CH701538A8 - Verfahren zum Abdichten mehrerer Brennkammern. - Google Patents

Verfahren zum Abdichten mehrerer Brennkammern. Download PDF

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Publication number
CH701538A8
CH701538A8 CH01146/10A CH11462010A CH701538A8 CH 701538 A8 CH701538 A8 CH 701538A8 CH 01146/10 A CH01146/10 A CH 01146/10A CH 11462010 A CH11462010 A CH 11462010A CH 701538 A8 CH701538 A8 CH 701538A8
Authority
CH
Switzerland
Prior art keywords
sealing
seal
combustion chambers
extended ends
outer circumferential
Prior art date
Application number
CH01146/10A
Other languages
English (en)
Other versions
CH701538B1 (de
CH701538A2 (de
Inventor
Kevin Weston Mcmahan
Timur R Repikov
Krishna Kumar Venkataraman
Kara Edwards
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH701538A2 publication Critical patent/CH701538A2/de
Publication of CH701538A8 publication Critical patent/CH701538A8/de
Publication of CH701538B1 publication Critical patent/CH701538B1/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
    • F05D2240/00—Components
    • F05D2240/55—Seals
    • F05D2240/57—Leaf seals
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gasket Seals (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Eine Seitendichtung (260) zur Abdichtung der Seitenränder benachbarter Brennkammern einer Turbinenmaschine enthält verlängerte Enden (262/624). Die verlängerten Enden der Seitendichtung liegen gegen eine innere und äussere Umfangsdichtung (250/254) an und dichten gegen diese ab, um eine Leckage von Verbrennungsgasen zu verhindern.
CH01146/10A 2009-07-20 2010-07-14 Verfahren zum Abdichten mehrerer Brennkammern. CH701538B1 (de)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
CH701538A2 CH701538A2 (de) 2011-01-31
CH701538A8 true CH701538A8 (de) 2011-06-30
CH701538B1 CH701538B1 (de) 2015-02-27

Family

ID=43384155

Family Applications (1)

Application Number Title Priority Date Filing Date
CH01146/10A CH701538B1 (de) 2009-07-20 2010-07-14 Verfahren zum Abdichten mehrerer Brennkammern.

Country Status (5)

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

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
EP3189215B1 (de) * 2014-09-05 2021-04-28 Siemens Energy Global GmbH & Co. KG Dichtungsanordnung am übergang zu einer turbine
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
US10830069B2 (en) 2016-09-26 2020-11-10 General Electric Company Pressure-loaded seals
US10690059B2 (en) 2016-09-26 2020-06-23 General Electric Company Advanced seals with reduced corner leakage
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
US7788932B2 (en) * 2005-08-23 2010-09-07 Mitsubishi Heavy Industries, Ltd. Seal structure for gas turbine combustor
US20070134087A1 (en) * 2005-12-08 2007-06-14 General Electric Company Methods and apparatus for assembling turbine engines

Also Published As

Publication number Publication date
US8141879B2 (en) 2012-03-27
JP5743442B2 (ja) 2015-07-01
CH701538B1 (de) 2015-02-27
JP2011021601A (ja) 2011-02-03
CH701538A2 (de) 2011-01-31
CN101956608A (zh) 2011-01-26
DE102010036347A1 (de) 2011-01-27
DE102010036347B4 (de) 2021-09-30
US20110014029A1 (en) 2011-01-20

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Free format text: ERFINDER BERICHTIGT.

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Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH

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