FR3132554B1 - Reducteur de vitesse pour une turbomachine d’aeronef - Google Patents
Reducteur de vitesse pour une turbomachine d’aeronef Download PDFInfo
- Publication number
- FR3132554B1 FR3132554B1 FR2201069A FR2201069A FR3132554B1 FR 3132554 B1 FR3132554 B1 FR 3132554B1 FR 2201069 A FR2201069 A FR 2201069A FR 2201069 A FR2201069 A FR 2201069A FR 3132554 B1 FR3132554 B1 FR 3132554B1
- Authority
- FR
- France
- Prior art keywords
- cage
- speed reducer
- solar
- aircraft turbomachine
- main axis
- 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 abstract 2
- 238000005452 bending Methods 0.000 abstract 1
Classifications
-
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/08—General details of gearing of gearings with members having orbital motion
- F16H57/082—Planet carriers
-
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H1/2809—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet-wheels
- F16H1/2827—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet-wheels by allowing limited movement of the planet carrier, e.g. relative to its shaft
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- 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
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/75—Shape given by its similarity to a letter, e.g. T-shaped
-
- 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
- F05D2260/98—Lubrication
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H2001/289—Toothed gearings for conveying rotary motion with gears having orbital motion comprising two or more coaxial and identical sets of orbital gears, e.g. for distributing torque between the coaxial sets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/04—Features relating to lubrication or cooling or heating
- F16H57/0467—Elements of gearings to be lubricated, cooled or heated
- F16H57/0479—Gears or bearings on planet carriers
-
- 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)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Retarders (AREA)
- General Details Of Gearings (AREA)
- Friction Gearing (AREA)
Abstract
Réducteur de vitesse (10) pour une turbomachine (1) d’aéronef, ce réducteur ayant un axe principal (X) et comportant : - un porte-satellites (13) comportant une cage (120) et un porte-cage (122), - un solaire (11) situé dans la cage (120) et centré sur l’axe principal (X), - une rangée annulaire de satellites (12) disposés autour de l’axe principal (X) et du solaire (11) et engrenés avec le solaire (11), - une couronne (14) disposée autour de l’axe (X) et de la cage (120) et engrenée avec les satellites (12), la cage (120) et le porte-cage (122) étant reliés entre eux par des liaisons dont la souplesse en flexion est optimisée. Figure pour l'abrégé : Figure 10
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2201069A FR3132554B1 (fr) | 2022-02-08 | 2022-02-08 | Reducteur de vitesse pour une turbomachine d’aeronef |
US18/165,173 US11933229B2 (en) | 2022-02-08 | 2023-02-06 | Speed reduction gear for an aircraft turbomachine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2201069 | 2022-02-08 | ||
FR2201069A FR3132554B1 (fr) | 2022-02-08 | 2022-02-08 | Reducteur de vitesse pour une turbomachine d’aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3132554A1 FR3132554A1 (fr) | 2023-08-11 |
FR3132554B1 true FR3132554B1 (fr) | 2024-03-22 |
Family
ID=81449199
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2201069A Active FR3132554B1 (fr) | 2022-02-08 | 2022-02-08 | Reducteur de vitesse pour une turbomachine d’aeronef |
Country Status (2)
Country | Link |
---|---|
US (1) | US11933229B2 (fr) |
FR (1) | FR3132554B1 (fr) |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1250861B (it) * | 1991-11-12 | 1995-04-21 | Fiat Avio Spa | Riduttore di velocita' epicicloidale atto ad essere inserito nella trasmissione tra una turbina a gas ed il compressore d'aria di un motore aeronautico. |
FR2853382B1 (fr) | 2003-04-04 | 2006-04-28 | Hispano Suiza Sa | Systeme de liaison souple entre un porte-satellites et le support fixe dans un reducteur de vitesse |
ITTO20111007A1 (it) * | 2011-11-03 | 2013-05-04 | Avio Spa | Rotismo epicicloidale |
FR2987416B1 (fr) | 2012-02-23 | 2015-09-04 | Snecma | Dispositif de lubrification d'un reducteur epicycloidal. |
CN204327938U (zh) * | 2014-11-28 | 2015-05-13 | 中航商用航空发动机有限责任公司 | 分体式行星架 |
FR3041054B1 (fr) | 2015-09-15 | 2017-09-15 | Hispano-Suiza | Dispositif d'alimentation en huile pour un reducteur a train epicycloidal. |
FR3052213B1 (fr) | 2016-06-07 | 2018-05-18 | Safran Transmission Systems | Procede d'assemblage d'un porte-satellites |
FR3073915B1 (fr) * | 2017-11-17 | 2019-10-25 | Safran Transmission Systems | Cage de reducteur de vitesse a train planetaire ou epicycloidal de turbomachine |
FR3076336B1 (fr) * | 2017-12-29 | 2020-09-04 | Safran Trans Systems | Porte-satellites pour un reducteur de vitesse a train epicycloidal |
FR3084428B1 (fr) * | 2018-07-26 | 2020-09-11 | Safran Trans Systems | Cage de reducteur de vitesse a train planetaire ou epicycloidal de turbomachine |
FR3092884B1 (fr) * | 2019-02-20 | 2022-12-16 | Safran Trans Systems | Ensemble a reducteur planetaire pour une turbomachine |
-
2022
- 2022-02-08 FR FR2201069A patent/FR3132554B1/fr active Active
-
2023
- 2023-02-06 US US18/165,173 patent/US11933229B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3132554A1 (fr) | 2023-08-11 |
US20230250761A1 (en) | 2023-08-10 |
US11933229B2 (en) | 2024-03-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20230811 |
|
PLFP | Fee payment |
Year of fee payment: 3 |