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FR3111671B1 - Turbomachine d’aeronef comportant un systeme de freinage en rotation d’un rotor pour une lubrification d’un reducteur entrainant une soufflante - Google Patents

Turbomachine d’aeronef comportant un systeme de freinage en rotation d’un rotor pour une lubrification d’un reducteur entrainant une soufflante Download PDF

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Publication number
FR3111671B1
FR3111671B1 FR2006415A FR2006415A FR3111671B1 FR 3111671 B1 FR3111671 B1 FR 3111671B1 FR 2006415 A FR2006415 A FR 2006415A FR 2006415 A FR2006415 A FR 2006415A FR 3111671 B1 FR3111671 B1 FR 3111671B1
Authority
FR
France
Prior art keywords
rotor
teeth
braking system
fan
lubrication
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
FR2006415A
Other languages
English (en)
Other versions
FR3111671A1 (fr
Inventor
Matthieu Bruno François Foglia
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 FR2006415A priority Critical patent/FR3111671B1/fr
Publication of FR3111671A1 publication Critical patent/FR3111671A1/fr
Application granted granted Critical
Publication of FR3111671B1 publication Critical patent/FR3111671B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • F02C7/06—Arrangements of bearings; Lubricating
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F05D2260/38—Retaining components in desired mutual position by a spring, i.e. spring loaded or biased towards a certain 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
    • F05D2260/40—Transmission of power
    • F05D2260/402—Transmission of power through friction drives
    • F05D2260/4023—Transmission of power through friction drives through a friction clutch
    • 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
    • F05D2260/90—Braking
    • F05D2260/902—Braking using frictional mechanical forces
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
  • Braking Arrangements (AREA)
  • General Details Of Gearings (AREA)

Abstract

L'invention concerne une turbomachine (1), comportant un arbre de soufflante (4), un arbre d’une turbine (3) couplé audit arbre (4) via un réducteur (6), un circuit principal (7) et une pompe auxiliaire (70) de lubrification dudit réducteur (6) comportant un rotor (74) entrainé autour d’un axe (A) par un dispositif de prélèvement de puissance (8) sur l’un desdits arbres (3, 4), et un système de freinage (9) du rotor (74) comportant des premières dents (92) complémentaires de secondes dents (72) portées par ledit rotor (74), ledit système (9) est mobile en translation le long de l’axe (A) entre une position de couplage dans laquelle lesdites dents (92, 72) sont engagées et une position de découplage dans laquelle lesdites dents (92, 72) sont désengagées, sélectivement en fonction d’un seuil de couple transmis par le rotor au système dans chacun des deux sens de rotation (S1, S2). Figure pour l'abrégé : Figure 2
FR2006415A 2020-06-19 2020-06-19 Turbomachine d’aeronef comportant un systeme de freinage en rotation d’un rotor pour une lubrification d’un reducteur entrainant une soufflante Active FR3111671B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2006415A FR3111671B1 (fr) 2020-06-19 2020-06-19 Turbomachine d’aeronef comportant un systeme de freinage en rotation d’un rotor pour une lubrification d’un reducteur entrainant une soufflante

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2006415A FR3111671B1 (fr) 2020-06-19 2020-06-19 Turbomachine d’aeronef comportant un systeme de freinage en rotation d’un rotor pour une lubrification d’un reducteur entrainant une soufflante
FR2006415 2020-06-19

Publications (2)

Publication Number Publication Date
FR3111671A1 FR3111671A1 (fr) 2021-12-24
FR3111671B1 true FR3111671B1 (fr) 2022-05-20

Family

ID=72178825

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2006415A Active FR3111671B1 (fr) 2020-06-19 2020-06-19 Turbomachine d’aeronef comportant un systeme de freinage en rotation d’un rotor pour une lubrification d’un reducteur entrainant une soufflante

Country Status (1)

Country Link
FR (1) FR3111671B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3144192A1 (fr) * 2022-12-21 2024-06-28 Safran Aircraft Engines Système propulsif aéronautique
US20240426250A1 (en) * 2023-06-21 2024-12-26 General Electric Company Unidirectional fan brake for a gas turbine engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7849668B2 (en) * 2006-10-25 2010-12-14 United Technologies Corporation Rotor brake and windmilling lubrication system for geared turbofan engine
US9970352B2 (en) * 2012-01-27 2018-05-15 United Technologies Corporation Turbomachine fan clutch
FR3075862B1 (fr) * 2017-12-22 2020-08-28 Safran Aircraft Engines Dispositif de freinage d'une soufflante de turbomachine
FR3075864B1 (fr) * 2017-12-22 2019-11-15 Safran Aircraft Engines Turbomachine comportant une soufflante decouplable d'une turbine par l'intermediaire d'un accouplement curvic rappele elastiquement

Also Published As

Publication number Publication date
FR3111671A1 (fr) 2021-12-24

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