FR3039203B1 - Ensemble de disque de rotor de turbomachine comportant au moins un palier a roulement integre - Google Patents
Ensemble de disque de rotor de turbomachine comportant au moins un palier a roulement integre Download PDFInfo
- Publication number
- FR3039203B1 FR3039203B1 FR1556875A FR1556875A FR3039203B1 FR 3039203 B1 FR3039203 B1 FR 3039203B1 FR 1556875 A FR1556875 A FR 1556875A FR 1556875 A FR1556875 A FR 1556875A FR 3039203 B1 FR3039203 B1 FR 3039203B1
- Authority
- FR
- France
- Prior art keywords
- rotor disc
- rolling bearing
- disc assembly
- integrated
- turbomachine
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
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- 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
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/056—Bearings
- F04D29/059—Roller bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
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- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
L'objet principal de l'invention est un ensemble (E) de disque de rotor (1) de turbomachine, comportant un disque de rotor (1), destiné à porter des aubes (3) d'un module de compression de turbomachine, et au moins un palier à roulement (2) pour le guidage en rotation du module de compression, intégré au disque de rotor (1), ledit au moins un palier (2) comprenant une bague intérieure (2i), destinée à être portée par un arbre de stator (ST) de la turbomachine, et une bague extérieure (2e) intégrée au disque de rotor (1), ledit au moins un palier (2) étant ainsi intégré au disque de rotor (1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1556875A FR3039203B1 (fr) | 2015-07-21 | 2015-07-21 | Ensemble de disque de rotor de turbomachine comportant au moins un palier a roulement integre |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1556875A FR3039203B1 (fr) | 2015-07-21 | 2015-07-21 | Ensemble de disque de rotor de turbomachine comportant au moins un palier a roulement integre |
FR1556875 | 2015-07-21 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3039203A1 FR3039203A1 (fr) | 2017-01-27 |
FR3039203B1 true FR3039203B1 (fr) | 2020-02-14 |
Family
ID=54608690
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1556875A Active FR3039203B1 (fr) | 2015-07-21 | 2015-07-21 | Ensemble de disque de rotor de turbomachine comportant au moins un palier a roulement integre |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3039203B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3095481B1 (fr) * | 2019-04-25 | 2021-05-21 | Safran Aircraft Engines | Roulement à double rangée de billes à contact oblique comprenant un moyen de rétention axiale de secours intégré au roulement |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB808410A (en) * | 1954-07-16 | 1959-02-04 | Rolls Royce | Improvements in or relating to bearing arrangements for gas turbine engines |
US5433584A (en) * | 1994-05-05 | 1995-07-18 | Pratt & Whitney Canada, Inc. | Bearing support housing |
-
2015
- 2015-07-21 FR FR1556875A patent/FR3039203B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3039203A1 (fr) | 2017-01-27 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20170127 |
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Year of fee payment: 3 |
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Year of fee payment: 4 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
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PLFP | Fee payment |
Year of fee payment: 9 |