KR100762535B1 - 터빈 - Google Patents
터빈 Download PDFInfo
- Publication number
- KR100762535B1 KR100762535B1 KR1020020084893A KR20020084893A KR100762535B1 KR 100762535 B1 KR100762535 B1 KR 100762535B1 KR 1020020084893 A KR1020020084893 A KR 1020020084893A KR 20020084893 A KR20020084893 A KR 20020084893A KR 100762535 B1 KR100762535 B1 KR 100762535B1
- Authority
- KR
- South Korea
- Prior art keywords
- turbine
- seal
- segment
- inner rail
- support ring
- 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.)
- Expired - Fee Related
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
- F16J15/0887—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing the sealing effect being obtained by elastic deformation of the packing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
- F16J15/0806—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment
- F16J15/0812—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment with a braided or knitted body
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/028,929 US6637752B2 (en) | 2001-12-28 | 2001-12-28 | Supplemental seal for the chordal hinge seal in a gas turbine |
| US10/028,929 | 2001-12-28 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| KR20030057422A KR20030057422A (ko) | 2003-07-04 |
| KR100762535B1 true KR100762535B1 (ko) | 2007-10-01 |
Family
ID=21846278
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR1020020084893A Expired - Fee Related KR100762535B1 (ko) | 2001-12-28 | 2002-12-27 | 터빈 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6637752B2 (enExample) |
| EP (1) | EP1323901B1 (enExample) |
| JP (1) | JP4315320B2 (enExample) |
| KR (1) | KR100762535B1 (enExample) |
| DE (1) | DE60212317T2 (enExample) |
Families Citing this family (39)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6648333B2 (en) | 2001-12-28 | 2003-11-18 | General Electric Company | Method of forming and installing a seal |
| US7094026B2 (en) * | 2004-04-29 | 2006-08-22 | General Electric Company | System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor |
| US7052234B2 (en) * | 2004-06-23 | 2006-05-30 | General Electric Company | Turbine vane collar seal |
| US7367567B2 (en) * | 2005-03-02 | 2008-05-06 | United Technologies Corporation | Low leakage finger seal |
| US7497443B1 (en) * | 2005-05-03 | 2009-03-03 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Resilient flexible pressure-activated seal |
| US20070149031A1 (en) * | 2005-12-22 | 2007-06-28 | United Technologies Corporation. | Reduced leakage finger seal |
| KR101124875B1 (ko) | 2006-04-26 | 2012-03-27 | 콸콤 인코포레이티드 | 펄스-간 듀티 사이클링 제어 장치 및 그 방법 |
| US7798768B2 (en) * | 2006-10-25 | 2010-09-21 | Siemens Energy, Inc. | Turbine vane ID support |
| JP5302979B2 (ja) * | 2008-02-27 | 2013-10-02 | ゼネラル・エレクトリック・カンパニイ | タービン・エンジン用高温シール |
| JP2009203841A (ja) * | 2008-02-27 | 2009-09-10 | Hitachi Ltd | ガスタービン,ガスタービンのシール装置及びガスタービンのシール方法 |
| US8413447B2 (en) * | 2009-09-16 | 2013-04-09 | General Electric Company | Fuel nozzle cup seal |
| US8231128B2 (en) * | 2010-04-01 | 2012-07-31 | General Electric Company | Integral seal and sealant packaging |
| US9206904B2 (en) * | 2010-07-08 | 2015-12-08 | Siemens Energy, Inc. | Seal including flexible seal strips |
| US20120119449A1 (en) * | 2010-11-11 | 2012-05-17 | General Electric Company | Transition Piece Sealing Assembly With Seal Overlay |
| 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 |
| US8985592B2 (en) * | 2011-02-07 | 2015-03-24 | Siemens Aktiengesellschaft | System for sealing a gap between a transition and a turbine |
