JP2006177355A5 - - Google Patents

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Publication number
JP2006177355A5
JP2006177355A5 JP2005365711A JP2005365711A JP2006177355A5 JP 2006177355 A5 JP2006177355 A5 JP 2006177355A5 JP 2005365711 A JP2005365711 A JP 2005365711A JP 2005365711 A JP2005365711 A JP 2005365711A JP 2006177355 A5 JP2006177355 A5 JP 2006177355A5
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JP
Japan
Prior art keywords
seal
diaphragm
supported
holder
seal holder
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
JP2005365711A
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English (en)
Japanese (ja)
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JP4740730B2 (ja
JP2006177355A (ja
Filing date
Publication date
Priority claimed from US11/017,661 external-priority patent/US7287956B2/en
Application filed filed Critical
Publication of JP2006177355A publication Critical patent/JP2006177355A/ja
Publication of JP2006177355A5 publication Critical patent/JP2006177355A5/ja
Application granted granted Critical
Publication of JP4740730B2 publication Critical patent/JP4740730B2/ja
Anticipated expiration legal-status Critical
Active legal-status Critical Current

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JP2005365711A 2004-12-22 2005-12-20 タービン Active JP4740730B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/017,661 2004-12-22
US11/017,661 US7287956B2 (en) 2004-12-22 2004-12-22 Removable abradable seal carriers for sealing between rotary and stationary turbine components

Publications (3)

Publication Number Publication Date
JP2006177355A JP2006177355A (ja) 2006-07-06
JP2006177355A5 true JP2006177355A5 (enExample) 2009-02-12
JP4740730B2 JP4740730B2 (ja) 2011-08-03

Family

ID=36585717

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005365711A Active JP4740730B2 (ja) 2004-12-22 2005-12-20 タービン

Country Status (6)

Country Link
US (1) US7287956B2 (enExample)
JP (1) JP4740730B2 (enExample)
CN (1) CN1800589B (enExample)
FR (1) FR2879649B1 (enExample)
IT (1) ITMI20052424A1 (enExample)
RU (1) RU2392449C2 (enExample)

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RU2447294C2 (ru) * 2010-02-02 2012-04-10 Сергей Владимирович Ушинин Вставка сотового надбандажного уплотнения паровой турбины и способ установки вставок сотового надбандажного уплотнения
FR2961564B1 (fr) 2010-06-17 2016-03-04 Snecma Compresseur et turbomachine a rendement optimise
JP5087147B2 (ja) * 2011-01-13 2012-11-28 株式会社日立製作所 蒸気タービン
US20120195742A1 (en) * 2011-01-28 2012-08-02 Jain Sanjeev Kumar Turbine bucket for use in gas turbine engines and methods for fabricating the same
DE102012005771B4 (de) 2011-03-25 2022-06-30 General Electric Technology Gmbh Dichtvorrichtung für drehende Turbinenschaufeln
US9109458B2 (en) * 2011-11-11 2015-08-18 United Technologies Corporation Turbomachinery seal
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JP5518032B2 (ja) * 2011-12-13 2014-06-11 三菱重工業株式会社 タービン、及びシール構造
US9080459B2 (en) * 2012-01-03 2015-07-14 General Electric Company Forward step honeycomb seal for turbine shroud
JP5567077B2 (ja) * 2012-08-23 2014-08-06 三菱重工業株式会社 回転機械
US9726031B2 (en) * 2012-09-28 2017-08-08 United Technologies Corporation Piston ring coated carbon seal
JP5951449B2 (ja) * 2012-11-02 2016-07-13 株式会社東芝 蒸気タービン
CZ305014B6 (cs) * 2013-05-22 2015-03-25 Doosan Ĺ koda Power s.r.o. Uložení segmentového odtahovacího těsnění ve statoru turbíny
US20150040567A1 (en) * 2013-08-08 2015-02-12 General Electric Company Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine
US10119410B2 (en) 2013-10-03 2018-11-06 United Technologies Corporation Vane seal system having spring positively locating seal member in axial direction
EP3489465B1 (en) 2013-10-03 2023-05-17 Raytheon Technologies Corporation Seal for a vane seal system and method for managing damping in a vane seal system
US9394801B2 (en) 2013-10-07 2016-07-19 General Electric Company Adjustable turbine seal and method of assembling same
US9429041B2 (en) 2014-05-14 2016-08-30 General Electric Company Turbomachine component displacement apparatus and method of use
FR3047075B1 (fr) * 2016-01-27 2018-02-23 Safran Aircraft Engines Piece de revolution pour banc d'essai de turbine ou pour turbomachine, banc d'essais de turbines comprenant ladite piece, et procede les utilisant
WO2016179608A2 (en) * 2016-04-29 2016-11-10 Stein Seal Company Intershaft seal with asymmetric sealing ring
US10598035B2 (en) * 2016-05-27 2020-03-24 General Electric Company Intershaft sealing systems for gas turbine engines and methods for assembling the same
FR3058755B1 (fr) * 2016-11-15 2020-09-25 Safran Aircraft Engines Turbine pour turbomachine
FR3058756B1 (fr) 2016-11-15 2020-10-16 Safran Aircraft Engines Turbine pour turbomachine
FR3068070B1 (fr) * 2017-06-26 2019-07-19 Safran Aircraft Engines Turbine pour turbomachine
JP7051656B2 (ja) * 2018-09-28 2022-04-11 三菱重工コンプレッサ株式会社 タービンステータ、蒸気タービン、及び仕切板
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CN112610335B (zh) * 2020-12-21 2021-12-31 杭州汽轮动力集团有限公司 一种燃气轮机涡轮盘腔密封结构
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