JP2013204592A5 - - Google Patents

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Publication number
JP2013204592A5
JP2013204592A5 JP2013061242A JP2013061242A JP2013204592A5 JP 2013204592 A5 JP2013204592 A5 JP 2013204592A5 JP 2013061242 A JP2013061242 A JP 2013061242A JP 2013061242 A JP2013061242 A JP 2013061242A JP 2013204592 A5 JP2013204592 A5 JP 2013204592A5
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JP
Japan
Prior art keywords
key
seal assembly
assembly
shaped
seal
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
JP2013061242A
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English (en)
Japanese (ja)
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JP2013204592A (ja
JP6074301B2 (ja
Filing date
Publication date
Priority claimed from US13/432,259 external-priority patent/US8789833B2/en
Application filed filed Critical
Publication of JP2013204592A publication Critical patent/JP2013204592A/ja
Publication of JP2013204592A5 publication Critical patent/JP2013204592A5/ja
Application granted granted Critical
Publication of JP6074301B2 publication Critical patent/JP6074301B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2013061242A 2012-03-28 2013-03-25 タービン組立体及びタービン組立方法 Expired - Fee Related JP6074301B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/432,259 2012-03-28
US13/432,259 US8789833B2 (en) 2012-03-28 2012-03-28 Turbine assembly and method for assembling a turbine

Publications (3)

Publication Number Publication Date
JP2013204592A JP2013204592A (ja) 2013-10-07
JP2013204592A5 true JP2013204592A5 (enExample) 2016-05-12
JP6074301B2 JP6074301B2 (ja) 2017-02-01

Family

ID=48226861

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013061242A Expired - Fee Related JP6074301B2 (ja) 2012-03-28 2013-03-25 タービン組立体及びタービン組立方法

Country Status (6)

Country Link
US (1) US8789833B2 (enExample)
JP (1) JP6074301B2 (enExample)
CN (1) CN103362567B (enExample)
DE (1) DE102013103093A1 (enExample)
GB (1) GB2502416B (enExample)
RU (1) RU2013113675A (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014133615A1 (en) * 2013-03-01 2014-09-04 Rolls-Royce Corporation Bi-metal strip-seal
EP2984291B8 (en) * 2013-04-11 2021-04-07 Raytheon Technologies Corporation Nozzle segment for a gas turbine engine
US9643733B2 (en) 2014-06-17 2017-05-09 The Boeing Company Fire seal for an aircraft
US10370994B2 (en) 2015-05-28 2019-08-06 Rolls-Royce North American Technologies Inc. Pressure activated seals for a gas turbine engine
CN104963886A (zh) * 2015-07-01 2015-10-07 南京航空航天大学 轴流压气机/风扇转静子径向间隙无泄漏封严结构及方法
CN106051156A (zh) * 2016-07-27 2016-10-26 苏州好特斯模具有限公司 热敏金属自动密封型热嘴
FR3107559A1 (fr) * 2020-02-24 2021-08-27 Airbus Operations Structure interne d’un conduit d’ejection primaire comportant un separateur dont la geometrie varie en fonction de la temperature
CN112253750A (zh) * 2020-10-21 2021-01-22 中国航发沈阳发动机研究所 一种柔性石墨编织密封条及其安装方法

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59116504U (ja) * 1983-01-28 1984-08-06 株式会社日立製作所 タ−ビンのインロ−構造
JPS6223503A (ja) * 1985-07-22 1987-01-31 Mitsubishi Heavy Ind Ltd タ−ボ機械の軸シ−ル装置
US4602795A (en) * 1985-12-06 1986-07-29 United Technologies Corporation Thermally expansive slip joint for formed sheet metal seals
JPH11257014A (ja) * 1998-03-06 1999-09-21 Toshiba Corp 軸流タービンの作動流体漏洩防止装置
US6193240B1 (en) * 1999-01-11 2001-02-27 General Electric Company Seal assembly
EP1177367B1 (de) * 1999-05-12 2003-08-20 Siemens Aktiengesellschaft Dichtung zur abdichtung eines spaltes, insbesondere in einer turbine, und turbine
EP1118806A1 (de) * 2000-01-20 2001-07-25 Siemens Aktiengesellschaft Thermisch belastbare Wand und Verfahren zur Abdichtung eines Spaltes in einer thermisch belasteten Wand
US6659472B2 (en) * 2001-12-28 2003-12-09 General Electric Company Seal for gas turbine nozzle and shroud interface
US6752592B2 (en) * 2001-12-28 2004-06-22 General Electric Company Supplemental seal for the chordal hinge seals in a gas turbine
US6648333B2 (en) * 2001-12-28 2003-11-18 General Electric Company Method of forming and installing a seal
US7121785B2 (en) 2004-07-02 2006-10-17 Siemens Power Generation, Inc. Retraction retainer system for biased turbine engine components
GB2417298B (en) * 2004-08-21 2008-12-24 Alstom Technology Ltd Sealing arrangement
EP1674771B1 (de) * 2004-12-23 2010-05-12 Siemens Aktiengesellschaft Anordnung zur Abdichtung eines Spaltes zwischen einem ersten Bauteil und einem zweiten Bauteil
GB2437298B (en) 2006-04-18 2008-10-01 Rolls Royce Plc A Seal Between Rotor Blade Platforms And Stator Vane Platforms, A Rotor Blade And A Stator Vane
US8210799B1 (en) 2008-03-31 2012-07-03 Florida Turbine Technologies, Inc. Bi-metallic strip seal for a turbine shroud
US8132442B2 (en) * 2008-09-22 2012-03-13 Siemens Energy, Inc. Compressible ceramic seal
JP5254774B2 (ja) * 2008-12-22 2013-08-07 三菱重工業株式会社 熱機関の流体シール構造
US8434999B2 (en) * 2010-03-25 2013-05-07 General Electric Company Bimetallic spline seal
US8366113B2 (en) * 2010-06-10 2013-02-05 Eaton Corporation Pre-compressed seal including removable pre-compression member

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