| US20120211943A1 (en) * | 2011-02-22 | 2012-08-23 | General Electric Company | Sealing device and method for providing a seal in a turbine system |
| US8845272B2 (en) | 2011-02-25 | 2014-09-30 | General Electric Company | Turbine shroud and a method for manufacturing the turbine shroud |
| FR2973467B1 (fr) * | 2011-03-31 | 2014-01-24 | Aircelle Sa | Dispositif d'etancheite destine a etre dispose entre deux structures d'une nacelle |
| US8777202B2 (en) * | 2011-05-19 | 2014-07-15 | General Electric Company | Tool for adjusting seal |
| EP2525047A1 (de) * | 2011-05-20 | 2012-11-21 | Siemens Aktiengesellschaft | Dichtungsvorrichtung zum Abdichten zweier aneinander grenzender Räume |
| US8888445B2 (en) | 2011-08-19 | 2014-11-18 | General Electric Company | Turbomachine seal assembly |
| US9938844B2 (en) | 2011-10-26 | 2018-04-10 | General Electric Company | Metallic stator seal |
| US10161523B2 (en) | 2011-12-23 | 2018-12-25 | General Electric Company | Enhanced cloth seal |
| US9771818B2 (en) | 2012-12-29 | 2017-09-26 | United Technologies Corporation | Seals for a circumferential stop ring in a turbine exhaust case |
| US9562478B2 (en) * | 2012-12-29 | 2017-02-07 | United Technologies Corporation | Inter-module finger seal |
| US9759081B2 (en) | 2013-10-08 | 2017-09-12 | General Electric Company | Method and system to facilitate sealing in gas turbines |
| US9416675B2 (en) | 2014-01-27 | 2016-08-16 | General Electric Company | Sealing device for providing a seal in a turbomachine |
| US9879556B2 (en) | 2014-04-11 | 2018-01-30 | United Technologies Corporation | Cooled finger seal |
| EP2960439A1 (en) * | 2014-06-26 | 2015-12-30 | Siemens Aktiengesellschaft | Turbomachine with an outer sealing and use of the turbomachine |
| US9828868B2 (en) | 2014-09-11 | 2017-11-28 | United Technologies Corporation | Hinged seal using wire mesh |
| US10099290B2 (en) | 2014-12-18 | 2018-10-16 | General Electric Company | Hybrid additive manufacturing methods using hybrid additively manufactured features for hybrid components |
| US9863259B2 (en) | 2015-05-11 | 2018-01-09 | United Technologies Corporation | Chordal seal |
| US10519807B2 (en) | 2017-04-19 | 2019-12-31 | Rolls-Royce Corporation | Seal segment retention ring with chordal seal feature |
| US10655489B2 (en) | 2018-01-04 | 2020-05-19 | General Electric Company | Systems and methods for assembling flow path components |
| US11248705B2 (en) * | 2018-06-19 | 2022-02-15 | General Electric Company | Curved seal with relief cuts for adjacent gas turbine components |
| DE102022207874A1 (de) | 2022-07-29 | 2024-02-01 | Siemens Energy Global GmbH & Co. KG | Dichtsegment mit Lasche und Tasche |
| CN116412005A (zh) * | 2023-05-05 | 2023-07-11 | 无锡威孚高科技集团股份有限公司 | 一种用于涡轮增压器的接触式密封装置 |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4815933A (en) * | 1987-11-13 | 1989-03-28 | The United States Of America As Represented By The Secretary Of The Air Force | Nozzle flange attachment and sealing arrangement |
| US4883405A (en) * | 1987-11-13 | 1989-11-28 | The United States Of America As Represented By The Secretary Of The Air Force | Turbine nozzle mounting arrangement |
| EP0501700A1 (en) * | 1991-02-28 | 1992-09-02 | General Electric Company | Gas turbine vane assembly seal and support system |
| US5372476A (en) * | 1993-06-18 | 1994-12-13 | General Electric Company | Turbine nozzle support assembly |
| US5509669A (en) * | 1995-06-19 | 1996-04-23 | General Electric Company | Gas-path leakage seal for a gas turbine |
| EP0903519A1 (en) * | 1997-09-22 | 1999-03-24 | General Electric Company | Flexible cloth seal assembly |
