DE60017676D1 - Sicherungsvorrichtung für ein Turbinendeckband - Google Patents
Sicherungsvorrichtung für ein TurbinendeckbandInfo
- Publication number
- DE60017676D1 DE60017676D1 DE60017676T DE60017676T DE60017676D1 DE 60017676 D1 DE60017676 D1 DE 60017676D1 DE 60017676 T DE60017676 T DE 60017676T DE 60017676 T DE60017676 T DE 60017676T DE 60017676 D1 DE60017676 D1 DE 60017676D1
- Authority
- DE
- Germany
- Prior art keywords
- safety device
- turbine shroud
- shroud
- turbine
- safety
- 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 - Lifetime
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- 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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
-
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9914103A FR2800797B1 (fr) | 1999-11-10 | 1999-11-10 | Assemblage d'un anneau bordant une turbine a la structure de turbine |
FR9914103 | 1999-11-10 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60017676D1 true DE60017676D1 (de) | 2005-03-03 |
DE60017676T2 DE60017676T2 (de) | 2005-12-29 |
Family
ID=9551941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60017676T Expired - Lifetime DE60017676T2 (de) | 1999-11-10 | 2000-11-09 | Sicherungsvorrichtung für ein Turbinendeckband |
Country Status (11)
Country | Link |
---|---|
US (1) | US6575697B1 (de) |
EP (1) | EP1099826B1 (de) |
JP (1) | JP4181323B2 (de) |
KR (1) | KR100724779B1 (de) |
CA (1) | CA2359049C (de) |
DE (1) | DE60017676T2 (de) |
ES (1) | ES2232397T3 (de) |
FR (1) | FR2800797B1 (de) |
RU (1) | RU2256082C2 (de) |
UA (1) | UA67818C2 (de) |
WO (1) | WO2001034946A1 (de) |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2815668B1 (fr) * | 2000-10-19 | 2003-01-10 | Snecma Moteurs | Agencement de liaison d'un anneau de stator de turbine a une entretoise de support |
FR2816352B1 (fr) * | 2000-11-09 | 2003-01-31 | Snecma Moteurs | Ensemble de ventilation d'un anneau de stator |
FR2852053B1 (fr) | 2003-03-06 | 2007-12-28 | Snecma Moteurs | Turbine haute pression pour turbomachine |
US6997673B2 (en) * | 2003-12-11 | 2006-02-14 | Honeywell International, Inc. | Gas turbine high temperature turbine blade outer air seal assembly |
FR2869070B1 (fr) * | 2004-04-15 | 2008-10-17 | Snecma Moteurs Sa | Anneau de turbine |
DE102005013797A1 (de) | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
DE102005013796A1 (de) | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment |
DE102005013798A1 (de) * | 2005-03-24 | 2006-09-28 | Alstom Technology Ltd. | Wärmestausegment zum Abdichten eines Strömungskanals einer Strömungsrotationsmaschine |
FR2885168A1 (fr) * | 2005-04-27 | 2006-11-03 | Snecma Moteurs Sa | Dispositif d'etancheite pour une enceinte d'une turbomachine, et moteur d'aeronef equipe de celui-ci |
FR2887920B1 (fr) * | 2005-06-29 | 2010-09-10 | Snecma | Dispositif de fixation de secteurs d'anneau sur un carter de turbine |
US7600967B2 (en) * | 2005-07-30 | 2009-10-13 | United Technologies Corporation | Stator assembly, module and method for forming a rotary machine |
JP4786362B2 (ja) * | 2006-02-14 | 2011-10-05 | 三菱重工業株式会社 | ケーシングおよび流体機械 |
EP1939459B1 (de) * | 2006-12-27 | 2018-04-25 | Safran Aero Boosters SA | Flanschverbindung mit Klemmbacke, insbesondere für einen Axialverdichter |
FR2921410B1 (fr) | 2007-09-24 | 2010-03-12 | Snecma | Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des moyens permettant sa prehension |
FR2923527B1 (fr) * | 2007-11-13 | 2013-12-27 | Snecma | Etage de turbine ou de compresseur, en particulier de turbomachine |
FR2923528B1 (fr) * | 2007-11-13 | 2009-12-11 | Snecma | Etage de turbine ou de compresseur d'un turboreacteur |
