FR2961848B1 - Etage de turbine - Google Patents
Etage de turbineInfo
- Publication number
- FR2961848B1 FR2961848B1 FR1055204A FR1055204A FR2961848B1 FR 2961848 B1 FR2961848 B1 FR 2961848B1 FR 1055204 A FR1055204 A FR 1055204A FR 1055204 A FR1055204 A FR 1055204A FR 2961848 B1 FR2961848 B1 FR 2961848B1
- Authority
- FR
- France
- Prior art keywords
- turbine floor
- turbine
- floor
- 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.)
- Active
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
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1055204A FR2961848B1 (fr) | 2010-06-29 | 2010-06-29 | Etage de turbine |
US13/169,411 US8734100B2 (en) | 2010-06-29 | 2011-06-27 | Turbine stage |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1055204A FR2961848B1 (fr) | 2010-06-29 | 2010-06-29 | Etage de turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2961848A1 FR2961848A1 (fr) | 2011-12-30 |
FR2961848B1 true FR2961848B1 (fr) | 2012-07-13 |
Family
ID=43629366
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1055204A Active FR2961848B1 (fr) | 2010-06-29 | 2010-06-29 | Etage de turbine |
Country Status (2)
Country | Link |
---|---|
US (1) | US8734100B2 (fr) |
FR (1) | FR2961848B1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2989724B1 (fr) | 2012-04-20 | 2015-12-25 | Snecma | Etage de turbine pour une turbomachine |
FR3027342B1 (fr) * | 2014-10-20 | 2016-10-28 | Snecma | Anneau d'etancheite de turbomachine |
EP3153671A1 (fr) * | 2015-10-08 | 2017-04-12 | MTU Aero Engines GmbH | Dispositif de protection pour turbomachine |
FR3061741B1 (fr) * | 2017-01-09 | 2021-04-02 | Safran Aircraft Engines | Turbine pour turbomachine |
EP3412871B1 (fr) | 2017-06-09 | 2021-04-28 | Ge Avio S.r.l. | Joint pour aube directrice de turbine à gaz |
RU2674813C1 (ru) * | 2017-10-05 | 2018-12-13 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Статор газовой турбины |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5201846A (en) * | 1991-11-29 | 1993-04-13 | General Electric Company | Low-pressure turbine heat shield |
US5333995A (en) * | 1993-08-09 | 1994-08-02 | General Electric Company | Wear shim for a turbine engine |
EP0844369B1 (fr) * | 1996-11-23 | 2002-01-30 | ROLLS-ROYCE plc | Assemblage d'un rotor à aubes et de son carter |
US6120242A (en) * | 1998-11-13 | 2000-09-19 | General Electric Company | Blade containing turbine shroud |
GB2378730B (en) | 2001-08-18 | 2005-03-16 | Rolls Royce Plc | Cooled segments surrounding turbine blades |
WO2005003518A1 (fr) * | 2003-07-04 | 2005-01-13 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Segment d'anneau de cerclage de turbine |
FR2875534B1 (fr) | 2004-09-21 | 2006-12-22 | Snecma Moteurs Sa | Module de turbine pour moteur a turbine a gaz avec rotor comportant un corps monobloc |
FR2899273B1 (fr) * | 2006-03-30 | 2012-08-17 | Snecma | Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine |
FR2914350B1 (fr) * | 2007-03-30 | 2011-06-24 | Snecma | Enveloppe externe etanche pour une roue de turbine de turbomachine |
-
2010
- 2010-06-29 FR FR1055204A patent/FR2961848B1/fr active Active
-
2011
- 2011-06-27 US US13/169,411 patent/US8734100B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US8734100B2 (en) | 2014-05-27 |
US20110318170A1 (en) | 2011-12-29 |
FR2961848A1 (fr) | 2011-12-30 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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PLFP | Fee payment |
Year of fee payment: 14 |