BE841997A - Dispositif d'etancheite entre des segments circulaires voisins - Google Patents
Dispositif d'etancheite entre des segments circulaires voisinsInfo
- Publication number
- BE841997A BE841997A BE167165A BE167165A BE841997A BE 841997 A BE841997 A BE 841997A BE 167165 A BE167165 A BE 167165A BE 167165 A BE167165 A BE 167165A BE 841997 A BE841997 A BE 841997A
- Authority
- BE
- Belgium
- Prior art keywords
- sealing device
- circular segments
- neighboring circular
- neighboring
- segments
- Prior art date
Links
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
- F01D11/005—Sealing means between non relatively rotating elements
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S277/00—Seal for a joint or juncture
- Y10S277/931—Seal including temperature responsive feature
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/617,072 US3970318A (en) | 1975-09-26 | 1975-09-26 | Sealing means for a segmented ring |
Publications (1)
Publication Number | Publication Date |
---|---|
BE841997A true BE841997A (fr) | 1976-09-16 |
Family
ID=24472129
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE167165A BE841997A (fr) | 1975-09-26 | 1976-05-19 | Dispositif d'etancheite entre des segments circulaires voisins |
Country Status (5)
Country | Link |
---|---|
US (1) | US3970318A (fr) |
BE (1) | BE841997A (fr) |
DE (1) | DE2620903A1 (fr) |
FR (1) | FR2325807A1 (fr) |
IT (1) | IT1060614B (fr) |
Families Citing this family (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4537024A (en) * | 1979-04-23 | 1985-08-27 | Solar Turbines, Incorporated | Turbine engines |
US4332523A (en) * | 1979-05-25 | 1982-06-01 | Teledyne Industries, Inc. | Turbine shroud assembly |
GB2078309B (en) * | 1980-05-31 | 1983-05-25 | Rolls Royce | Mounting nozzle guide vane assemblies |
GB2131895B (en) * | 1982-12-14 | 1986-04-23 | Rolls Royce | Improvements in or relating to seals |
US4492517A (en) * | 1983-01-06 | 1985-01-08 | General Electric Company | Segmented inlet nozzle for gas turbine, and methods of installation |
US4688988A (en) * | 1984-12-17 | 1987-08-25 | United Technologies Corporation | Coolable stator assembly for a gas turbine engine |
US4749333A (en) * | 1986-05-12 | 1988-06-07 | The United States Of America As Represented By The Secretary Of The Air Force | Vane platform sealing and retention means |
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 |
US5062767A (en) * | 1990-04-27 | 1991-11-05 | The United States Of America As Represented By The Secretary Of The Air Force | Segmented composite inner shrouds |
US5221096A (en) * | 1990-10-19 | 1993-06-22 | Allied-Signal Inc. | Stator and multiple piece seal |
US5088888A (en) * | 1990-12-03 | 1992-02-18 | General Electric Company | Shroud seal |
US5141395A (en) * | 1991-09-05 | 1992-08-25 | General Electric Company | Flow activated flowpath liner seal |
DE4215440A1 (de) * | 1992-05-11 | 1993-11-18 | Mtu Muenchen Gmbh | Einrichtung zur Bauteilabdichtung, insbesondere bei Turbomaschinen |
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 |
US5915697A (en) * | 1997-09-22 | 1999-06-29 | General Electric Company | Flexible cloth seal assembly |
JP3999395B2 (ja) * | 1999-03-03 | 2007-10-31 | 三菱重工業株式会社 | ガスタービン分割環 |
US6234750B1 (en) * | 1999-03-12 | 2001-05-22 | General Electric Company | Interlocked compressor stator |
US6290459B1 (en) * | 1999-11-01 | 2001-09-18 | General Electric Company | Stationary flowpath components for gas turbine engines |
US6425738B1 (en) * | 2000-05-11 | 2002-07-30 | General Electric Company | Accordion nozzle |
