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FR3086341B1 - Turbomachine a reducteur pour un aeronef - Google Patents

Turbomachine a reducteur pour un aeronef Download PDF

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Publication number
FR3086341B1
FR3086341B1 FR1858672A FR1858672A FR3086341B1 FR 3086341 B1 FR3086341 B1 FR 3086341B1 FR 1858672 A FR1858672 A FR 1858672A FR 1858672 A FR1858672 A FR 1858672A FR 3086341 B1 FR3086341 B1 FR 3086341B1
Authority
FR
France
Prior art keywords
shaft
turbomachine
support
downstream
pipe
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
Application number
FR1858672A
Other languages
English (en)
Other versions
FR3086341A1 (fr
Inventor
Julien Fabien Patrick Becoulet
Xavier Jean Yves Alain Agneray
Michel Gilbert Roland Brault
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1858672A priority Critical patent/FR3086341B1/fr
Priority to US16/580,823 priority patent/US11085329B2/en
Priority to GB1913713.2A priority patent/GB2578522B/en
Publication of FR3086341A1 publication Critical patent/FR3086341A1/fr
Application granted granted Critical
Publication of FR3086341B1 publication Critical patent/FR3086341B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D25/18—Lubricating arrangements
    • 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
    • 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
    • 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
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/042—Guidance of lubricant
    • F16H57/0421—Guidance of lubricant on or within the casing, e.g. shields or baffles for collecting lubricant, tubes, pipes, grooves, channels or the like
    • F16H57/0423—Lubricant guiding means mounted or supported on the casing, e.g. shields or baffles for collecting lubricant, tubes or pipes
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/53—Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece construction
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • 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
    • F05D2230/72—Maintenance
    • 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
    • F05D2260/98—Lubrication

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • General Details Of Gearings (AREA)
  • Rolling Contact Bearings (AREA)

Abstract

Turbomachine (1) comprenant une soufflante (2) comportant un premier arbre (5) entraîné en rotation via un réducteur (6), ledit premier arbre (5) étant guidé en rotation par rapport à un support (14) d'une structure fixe (8) via un palier amont (15) et un palier aval (16), ledit palier aval (16) guidant en rotation ledit premier arbre (5) par rapport à une branche aval (18) dudit support (14), ledit premier arbre (5) et ledit support (14) définissant entre eux une enceinte (19), ledit réducteur (6) comprenant une couronne (20) fixée à ladite structure (8) via une enveloppe (21), ladite turbomachine (1) comprenant des moyens de lubrification comportant au moins une canalisation d'acheminement (22) d'un lubrifiant liquide, caractérisée en ce que ladite canalisation (22) est située dans ladite enceinte (19), ladite canalisation (22) traversant un orifice (23) pratiqué dans ladite enveloppe (21) et une ouverture (24) pratiquée dans ladite branche aval (18).
FR1858672A 2018-09-24 2018-09-24 Turbomachine a reducteur pour un aeronef Active FR3086341B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1858672A FR3086341B1 (fr) 2018-09-24 2018-09-24 Turbomachine a reducteur pour un aeronef
US16/580,823 US11085329B2 (en) 2018-09-24 2019-09-24 Aircraft turbine engine with reduction gear
GB1913713.2A GB2578522B (en) 2018-09-24 2019-09-24 Aircraft turbine engine with reduction gear

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1858672 2018-09-24
FR1858672A FR3086341B1 (fr) 2018-09-24 2018-09-24 Turbomachine a reducteur pour un aeronef

Publications (2)

Publication Number Publication Date
FR3086341A1 FR3086341A1 (fr) 2020-03-27
FR3086341B1 true FR3086341B1 (fr) 2020-11-27

Family

ID=65243816

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1858672A Active FR3086341B1 (fr) 2018-09-24 2018-09-24 Turbomachine a reducteur pour un aeronef

Country Status (3)

Country Link
US (1) US11085329B2 (fr)
FR (1) FR3086341B1 (fr)
GB (1) GB2578522B (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3114836B1 (fr) * 2020-10-01 2022-09-02 Safran Aircraft Engines Support statorique pour un arbre de soufflante entraine par une boite de reduction de vitesse dans une turbomachine
FR3132732B1 (fr) * 2022-02-17 2024-07-05 Safran Aircraft Engines Turbomachine pour un aeronef
FR3135303B1 (fr) 2022-05-04 2024-05-24 Safran Trans Systems Procédé de pré-assemblage pour une turbomachine d’aéronef
FR3137720B1 (fr) * 2022-07-07 2024-09-20 Safran Aircraft Engines Dispositif de recuperation d’huile pour une turbomachine

