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
- Authority
- 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
Links
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)
| 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)
| 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 |
-
2012
- 2012-03-28 US US13/432,259 patent/US8789833B2/en active Active
-
2013
- 2013-03-22 GB GB1305258.4A patent/GB2502416B/en not_active Expired - Fee Related
- 2013-03-25 JP JP2013061242A patent/JP6074301B2/ja not_active Expired - Fee Related
- 2013-03-26 DE DE102013103093A patent/DE102013103093A1/de not_active Withdrawn
- 2013-03-27 RU RU2013113675/06A patent/RU2013113675A/ru not_active Application Discontinuation
- 2013-03-28 CN CN201310104084.9A patent/CN103362567B/zh not_active Expired - Fee Related
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