| US6164656A (en) * | 1999-01-29 | 2000-12-26 | General Electric Company | Turbine nozzle interface seal and methods |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4314793A (en) * | 1978-12-20 | 1982-02-09 | United Technologies Corporation | Temperature actuated turbine seal |
| US4318668A (en) * | 1979-11-01 | 1982-03-09 | United Technologies Corporation | Seal means for a gas turbine engine |
| US4645217A (en) * | 1985-11-29 | 1987-02-24 | United Technologies Corporation | Finger seal assembly |
| US4863343A (en) * | 1988-05-16 | 1989-09-05 | Westinghouse Electric Corp. | Turbine vane shroud sealing system |
| 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 |
| US5653580A (en) * | 1995-03-06 | 1997-08-05 | Solar Turbines Incorporated | Nozzle and shroud assembly mounting structure |
| US5586773A (en) * | 1995-06-19 | 1996-12-24 | General Electric Company | Gas-path leakage seal for a gas turbine made from metallic mesh |
| US5839878A (en) * | 1996-09-30 | 1998-11-24 | United Technologies Corporation | Gas turbine stator vane |
| US5934687A (en) * | 1997-07-07 | 1999-08-10 | General Electric Company | Gas-path leakage seal for a turbine |
| US6162014A (en) * | 1998-09-22 | 2000-12-19 | General Electric Company | Turbine spline seal and turbine assembly containing such spline seal |
-
2001
- 2001-12-28 US US10/028,929 patent/US6637752B2/en not_active Expired - Fee Related
-
2002
- 2002-12-23 EP EP02258895A patent/EP1323901B1/en not_active Expired - Lifetime
- 2002-12-23 DE DE60212317T patent/DE60212317T2/de not_active Expired - Lifetime
- 2002-12-26 JP JP2002376195A patent/JP4315320B2/ja not_active Expired - Fee Related
- 2002-12-27 KR KR1020020084893A patent/KR100762535B1/ko not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4815933A (en) * | 1987-11-13 | 1989-03-28 | The United States Of America As Represented By The Secretary Of The Air Force | Nozzle flange attachment and sealing arrangement |
| US4883405A (en) * | 1987-11-13 | 1989-11-28 | The United States Of America As Represented By The Secretary Of The Air Force | Turbine nozzle mounting arrangement |
| EP0501700A1 (en) * | 1991-02-28 | 1992-09-02 | General Electric Company | Gas turbine vane assembly seal and support system |
| US5372476A (en) * | 1993-06-18 | 1994-12-13 | General Electric Company | Turbine nozzle support assembly |
| US5509669A (en) * | 1995-06-19 | 1996-04-23 | General Electric Company | Gas-path leakage seal for a gas turbine |
| EP0903519A1 (en) * | 1997-09-22 | 1999-03-24 | General Electric Company | Flexible cloth seal assembly |
| US6164656A (en) * | 1999-01-29 | 2000-12-26 | General Electric Company | Turbine nozzle interface seal and methods |
Also Published As
| Publication number | Publication date |
|---|---|
| DE60212317T2 (de) | 2007-05-24 |
| US20030122316A1 (en) | 2003-07-03 |
| JP4315320B2 (ja) | 2009-08-19 |
| US6637752B2 (en) | 2003-10-28 |
| EP1323901A3 (en) | 2004-03-31 |
| KR20030057422A (ko) | 2003-07-04 |
| JP2003227353A (ja) | 2003-08-15 |
| EP1323901A2 (en) | 2003-07-02 |
| DE60212317D1 (de) | 2006-07-27 |
| EP1323901B1 (en) | 2006-06-14 |
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St.27 status event code: A-0-1-A10-A12-nap-PA0109 |
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| P13-X000 | Application amended |
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| E701 | Decision to grant or registration of patent right | ||
| PE0701 | Decision of registration |
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| GRNT | Written decision to grant | ||
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