン用のシール及びタービンエンジンを組立てる方法

Country Status (5)

Country Link
US (1) US8141879B2 (enExample)
JP (1) JP5743442B2 (enExample)
CN (1) CN101956608A (enExample)
CH (1) CH701538B1 (enExample)
DE (1) DE102010036347B4 (enExample)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120119449A1 (en) * 2010-11-11 2012-05-17 General Electric Company Transition Piece Sealing Assembly With Seal Overlay
US20120280460A1 (en) * 2011-05-06 2012-11-08 General Electric Company Two-piece side seal with covers
US9115585B2 (en) 2011-06-06 2015-08-25 General Electric Company Seal assembly for gas turbine
US8701415B2 (en) * 2011-11-09 2014-04-22 General Electric Company Flexible metallic seal for transition duct in turbine system
US9115808B2 (en) * 2012-02-13 2015-08-25 General Electric Company Transition piece seal assembly for a turbomachine
US20130283817A1 (en) * 2012-04-30 2013-10-31 General Electric Company Flexible seal for transition duct in turbine system
US9038394B2 (en) * 2012-04-30 2015-05-26 General Electric Company Convolution seal for transition duct in turbine system
FR2991387B1 (fr) * 2012-06-01 2016-03-04 Snecma Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
US9528383B2 (en) * 2013-12-31 2016-12-27 General Electric Company System for sealing between combustors and turbine of gas turbine engine
US9416675B2 (en) * 2014-01-27 2016-08-16 General Electric Company Sealing device for providing a seal in a turbomachine
JP6545257B2 (ja) * 2014-09-05 2019-07-17 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ トランジション−タービンシールアセンブリ
US20160131041A1 (en) * 2014-11-06 2016-05-12 General Electric Company Turbomachine including a tranistion piece to turbine portion variable purge flow seal member
JP5886465B1 (ja) * 2015-09-08 2016-03-16 三菱日立パワーシステムズ株式会社 シール部材の組付構造及び組付方法、シール部材、ガスタービン
US10689995B2 (en) * 2016-05-27 2020-06-23 General Electric Company Side seal with reduced corner leakage
US10508602B2 (en) 2016-09-01 2019-12-17 General Electric Company Corner flow reduction seals
US10690059B2 (en) 2016-09-26 2020-06-23 General Electric Company Advanced seals with reduced corner leakage
US10830069B2 (en) * 2016-09-26 2020-11-10 General Electric Company Pressure-loaded seals
IT201800003496A1 (it) 2018-03-13 2019-09-13 Nuovo Pignone Tecnologie Srl Un sistema di tenuta per turbomacchine e turbomacchina comprendente il sistema di tenuta
JP7149807B2 (ja) 2018-11-01 2022-10-07 三菱重工業株式会社 ガスタービン燃焼器

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3965066A (en) 1974-03-15 1976-06-22 General Electric Company Combustor-turbine nozzle interconnection
CH633351A5 (de) * 1978-11-09 1982-11-30 Sulzer Ag Waermedehnungen nachgebende abdichtung einer ringbrennkammer fuer eine gasturbine.
US5289677A (en) 1992-12-16 1994-03-01 United Technologies Corporation Combined support and seal ring for a combustor
JPH09195799A (ja) * 1996-01-17 1997-07-29 Mitsubishi Heavy Ind Ltd 燃焼器のスプリングシール装置
JPH11200894A (ja) 1998-01-12 1999-07-27 Hitachi Ltd ガスタービン及びその圧縮空気漏洩防止装置
US6162014A (en) 1998-09-22 2000-12-19 General Electric Company Turbine spline seal and turbine assembly containing such spline seal
FR2786222B1 (fr) * 1998-11-19 2000-12-29 Snecma Dispositif d'etancheite a lamelle
US20020121744A1 (en) * 2001-03-05 2002-09-05 General Electric Company Low leakage flexible cloth seals for turbine combustors
US20030039542A1 (en) * 2001-08-21 2003-02-27 Cromer Robert Harold Transition piece side sealing element and turbine assembly containing such seal
JP3848155B2 (ja) * 2001-12-25 2006-11-22 株式会社日立製作所 ガスタービン燃焼器
US6599089B2 (en) * 2001-12-28 2003-07-29 General Electric Company Supplemental seal for the chordal hinge seal in a gas turbine
JP4025172B2 (ja) * 2002-10-30 2007-12-19 株式会社日立製作所 ガスタービン設備
US7178340B2 (en) 2003-09-24 2007-02-20 Power Systems Mfg., Llc Transition duct honeycomb seal
FR2860264B1 (fr) * 2003-09-30 2006-02-10 Snecma Moteurs Turbomachine comprenant deux elements mis en communication avec interposition d'un joint
US20060076126A1 (en) * 2004-10-07 2006-04-13 Fandry Shane L Heat exchanger baffle
US7246995B2 (en) * 2004-12-10 2007-07-24 Siemens Power Generation, Inc. Seal usable between a transition and a turbine vane assembly in a turbine engine
CN101694181B (zh) * 2005-08-23 2012-09-05 三菱重工业株式会社 用于燃气轮机燃烧室的密封结构
US20070134087A1 (en) * 2005-12-08 2007-06-14 General Electric Company Methods and apparatus for assembling turbine engines

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