JP2013194737A5 - - Google Patents
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- Publication number
- JP2013194737A5 JP2013194737A5 JP2013054483A JP2013054483A JP2013194737A5 JP 2013194737 A5 JP2013194737 A5 JP 2013194737A5 JP 2013054483 A JP2013054483 A JP 2013054483A JP 2013054483 A JP2013054483 A JP 2013054483A JP 2013194737 A5 JP2013194737 A5 JP 2013194737A5
- Authority
- JP
- Japan
- Prior art keywords
- thermal
- recess
- casing
- flange
- annular
- 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 |
|---|---|---|---|
| US13/425,029 US9121301B2 (en) | 2012-03-20 | 2012-03-20 | Thermal isolation apparatus |
| US13/425,029 | 2012-03-20 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2013194737A JP2013194737A (ja) | 2013-09-30 |
| JP2013194737A5 true JP2013194737A5 (enExample) | 2016-04-28 |
| JP6087182B2 JP6087182B2 (ja) | 2017-03-01 |
Family
ID=47915444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013054483A Expired - Fee Related JP6087182B2 (ja) | 2012-03-20 | 2013-03-18 | 熱分離装置 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9121301B2 (enExample) |
| EP (1) | EP2642082B1 (enExample) |
| JP (1) | JP6087182B2 (enExample) |
| CN (1) | CN103321692B (enExample) |
| RU (1) | RU2013112114A (enExample) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9757936B2 (en) * | 2014-12-29 | 2017-09-12 | General Electric Company | Hot gas path component |
| US10309257B2 (en) * | 2015-03-02 | 2019-06-04 | Rolls-Royce North American Technologies Inc. | Turbine assembly with load pads |
| US10612408B2 (en) * | 2015-05-06 | 2020-04-07 | United Technologies Corporation | Control rings |
| US11441449B2 (en) * | 2017-05-11 | 2022-09-13 | Mitsubishi Heavy Industries, Ltd. | Heat retention device for turbine casing, securing tool for securing heat retention block for turbine casing, and method for securing heat retention block for turbine casing |
| US10711637B2 (en) * | 2017-06-15 | 2020-07-14 | General Electric Company | Turbine component assembly |
| US10822981B2 (en) | 2017-10-30 | 2020-11-03 | General Electric Company | Variable guide vane sealing |
| US10815821B2 (en) | 2018-08-31 | 2020-10-27 | General Electric Company | Variable airfoil with sealed flowpath |
| US11686210B2 (en) | 2021-03-24 | 2023-06-27 | General Electric Company | Component assembly for variable airfoil systems |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3910716A (en) * | 1974-05-23 | 1975-10-07 | Westinghouse Electric Corp | Gas turbine inlet vane structure utilizing a stable ceramic spherical interface arrangement |
| GB2397102B (en) * | 1981-12-30 | 2004-11-03 | Rolls Royce | Turbine shroud assembly |
| US4648792A (en) * | 1985-04-30 | 1987-03-10 | United Technologies Corporation | Stator vane support assembly |
| JPH08165902A (ja) * | 1994-10-12 | 1996-06-25 | Hitachi Ltd | セラミック静翼 |
| US5562408A (en) | 1995-06-06 | 1996-10-08 | General Electric Company | Isolated turbine shroud |
| JPH10331602A (ja) * | 1997-05-29 | 1998-12-15 | Toshiba Corp | ガスタービン |
| US6120242A (en) * | 1998-11-13 | 2000-09-19 | General Electric Company | Blade containing turbine shroud |
| EP1448874B1 (de) * | 2001-09-25 | 2007-12-26 | ALSTOM Technology Ltd | Dichtungsanordnung zur dichtspaltreduzierung innerhalb einer strömungsrotationsmaschine |
| JP2004036443A (ja) * | 2002-07-02 | 2004-02-05 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービンシュラウド構造 |
| US7195452B2 (en) | 2004-09-27 | 2007-03-27 | Honeywell International, Inc. | Compliant mounting system for turbine shrouds |
| US7238002B2 (en) * | 2005-11-03 | 2007-07-03 | General Electric Company | Damper seal system and method |
| US20070237629A1 (en) * | 2006-04-05 | 2007-10-11 | General Electric Company | Gas turbine compressor casing flowpath rings |
| FR2906295B1 (fr) | 2006-09-22 | 2011-11-18 | Snecma | Dispositif de toles isolantes sur carter pour amelioration du jeu en sommet d'aube |
| DE102007031711A1 (de) | 2007-07-06 | 2009-01-08 | Rolls-Royce Deutschland Ltd & Co Kg | Gehäusedeckbandsegment-Aufhängung |
| US8313288B2 (en) * | 2007-09-06 | 2012-11-20 | United Technologies Corporation | Mechanical attachment of ceramic or metallic foam materials |
| FR2923528B1 (fr) * | 2007-11-13 | 2009-12-11 | Snecma | Etage de turbine ou de compresseur d'un turboreacteur |
| DE102008007321A1 (de) | 2008-02-02 | 2009-08-13 | Mtu Aero Engines Gmbh | Vorrichtung mit Rotor, Gehäuse und Anstreifdichtung |
| US8052380B2 (en) | 2008-10-29 | 2011-11-08 | General Electric Company | Thermally-activated clearance reduction for a steam turbine |
| JP5490736B2 (ja) * | 2010-01-25 | 2014-05-14 | 株式会社日立製作所 | セラミックアブレーダブルコーテイングを有するガスタービン用シュラウド |
| JP5595241B2 (ja) * | 2010-11-18 | 2014-09-24 | 三菱重工業株式会社 | ガスタービン、分割セグメント、分割セグメントの形成方法 |
| CH705551A1 (de) | 2011-09-19 | 2013-03-28 | Alstom Technology Ltd | Selbstjustierende Einrichtung zum Steuern des Spielraums, insbesondere in radialer Richtung, zwischen rotierenden und stationären Komponenten einer thermisch belasteten Turbomaschine. |
-
2012
- 2012-03-20 US US13/425,029 patent/US9121301B2/en active Active
-
2013
- 2013-03-13 EP EP20130159007 patent/EP2642082B1/en active Active
- 2013-03-18 JP JP2013054483A patent/JP6087182B2/ja not_active Expired - Fee Related
- 2013-03-19 RU RU2013112114/06A patent/RU2013112114A/ru not_active Application Discontinuation
- 2013-03-20 CN CN201310090600.7A patent/CN103321692B/zh not_active Expired - Fee Related
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