JP2002333067A5 - - Google Patents
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- Publication number
- JP2002333067A5 JP2002333067A5 JP2001390757A JP2001390757A JP2002333067A5 JP 2002333067 A5 JP2002333067 A5 JP 2002333067A5 JP 2001390757 A JP2001390757 A JP 2001390757A JP 2001390757 A JP2001390757 A JP 2001390757A JP 2002333067 A5 JP2002333067 A5 JP 2002333067A5
- Authority
- JP
- Japan
- Prior art keywords
- labyrinth seals
- seals
- rotating
- labyrinth
- proven
- 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
- 230000002950 deficient Effects 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 230000003534 oscillatory effect Effects 0.000 description 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/745841 | 2000-12-26 | ||
| US09/745,841 US6502825B2 (en) | 2000-12-26 | 2000-12-26 | Pressure activated cloth seal |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2002333067A JP2002333067A (ja) | 2002-11-22 |
| JP2002333067A5 true JP2002333067A5 (enExample) | 2005-05-26 |
| JP4405121B2 JP4405121B2 (ja) | 2010-01-27 |
Family
ID=24998467
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001390757A Expired - Fee Related JP4405121B2 (ja) | 2000-12-26 | 2001-12-25 | 圧力作動クロスシール組立体および装置 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6502825B2 (enExample) |
| EP (1) | EP1219872B1 (enExample) |
| JP (1) | JP4405121B2 (enExample) |
| KR (1) | KR100779292B1 (enExample) |
| DE (1) | DE60134209D1 (enExample) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0127643D0 (en) * | 2001-11-17 | 2002-01-09 | Cross Mfg 1938 Company Ltd | A brush seal element |
| JP3795036B2 (ja) * | 2003-03-14 | 2006-07-12 | 三菱重工業株式会社 | タービン尾筒のシール構造およびシール装置 |
| US6923002B2 (en) * | 2003-08-28 | 2005-08-02 | General Electric Company | Combustion liner cap assembly for combustion dynamics reduction |
| FR2860264B1 (fr) * | 2003-09-30 | 2006-02-10 | Snecma Moteurs | Turbomachine comprenant deux elements mis en communication avec interposition d'un joint |
| US7152864B2 (en) * | 2003-10-02 | 2006-12-26 | Alstom Technology Ltd. | Seal assembly |
| JP2005337122A (ja) * | 2004-05-27 | 2005-12-08 | Ishikawajima Harima Heavy Ind Co Ltd | ガスシール装置 |
| US7052234B2 (en) * | 2004-06-23 | 2006-05-30 | General Electric Company | Turbine vane collar seal |
| US7600970B2 (en) * | 2005-12-08 | 2009-10-13 | General Electric Company | Ceramic matrix composite vane seals |
| US7565729B2 (en) | 2006-03-17 | 2009-07-28 | General Electric Company | Methods of manufacturing a segmented brush seal for sealing between stationary and rotary components |
| US8528339B2 (en) | 2007-04-05 | 2013-09-10 | Siemens Energy, Inc. | Stacked laminate gas turbine component |
| US8974891B2 (en) | 2007-10-26 | 2015-03-10 | Coi Ceramics, Inc. | Thermal protection systems comprising flexible regions of inter-bonded lamina of ceramic matrix composite material and methods of forming the same |
| US8491259B2 (en) * | 2009-08-26 | 2013-07-23 | Siemens Energy, Inc. | Seal system between transition duct exit section and turbine inlet in a gas turbine engine |
| US8511972B2 (en) * | 2009-12-16 | 2013-08-20 | Siemens Energy, Inc. | Seal member for use in a seal system between a transition duct exit section and a turbine inlet in a gas turbine engine |
| US8613451B2 (en) | 2010-11-29 | 2013-12-24 | General Electric Company | Cloth seal for turbo-machinery |
| US8678754B2 (en) | 2011-01-24 | 2014-03-25 | General Electric Company | Assembly for preventing fluid flow |
| US9353635B2 (en) | 2011-08-16 | 2016-05-31 | General Electric Company | Seal end attachment |
| US9938844B2 (en) * | 2011-10-26 | 2018-04-10 | General Electric Company | Metallic stator seal |
| US9188228B2 (en) | 2011-10-26 | 2015-11-17 | General Electric Company | Layered seal for turbomachinery |
| US10161523B2 (en) | 2011-12-23 | 2018-12-25 | General Electric Company | Enhanced cloth seal |
| US9835090B2 (en) * | 2012-09-18 | 2017-12-05 | United Technologies Corporation | Fire seal for a gas turbine engine |
| US10047622B2 (en) * | 2014-07-22 | 2018-08-14 | General Electric Company | Flexible layered seal for turbomachinery |
| US10400896B2 (en) * | 2014-08-28 | 2019-09-03 | United Technologies Corporation | Dual-ended brush seal assembly and method of manufacture |
| US10370994B2 (en) | 2015-05-28 | 2019-08-06 | Rolls-Royce North American Technologies Inc. | Pressure activated seals for a gas turbine engine |
| EP3306199B1 (en) * | 2016-10-06 | 2020-12-30 | Ansaldo Energia Switzerland AG | Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4453723A (en) * | 1980-12-02 | 1984-06-12 | General Connectors Corp. | Seal |
| US4645217A (en) * | 1985-11-29 | 1987-02-24 | United Technologies Corporation | Finger seal assembly |
| US5104286A (en) | 1991-02-08 | 1992-04-14 | Westinghouse Electric Corp. | Recirculation seal for a gas turbine exhaust diffuser |
| DE4109637C1 (enExample) | 1991-03-23 | 1992-05-14 | Metallgesellschaft Ag, 6000 Frankfurt, De | |
| US5400586A (en) | 1992-07-28 | 1995-03-28 | General Electric Co. | Self-accommodating brush seal for gas turbine combustor |
| US5265412A (en) | 1992-07-28 | 1993-11-30 | General Electric Company | Self-accommodating brush seal for gas turbine combustor |
| US5474306A (en) | 1992-11-19 | 1995-12-12 | General Electric Co. | Woven seal and hybrid cloth-brush seals for turbine applications |
| US5657998A (en) | 1994-09-19 | 1997-08-19 | General Electric Company | Gas-path leakage seal for a gas turbine |
| US5586773A (en) | 1995-06-19 | 1996-12-24 | General Electric Company | Gas-path leakage seal for a gas turbine made from metallic mesh |
| US5509669A (en) | 1995-06-19 | 1996-04-23 | General Electric Company | Gas-path leakage seal for a gas turbine |
| DE19618475B4 (de) * | 1996-05-08 | 2005-10-20 | Mtu Aero Engines Gmbh | Bürstendichtung |
| US5934687A (en) | 1997-07-07 | 1999-08-10 | General Electric Company | Gas-path leakage seal for a turbine |
| US5915697A (en) * | 1997-09-22 | 1999-06-29 | General Electric Company | Flexible cloth seal assembly |
| US6162014A (en) | 1998-09-22 | 2000-12-19 | General Electric Company | Turbine spline seal and turbine assembly containing such spline seal |
-
2000
- 2000-12-26 US US09/745,841 patent/US6502825B2/en not_active Expired - Lifetime
-
2001
- 2001-12-19 EP EP01310647A patent/EP1219872B1/en not_active Expired - Lifetime
- 2001-12-19 DE DE60134209T patent/DE60134209D1/de not_active Expired - Lifetime
- 2001-12-24 KR KR1020010084378A patent/KR100779292B1/ko not_active Expired - Fee Related
- 2001-12-25 JP JP2001390757A patent/JP4405121B2/ja not_active Expired - Fee Related
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