FR2987402B1 - Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire. - Google Patents
Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire.Info
- Publication number
- FR2987402B1 FR2987402B1 FR1251656A FR1251656A FR2987402B1 FR 2987402 B1 FR2987402 B1 FR 2987402B1 FR 1251656 A FR1251656 A FR 1251656A FR 1251656 A FR1251656 A FR 1251656A FR 2987402 B1 FR2987402 B1 FR 2987402B1
- Authority
- FR
- France
- Prior art keywords
- lubricating
- compatible
- modular assembly
- epicycloidal reducer
- epicycloidal
- 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
- 239000003638 chemical reducing agent Substances 0.000 title 1
- 230000001050 lubricating effect Effects 0.000 title 1
Classifications
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- 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
- F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
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- 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
- F01D25/18—Lubricating arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- 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
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- 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
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
-
- 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
- F05D2260/00—Function
- F05D2260/40—Transmission of power
- F05D2260/403—Transmission of power through the shape of the drive components
- F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
- F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
-
- 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
- F05D2260/00—Function
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/53—Kinematic linkage, i.e. transmission of position using gears
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Details Of Gearings (AREA)
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1251656A FR2987402B1 (fr) | 2012-02-23 | 2012-02-23 | Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire. |
EP13710502.9A EP2834503B1 (fr) | 2012-02-23 | 2013-02-22 | Dispositif de récupération de l'huile de lubrification d'un réducteur épicycloïdal |
RU2014136992A RU2627990C2 (ru) | 2012-02-23 | 2013-02-22 | Редуктор с эпициклоидной передачей, вентиляторный модуль двухконтурного турбореактивного двигателя и двухконтурный турбореактивный двигатель |
JP2014558185A JP6178344B2 (ja) | 2012-02-23 | 2013-02-22 | 減速歯車装置、ファンモジュールおよびバイパスターボジェットエンジン |
CN201380013395.2A CN104169546B (zh) | 2012-02-23 | 2013-02-22 | 用于从行星减速齿轮中回收润滑油的装置 |
BR112014020616-3A BR112014020616B1 (pt) | 2012-02-23 | 2013-02-22 | Redutor de trem epicicloidal, módulo de ventilador d e um turborreator de duplo fluxo e turborreator de duplo fluxo |
PCT/FR2013/050361 WO2013124590A1 (fr) | 2012-02-23 | 2013-02-22 | Dispositif de récupération de l'huile de lubrification d'un réducteur épicycloïdal |
CA2864975A CA2864975C (fr) | 2012-02-23 | 2013-02-22 | Dispositif de recuperation de l'huile de lubrification d'un reducteur epicycloidal |
US14/379,840 US9404420B2 (en) | 2012-02-23 | 2013-02-22 | Device for recovering lubricating oil from an epicyclic reduction gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1251656A FR2987402B1 (fr) | 2012-02-23 | 2012-02-23 | Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2987402A1 FR2987402A1 (fr) | 2013-08-30 |
FR2987402B1 true FR2987402B1 (fr) | 2015-02-27 |
Family
ID=45954956
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1251656A Active FR2987402B1 (fr) | 2012-02-23 | 2012-02-23 | Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2987402B1 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3018861B1 (fr) * | 2014-03-24 | 2016-04-08 | Snecma | Ensemble de transmission comprenant un organe de transmission et un systeme de distribution d'huile |
CA2889542A1 (fr) * | 2014-04-30 | 2015-10-30 | Ge Avio S.R.L. | Transmission epyciclique comportant un mecanisme de lubrification |
FR3052522B1 (fr) * | 2016-06-10 | 2018-06-01 | Safran Aircraft Engines | Dispositif de recuperation d'huile de lubrification ejectee par effet centrifuge dans une turbomachine |
FR3061242B1 (fr) | 2016-12-23 | 2019-05-17 | Safran Aircraft Engines | Turbomachine comportant un moyen de decouplage d'une soufflante |
FR3074552B1 (fr) | 2017-12-06 | 2019-11-22 | Safran Transmission Systems | Couronne de reducteur de vitesse a train planetaire de turbomachine |
FR3082553B1 (fr) * | 2018-06-18 | 2020-09-25 | Safran Aircraft Engines | Ensemble pour turbomachine d'aeronef comportant un systeme ameliore de lubrification d'un reducteur d'entrainement de soufflante en cas d'autorotation de la soufflante |
FR3086343B1 (fr) * | 2018-09-24 | 2020-09-04 | Safran Aircraft Engines | Turbomachine a reducteur pour un aeronef |
FR3086341B1 (fr) | 2018-09-24 | 2020-11-27 | Safran Aircraft Engines | Turbomachine a reducteur pour un aeronef |
FR3088683B1 (fr) | 2018-11-16 | 2022-12-23 | Safran Aircraft Engines | Ensemble pour turbomachine d'aeronef comportant un systeme a lubrifier ainsi qu'un dispositif ameliore d'injection de lubrifiant |
FR3108952B1 (fr) | 2020-04-02 | 2022-04-22 | Safran Aircraft Engines | Ensemble pour turbomachine d’aeronef comportant un systeme ameliore de lubrification d’un reducteur d’entrainement de soufflante |
FR3109801B1 (fr) | 2020-05-04 | 2022-04-01 | Safran Aircraft Engines | Agencement pour turbomachine d’aeronef a lubrification amelioree, l’agencement comprenant un arbre couple en rotation a un element suiveur, par des cannelures |
FR3117171B1 (fr) * | 2020-12-03 | 2022-10-21 | Safran | Systeme de transmission de puissance comportant une gouttiere de recuperation d’huile amelioree |
IT202200015483A1 (it) | 2022-07-22 | 2024-01-22 | Ge Avio Srl | Gruppo di trasmissione ad ingranaggi |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6223616B1 (en) * | 1999-12-22 | 2001-05-01 | United Technologies Corporation | Star gear system with lubrication circuit and lubrication method therefor |
US7591754B2 (en) * | 2006-03-22 | 2009-09-22 | United Technologies Corporation | Epicyclic gear train integral sun gear coupling design |
US7704178B2 (en) * | 2006-07-05 | 2010-04-27 | United Technologies Corporation | Oil baffle for gas turbine fan drive gear system |
US7926260B2 (en) * | 2006-07-05 | 2011-04-19 | United Technologies Corporation | Flexible shaft for gas turbine engine |
US8753243B2 (en) * | 2006-08-15 | 2014-06-17 | United Technologies Corporation | Ring gear mounting arrangement with oil scavenge scheme |
US8020665B2 (en) * | 2006-11-22 | 2011-09-20 | United Technologies Corporation | Lubrication system with extended emergency operability |
US8246503B2 (en) * | 2009-06-10 | 2012-08-21 | United Technologies Corporation | Epicyclic gear system with improved lubrication system |
US8333678B2 (en) * | 2009-06-26 | 2012-12-18 | United Technologies Corporation | Epicyclic gear system with load share reduction |
US8672801B2 (en) * | 2009-11-30 | 2014-03-18 | United Technologies Corporation | Mounting system for a planetary gear train in a gas turbine engine |
DE102010014968A1 (de) * | 2010-04-14 | 2011-10-20 | Mtu Aero Engines Gmbh | Mehrwelliges Triebwerk mit Tandem-Generator |
-
2012
- 2012-02-23 FR FR1251656A patent/FR2987402B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2987402A1 (fr) | 2013-08-30 |
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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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Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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Year of fee payment: 8 |
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Year of fee payment: 9 |
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Year of fee payment: 13 |