FR3010154B1 - Panneau d'etancheite de carter intermediaire de turbomachine d'aeronef a double flux - Google Patents
Panneau d'etancheite de carter intermediaire de turbomachine d'aeronef a double fluxInfo
- Publication number
- FR3010154B1 FR3010154B1 FR1358491A FR1358491A FR3010154B1 FR 3010154 B1 FR3010154 B1 FR 3010154B1 FR 1358491 A FR1358491 A FR 1358491A FR 1358491 A FR1358491 A FR 1358491A FR 3010154 B1 FR3010154 B1 FR 3010154B1
- Authority
- FR
- France
- Prior art keywords
- double flow
- seal panel
- aircraft turbomachine
- flow aircraft
- intermediate caster
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
-
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/083—Sealings especially adapted for elastic fluid pumps
-
- 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 (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1358491A FR3010154B1 (fr) | 2013-09-05 | 2013-09-05 | Panneau d'etancheite de carter intermediaire de turbomachine d'aeronef a double flux |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1358491A FR3010154B1 (fr) | 2013-09-05 | 2013-09-05 | Panneau d'etancheite de carter intermediaire de turbomachine d'aeronef a double flux |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3010154A1 FR3010154A1 (fr) | 2015-03-06 |
FR3010154B1 true FR3010154B1 (fr) | 2015-10-02 |
Family
ID=49326774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1358491A Active FR3010154B1 (fr) | 2013-09-05 | 2013-09-05 | Panneau d'etancheite de carter intermediaire de turbomachine d'aeronef a double flux |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3010154B1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3039598B1 (fr) | 2015-07-29 | 2019-12-27 | Safran Aircraft Engines | Ensemble de redressement de flux d'air a performances aerodynamiques ameliorees |
FR3041700B1 (fr) * | 2015-09-25 | 2017-10-13 | Snecma | Agencement comprenant un tube a fluide se raccordant a un bras creux a haute temperature |
FR3051840B1 (fr) * | 2016-05-31 | 2020-01-10 | Safran Aircraft Engines | Carter intermediaire de turbomachine, equipee d'une piece d'etancheite a interface bras/virole |
FR3063117B1 (fr) | 2017-02-23 | 2021-07-02 | Safran Aircraft Engines | Raccordement entre une virole circulaire et un bras radial de structure d'une turbomachine, comprenant un joint d'etancheite et son support |
FR3133215B1 (fr) * | 2022-03-04 | 2024-02-02 | Safran Aircraft Engines | Carter intermédiaire de turbomachine comprenant un anneau ouvert d’étanchéité au feu, turbomachine et procédé d’assemblage correspondants |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2037901B (en) * | 1978-11-25 | 1982-07-28 | Rolls Royce | Nozzle guide vane assembly |
FR2610673B1 (fr) * | 1987-02-05 | 1991-03-15 | Snecma | Turboreacteur multiflux a couronne externe de redresseur de soufflante frettee sur le carter |
US7798768B2 (en) * | 2006-10-25 | 2010-09-21 | Siemens Energy, Inc. | Turbine vane ID support |
GB0905729D0 (en) * | 2009-04-03 | 2009-05-20 | Rolls Royce Plc | Stator vane assembly |
US9951639B2 (en) * | 2012-02-10 | 2018-04-24 | Pratt & Whitney Canada Corp. | Vane assemblies for gas turbine engines |
-
2013
- 2013-09-05 FR FR1358491A patent/FR3010154B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3010154A1 (fr) | 2015-03-06 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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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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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 |