JP2001271607A5 - - Google Patents
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- Publication number
- JP2001271607A5 JP2001271607A5 JP2001065848A JP2001065848A JP2001271607A5 JP 2001271607 A5 JP2001271607 A5 JP 2001271607A5 JP 2001065848 A JP2001065848 A JP 2001065848A JP 2001065848 A JP2001065848 A JP 2001065848A JP 2001271607 A5 JP2001271607 A5 JP 2001271607A5
- Authority
- JP
- Japan
- 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 |
|---|---|---|---|
| US09/522564 | 2000-03-10 | ||
| US09/522,564 US6341938B1 (en) | 2000-03-10 | 2000-03-10 | Methods and apparatus for minimizing thermal gradients within turbine shrouds |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2001271607A JP2001271607A (ja) | 2001-10-05 |
| JP2001271607A5 true JP2001271607A5 (enExample) | 2008-04-24 |
| JP4671516B2 JP4671516B2 (ja) | 2011-04-20 |
Family
ID=24081372
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001065848A Expired - Fee Related JP4671516B2 (ja) | 2000-03-10 | 2001-03-09 | タービン・シュラウド内の温度勾配を最小にする方法と装置 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6341938B1 (enExample) |
| EP (1) | EP1132576B1 (enExample) |
| JP (1) | JP4671516B2 (enExample) |
| DE (1) | DE60118300T2 (enExample) |
Families Citing this family (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6467339B1 (en) * | 2000-07-13 | 2002-10-22 | United Technologies Corporation | Method for deploying shroud segments in a turbine engine |
| FR2835563B1 (fr) * | 2002-02-07 | 2004-04-02 | Snecma Moteurs | Agencement d'accrochage de secteurs en arc de cercle de distributeur porteur d'aubes |
| JP4269829B2 (ja) | 2003-07-04 | 2009-05-27 | 株式会社Ｉｈｉ | シュラウドセグメント |
| WO2005003518A1 (en) * | 2003-07-04 | 2005-01-13 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine shroud segment |
| WO2005003519A1 (en) * | 2003-07-04 | 2005-01-13 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Turbine shroud segment |
| JP4285134B2 (ja) * | 2003-07-04 | 2009-06-24 | 株式会社Ｉｈｉ | シュラウドセグメント |
| US7255929B2 (en) * | 2003-12-12 | 2007-08-14 | General Electric Company | Use of spray coatings to achieve non-uniform seal clearances in turbomachinery |
| US8074998B2 (en) * | 2006-05-05 | 2011-12-13 | The Texas A&M University System | Annular seals for non-contact sealing of fluids in turbomachinery |
| US8608424B2 (en) * | 2009-10-09 | 2013-12-17 | General Electric Company | Contoured honeycomb seal for a turbomachine |
| US9080459B2 (en) * | 2012-01-03 | 2015-07-14 | General Electric Company | Forward step honeycomb seal for turbine shroud |
| US9097136B2 (en) * | 2012-01-03 | 2015-08-04 | General Electric Company | Contoured honeycomb seal for turbine shroud |
| US9238977B2 (en) * | 2012-11-21 | 2016-01-19 | General Electric Company | Turbine shroud mounting and sealing arrangement |
| US20140271142A1 (en) | 2013-03-14 | 2014-09-18 | General Electric Company | Turbine Shroud with Spline Seal |
| FR3025124B1 (fr) * | 2014-08-28 | 2016-09-30 | Snecma | Procede de fabrication de supports d'anneaux d'organe de turbomachine |
| EP3375980B1 (de) * | 2017-03-13 | 2019-12-11 | MTU Aero Engines GmbH | Dichtungsträger für eine strömungsmaschine |
| JP6864510B2 (ja) * | 2017-03-17 | 2021-04-28 | 三菱重工航空エンジン株式会社 | シール支持リングおよびシール構造 |
| US10774670B2 (en) * | 2017-06-07 | 2020-09-15 | General Electric Company | Filled abradable seal component and associated methods thereof |
| US10753222B2 (en) | 2017-09-11 | 2020-08-25 | Raytheon Technologies Corporation | Gas turbine engine blade outer air seal |
| FR3071273B1 (fr) * | 2017-09-21 | 2019-08-30 | Safran Aircraft Engines | Ensemble d'etancheite de turbine pour turbomachine |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3907455A (en) * | 1974-02-07 | 1975-09-23 | United Technologies Corp | Intermediate compressor case for gas turbine engines |
| GB1485032A (en) * | 1974-08-23 | 1977-09-08 | Rolls Royce | Gas turbine engine casing |
| US4371311A (en) * | 1980-04-28 | 1983-02-01 | United Technologies Corporation | Compression section for an axial flow rotary machine |
| JPS63154805A (ja) * | 1986-12-17 | 1988-06-28 | Mitsubishi Heavy Ind Ltd | ガスタ−ビン翼先端すき間の自動最適化機構 |
| US5314304A (en) * | 1991-08-15 | 1994-05-24 | The United States Of America As Represented By The Secretary Of The Air Force | Abradeable labyrinth stator seal |
| US5188507A (en) * | 1991-11-27 | 1993-02-23 | General Electric Company | Low-pressure turbine shroud |
| US5201846A (en) * | 1991-11-29 | 1993-04-13 | General Electric Company | Low-pressure turbine heat shield |
| GB2310255B (en) * | 1996-02-13 | 1999-06-16 | Rolls Royce Plc | A turbomachine |
| US5749701A (en) * | 1996-10-28 | 1998-05-12 | General Electric Company | Interstage seal assembly for a turbine |
| US6120242A (en) * | 1998-11-13 | 2000-09-19 | General Electric Company | Blade containing turbine shroud |
-
2000
- 2000-03-10 US US09/522,564 patent/US6341938B1/en not_active Expired - Lifetime
-
2001
- 2001-03-09 DE DE60118300T patent/DE60118300T2/de not_active Expired - Lifetime
- 2001-03-09 JP JP2001065848A patent/JP4671516B2/ja not_active Expired - Fee Related
- 2001-03-09 EP EP01302177A patent/EP1132576B1/en not_active Expired - Lifetime