US6439844B1 (en) * | 2000-12-11 | 2002-08-27 | General Electric Company | Turbine bucket cover and brush seal |
US6910854B2 (en) | 2002-10-08 | 2005-06-28 | United Technologies Corporation | Leak resistant vane cluster |
US20050067788A1 (en) * | 2003-09-25 | 2005-03-31 | Siemens Westinghouse Power Corporation | Outer air seal assembly |
US7128522B2 (en) * | 2003-10-28 | 2006-10-31 | Pratt & Whitney Canada Corp. | Leakage control in a gas turbine engine |
GB2412702B (en) * | 2004-03-31 | 2006-05-03 | Rolls Royce Plc | Seal assembly |
US7329098B2 (en) * | 2005-05-06 | 2008-02-12 | Geenral Electric Company | Adjustable support bar with adjustable shim design for steam turbine diaphragms |
US7967555B2 (en) * | 2006-12-14 | 2011-06-28 | United Technologies Corporation | Process to cast seal slots in turbine vane shrouds |
FR2914350B1 (fr) * | 2007-03-30 | 2011-06-24 | Snecma | Enveloppe externe etanche pour une roue de turbine de turbomachine |
EP1995413B1 (fr) * | 2007-04-05 | 2010-04-28 | ALSTOM Technology Ltd | Joint d'étanchéité pour le jeu d'aubes d'une turbomachine |
US8092165B2 (en) * | 2008-01-21 | 2012-01-10 | Pratt & Whitney Canada Corp. | HP segment vanes |
US20110164965A1 (en) * | 2010-01-06 | 2011-07-07 | General Electric Company | Steam turbine stationary component seal |
US8821114B2 (en) | 2010-06-04 | 2014-09-02 | Siemens Energy, Inc. | Gas turbine engine sealing structure |
DE102010063594A1 (de) | 2010-12-20 | 2012-06-21 | Mtu Aero Engines Gmbh | Dichtanordnung und Turbomaschine mit einer derartigen Dichtanordnung |
JP6125329B2 (ja) * | 2013-05-27 | 2017-05-10 | 株式会社東芝 | 静止部シール構造 |
US10180082B2 (en) * | 2014-06-05 | 2019-01-15 | Rolls-Royce Corporation | Fan case |
JP6505860B2 (ja) * | 2016-03-15 | 2019-04-24 | 東芝エネルギーシステムズ株式会社 | タービン及びタービン静翼 |
GB201616197D0 (en) * | 2016-09-23 | 2016-11-09 | Rolls Royce Plc | Gas turbine engine |
DE102018210601A1 (de) * | 2018-06-28 | 2020-01-02 | MTU Aero Engines AG | Segmentring zur montage in einer strömungsmaschine |
US10927692B2 (en) | 2018-08-06 | 2021-02-23 | General Electric Company | Turbomachinery sealing apparatus and method |
US10907487B2 (en) | 2018-10-16 | 2021-02-02 | Honeywell International Inc. | Turbine shroud assemblies for gas turbine engines |
US11078802B2 (en) | 2019-05-10 | 2021-08-03 | Rolls-Royce Plc | Turbine engine assembly with ceramic matrix composite components and end face seals |
US11255208B2 (en) * | 2019-05-15 | 2022-02-22 | Raytheon Technologies Corporation | Feather seal for CMC BOAS |
FR3126442B1 (fr) * | 2021-08-25 | 2024-03-01 | Safran Aircraft Engines | Roue aubagée de stator de turbine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3690785A (en) * | 1970-12-17 | 1972-09-12 | Westinghouse Electric Corp | Spring plate sealing system |
US3752599A (en) * | 1971-03-29 | 1973-08-14 | Gen Electric | Bucket vibration damping device |
US3728041A (en) * | 1971-10-04 | 1973-04-17 | Gen Electric | Fluidic seal for segmented nozzle diaphragm |
US3752598A (en) * | 1971-11-17 | 1973-08-14 | United Aircraft Corp | Segmented duct seal |
-
1975
- 1975-09-26 US US05/617,072 patent/US3970318A/en not_active Expired - Lifetime
-
1976
- 1976-05-12 DE DE19762620903 patent/DE2620903A1/de active Pending
- 1976-05-13 IT IT23236/76A patent/IT1060614B/it active
- 1976-05-14 FR FR7614684A patent/FR2325807A1/fr not_active Withdrawn
- 1976-05-19 BE BE167165A patent/BE841997A/fr unknown
Also Published As
Publication number | Publication date |
---|---|
US3970318A (en) | 1976-07-20 |
FR2325807A1 (fr) | 1977-04-22 |
DE2620903A1 (de) | 1977-03-10 |
IT1060614B (it) | 1982-08-20 |
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