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2234035B (en) * 1989-07-21 1993-05-12 Rolls Royce Plc A reduction gear assembly and a gas turbine engine
US5603602A (en) * 1994-08-08 1997-02-18 Pratt & Whitney Canada Inc. Pressurized ball bearing assemblies
US10151248B2 (en) * 2007-10-03 2018-12-11 United Technologies Corporation Dual fan gas turbine engine and gear train
US9995174B2 (en) 2010-10-12 2018-06-12 United Technologies Corporation Planetary gear system arrangement with auxiliary oil system
US9004849B2 (en) * 2012-01-10 2015-04-14 United Technologies Corporation Gas turbine engine forward bearing compartment architecture
US9416677B2 (en) * 2012-01-10 2016-08-16 United Technologies Corporation Gas turbine engine forward bearing compartment architecture
US8402741B1 (en) * 2012-01-31 2013-03-26 United Technologies Corporation Gas turbine engine shaft bearing configuration
FR2987402B1 (fr) * 2012-02-23 2015-02-27 Snecma Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire.
CA2864975C (fr) 2012-02-23 2019-03-12 Snecma Dispositif de recuperation de l'huile de lubrification d'un reducteur epicycloidal
US9410447B2 (en) * 2012-07-30 2016-08-09 United Technologies Corporation Forward compartment service system for a geared architecture gas turbine engine
US10508562B2 (en) * 2015-12-01 2019-12-17 United Technologies Corporation Geared turbofan with four star/planetary gear reduction
US10066734B2 (en) * 2015-12-07 2018-09-04 United Technologies Corporation Gear driven gas turbine engine assembly
FR3049006B1 (fr) * 2016-03-15 2018-03-16 Safran Aircraft Engines Turboreacteur ayant un groupe lubrification des paliers simplifie
FR3049007B1 (fr) * 2016-03-15 2019-05-10 Safran Aircraft Engines Turboreacteur ayant un groupe lubrification des paliers simplifie
US10316855B2 (en) * 2016-06-13 2019-06-11 United Technologies Corporation Shaft anti-rotation device
US9932986B2 (en) * 2016-08-05 2018-04-03 United Technologies Corporation Variable preloaded duplex thrust bearing system for a geared turbofan engine
US10436065B2 (en) * 2016-08-18 2019-10-08 United Technologies Corporation Resilient bearing mount with integral damper fluid passage for a geared turbofan engine
FR3066559B1 (fr) * 2017-05-18 2019-06-07 Safran Aircraft Engines Module de soufflante a pales a calage variable
FR3066558B1 (fr) * 2017-05-18 2019-07-19 Safran Aircraft Engines Module de soufflante a pales a calage variable
FR3074552B1 (fr) * 2017-12-06 2019-11-22 Safran Transmission Systems Couronne de reducteur de vitesse a train planetaire de turbomachine
FR3075878B1 (fr) * 2017-12-22 2019-11-22 Safran Aircraft Engines Dispositif d'accouplement de deux arbres de turbomachine d'aeronef
US11168585B2 (en) * 2018-01-08 2021-11-09 Raytheon Technologies Corporation Geared gas turbine engine with improved breather air venting
FR3081513B1 (fr) * 2018-05-28 2021-06-18 Safran Aircraft Engines Systeme de transmission de puissance comprenant un dispositif de recuperation d'huile de lubrification et turbomachine equipee d'un tel systeme de transmission de puissance
DE102019204507B4 (de) * 2019-03-29 2024-01-11 Rolls-Royce Deutschland Ltd & Co Kg Gleitlagervorrichtung, ein Verfahren zum Betrieb einer Gleitlagervorrichtung und ein Gasturbinentriebwerk

Also Published As

Publication number Publication date
GB2578522B (en) 2022-05-11
US20200095890A1 (en) 2020-03-26
US11085329B2 (en) 2021-08-10
GB2578522A (en) 2020-05-13
FR3086341A1 (fr) 2020-03-27
GB201913713D0 (en) 2019-11-06

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