FR2923526B1 (fr) * | 2007-11-13 | 2013-12-13 | Snecma | Etage de turbine ou de compresseur de turbomachine |
FR2931197B1 (fr) * | 2008-05-16 | 2010-06-18 | Snecma | Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages axiaux pour sa prehension |
FR2931196B1 (fr) * | 2008-05-16 | 2010-06-18 | Snecma | Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages radiaux permettant sa prehension |
FR2931195B1 (fr) * | 2008-05-16 | 2014-05-30 | Snecma | Organe dissymetrique de verrouillage de secteurs d'anneau sur un carter de turbomachine |
US8118548B2 (en) * | 2008-09-15 | 2012-02-21 | General Electric Company | Shroud for a turbomachine |
FR2941488B1 (fr) * | 2009-01-28 | 2011-09-16 | Snecma | Anneau de turbine a encoche anti-rotation |
FR2942844B1 (fr) * | 2009-03-09 | 2014-06-27 | Snecma | Ensemble d'anneau de turbine avec arret axial |
RU2522264C2 (ru) | 2009-03-09 | 2014-07-10 | Снекма | Сборка обоймы турбины |
FR2942845B1 (fr) * | 2009-03-09 | 2011-04-01 | Snecma | Ensemble d'anneau de turbine |
FR2952965B1 (fr) * | 2009-11-25 | 2012-03-09 | Snecma | Isolation d'un rebord circonferentiel d'un carter externe de turbomachine vis-a-vis d'un secteur d'anneau correspondant |
FR2955359B1 (fr) * | 2010-01-21 | 2013-07-19 | Snecma | Etancheite amont d'un anneau en cmc d'un etage de turbine |
FR2955898B1 (fr) * | 2010-02-02 | 2012-10-26 | Snecma | Etancheite amont d'un anneau en cmc dans une turbine de turbomachine |
FR2957093B1 (fr) * | 2010-03-02 | 2012-03-23 | Snecma | Preforme fibreuse pour un secteur d'anneau de turbine et son procede de fabrication. |
EP2800903B1 (de) | 2011-12-31 | 2018-12-05 | Rolls-Royce Corporation | Schaufelummantelungsvorrichtung und montageverfahren für eine schaufelummantelungsvorrichtung |
US20130272870A1 (en) * | 2012-04-17 | 2013-10-17 | General Electric Company | Mica-based seals for gas turbine shroud retaining clip |
CA2870765C (en) * | 2012-04-27 | 2017-03-28 | General Electric Company | System and method of limiting axial movement between a hanger and a fairing assembly in a turbine assembly |
EP2841716A1 (de) * | 2012-04-27 | 2015-03-04 | General Electric Company | Halteklammer, turbinenrahmen und verfahren zur begrenzung einer radialbewegung |
WO2013163505A1 (en) | 2012-04-27 | 2013-10-31 | General Electric Company | Shroud assembly and seal for a gas turbine engine |
ES2531468T3 (es) | 2012-10-12 | 2015-03-16 | Mtu Aero Engines Gmbh | Estructura de caja con obturación y refrigeración mejoradas |
FR3009739B1 (fr) * | 2013-08-13 | 2015-09-11 | Snecma | Amelioration pour le verrouillage de pieces de support d'aubage |
FR3009740B1 (fr) * | 2013-08-13 | 2017-12-15 | Snecma | Amelioration pour le verrouillage de pieces de support d'aubage |
EP2846001B1 (de) * | 2013-09-06 | 2023-01-11 | MTU Aero Engines AG | Montage- und Demontageverfahren eines Gasturbinenrotors und zugehörige Werkzeug |
US9828879B2 (en) * | 2015-05-11 | 2017-11-28 | General Electric Company | Shroud retention system with keyed retention clips |
US9932901B2 (en) | 2015-05-11 | 2018-04-03 | General Electric Company | Shroud retention system with retention springs |
FR3036433B1 (fr) * | 2015-05-22 | 2019-09-13 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien par crabotage |
FR3036436B1 (fr) * | 2015-05-22 | 2020-01-24 | Safran Ceramics | Ensemble d'anneau de turbine avec maintien par brides |
US10450895B2 (en) * | 2016-04-22 | 2019-10-22 | United Technologies Corporation | Stator arrangement |
US10697314B2 (en) | 2016-10-14 | 2020-06-30 | Rolls-Royce Corporation | Turbine shroud with I-beam construction |
FR3064022B1 (fr) * | 2017-03-16 | 2019-09-13 | Safran Aircraft Engines | Ensemble d'anneau de turbine |
RU2657404C1 (ru) * | 2017-06-16 | 2018-06-13 | Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Разъемный корпус турбомашины |
FR3070718B1 (fr) * | 2017-09-06 | 2019-08-23 | Safran Aircraft Engines | Ensemble de turbine a secteurs d'anneau |
US10557365B2 (en) | 2017-10-05 | 2020-02-11 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having reaction load distribution features |
DE102018210597A1 (de) * | 2018-06-28 | 2020-01-02 | MTU Aero Engines AG | Leitschaufelanordnung für eine strömungsmaschine |
US10934876B2 (en) * | 2018-07-18 | 2021-03-02 | Raytheon Technologies Corporation | Blade outer air seal AFT hook retainer |
US10634010B2 (en) | 2018-09-05 | 2020-04-28 | United Technologies Corporation | CMC BOAS axial retaining clip |
US11021987B2 (en) * | 2019-05-15 | 2021-06-01 | Raytheon Technologies Corporation | CMC BOAS arrangement |
US11149563B2 (en) | 2019-10-04 | 2021-10-19 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having axial reaction load distribution features |
US11933221B2 (en) | 2021-10-21 | 2024-03-19 | Rtx Corporation | Tongue joint including mating channel for cooling |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5197853A (en) | 1991-08-28 | 1993-03-30 | General Electric Company | Airtight shroud support rail and method for assembling in turbine engine |
US5320486A (en) * | 1993-01-21 | 1994-06-14 | General Electric Company | Apparatus for positioning compressor liner segments |
US5641267A (en) * | 1995-06-06 | 1997-06-24 | General Electric Company | Controlled leakage shroud panel |
US5609469A (en) * | 1995-11-22 | 1997-03-11 | United Technologies Corporation | Rotor assembly shroud |
US5669757A (en) * | 1995-11-30 | 1997-09-23 | General Electric Company | Turbine nozzle retainer assembly |
FR2780443B1 (fr) * | 1998-06-25 | 2000-08-04 | Snecma | Anneau de stator de turbine haute pression d'une turbomachine |
US6435820B1 (en) * | 1999-08-25 | 2002-08-20 | General Electric Company | Shroud assembly having C-clip retainer |
-
1999
- 1999-11-10 FR FR9914103A patent/FR2800797B1/fr not_active Expired - Fee Related
-
2000
- 2000-09-11 UA UA2001074775A patent/UA67818C2/uk unknown
- 2000-11-09 DE DE60017676T patent/DE60017676T2/de not_active Expired - Lifetime
- 2000-11-09 KR KR1020017008681A patent/KR100724779B1/ko not_active IP Right Cessation
- 2000-11-09 EP EP00403105A patent/EP1099826B1/de not_active Expired - Lifetime
- 2000-11-09 JP JP2001536854A patent/JP4181323B2/ja not_active Expired - Fee Related
- 2000-11-09 US US09/868,902 patent/US6575697B1/en not_active Expired - Lifetime
- 2000-11-09 CA CA002359049A patent/CA2359049C/fr not_active Expired - Fee Related
- 2000-11-09 WO PCT/FR2000/003126 patent/WO2001034946A1/fr active Application Filing
- 2000-11-09 ES ES00403105T patent/ES2232397T3/es not_active Expired - Lifetime
- 2000-11-09 RU RU2001122340/06A patent/RU2256082C2/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
FR2800797B1 (fr) | 2001-12-07 |
EP1099826B1 (de) | 2005-01-26 |
KR100724779B1 (ko) | 2007-06-04 |
ES2232397T3 (es) | 2005-06-01 |
UA67818C2 (uk) | 2004-07-15 |
US6575697B1 (en) | 2003-06-10 |
EP1099826A1 (de) | 2001-05-16 |
JP4181323B2 (ja) | 2008-11-12 |
DE60017676T2 (de) | 2005-12-29 |
FR2800797A1 (fr) | 2001-05-11 |
JP2003514182A (ja) | 2003-04-15 |
CA2359049C (fr) | 2009-01-13 |
CA2359049A1 (fr) | 2001-05-17 |
KR20010089800A (ko) | 2001-10-08 |
WO2001034946A1 (fr) | 2001-05-17 |
RU2256082C2 (ru) | 2005-07-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: SNECMA, PARIS, FR |