FR3118483B1 - Module de turbomachine equipe d’une machine electrique et turbomachine equipee d’un tel module - Google Patents

Module de turbomachine equipe d’une machine electrique et turbomachine equipee d’un tel module Download PDF

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Publication number
FR3118483B1
FR3118483B1 FR2014169A FR2014169A FR3118483B1 FR 3118483 B1 FR3118483 B1 FR 3118483B1 FR 2014169 A FR2014169 A FR 2014169A FR 2014169 A FR2014169 A FR 2014169A FR 3118483 B1 FR3118483 B1 FR 3118483B1
Authority
FR
France
Prior art keywords
module
turbomachine
electric machine
transfer shaft
power transmission
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
FR2014169A
Other languages
English (en)
Other versions
FR3118483A1 (fr
Inventor
Frédéric Dautreppe
Jean-Pierre Elie Galivel
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 FR2014169A priority Critical patent/FR3118483B1/fr
Priority to PCT/FR2021/052401 priority patent/WO2022144514A1/fr
Priority to EP21852035.1A priority patent/EP4267839A1/fr
Priority to CN202180088125.2A priority patent/CN116745512A/zh
Priority to US18/259,226 priority patent/US20240052789A1/en
Publication of FR3118483A1 publication Critical patent/FR3118483A1/fr
Application granted granted Critical
Publication of FR3118483B1 publication Critical patent/FR3118483B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • 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
    • 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
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • 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
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

TITRE : MODULE DE TURBOMACHINE EQUIPE D’UNE MACHINE ELECTRIQUE ET TURBOMACHINE EQUIPEE D’UN TEL MODULE L’invention concerne un module de turbomachine pour aéronef, comprenant un boîtier d’accessoires (30) ainsi qu’un arbre de transfert (34) et un arbre d’entrainement (25) liés en rotation l’un à l’autre par l’intermédiaire d’un dispositif de transmission de puissance (37), le dispositif de transmission de puissance (37) étant logé dans un boitier de transmission (50), le module comprenant en outre une machine électrique (54) reliée en rotation à l’arbre de transfert (34). Selon l’invention, la machine électrique (54) est intercalée entre le boitier de transmission (50) et au moins une partie (64a) de l’arbre de transfert (34). Figure pour l’abrégé : Figure  2
FR2014169A 2020-12-28 2020-12-28 Module de turbomachine equipe d’une machine electrique et turbomachine equipee d’un tel module Active FR3118483B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR2014169A FR3118483B1 (fr) 2020-12-28 2020-12-28 Module de turbomachine equipe d’une machine electrique et turbomachine equipee d’un tel module
PCT/FR2021/052401 WO2022144514A1 (fr) 2020-12-28 2021-12-20 Module de turbomachine equipe d'une machine electrique et turbomachine equipee d'un tel module
EP21852035.1A EP4267839A1 (fr) 2020-12-28 2021-12-20 Module de turbomachine equipe d'une machine electrique et turbomachine equipee d'un tel module
CN202180088125.2A CN116745512A (zh) 2020-12-28 2021-12-20 配备有电机的涡轮机模块以及配备有这种模块的涡轮机
US18/259,226 US20240052789A1 (en) 2020-12-28 2021-12-20 Turbomachine module equipped with an electric machine, and turbomachine equipped with such a module

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2014169 2020-12-28
FR2014169A FR3118483B1 (fr) 2020-12-28 2020-12-28 Module de turbomachine equipe d’une machine electrique et turbomachine equipee d’un tel module

Publications (2)

Publication Number Publication Date
FR3118483A1 FR3118483A1 (fr) 2022-07-01
FR3118483B1 true FR3118483B1 (fr) 2024-02-16

Family

ID=74669115

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2014169A Active FR3118483B1 (fr) 2020-12-28 2020-12-28 Module de turbomachine equipe d’une machine electrique et turbomachine equipee d’un tel module

Country Status (5)

Country Link
US (1) US20240052789A1 (fr)
EP (1) EP4267839A1 (fr)
CN (1) CN116745512A (fr)
FR (1) FR3118483B1 (fr)
WO (1) WO2022144514A1 (fr)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2905414B1 (fr) * 2006-08-29 2013-03-01 Snecma Dispositif d'entrainement du rotor d'un equipement auxiliaire d'un turbomoteur.
US7997085B2 (en) * 2006-09-27 2011-08-16 General Electric Company Gas turbine engine assembly and method of assembling same
FR2950657A1 (fr) 2009-09-29 2011-04-01 Snecma Procede et dispositif de controle d'une partie tournante du corps haute pression d'un moteur d'avion.
US8814502B2 (en) * 2011-05-31 2014-08-26 Pratt & Whitney Canada Corp. Dual input drive AGB for gas turbine engines
DE102011112252A1 (de) * 2011-09-02 2013-03-07 Rolls-Royce Deutschland Ltd & Co Kg Generator und Hilfsgerätegetriebeeinrichtung mit einem Generator
DE102011112255A1 (de) * 2011-09-02 2013-03-07 Rolls-Royce Deutschland Ltd & Co Kg Hilfsgerätegetriebeeinrichtung für ein Triebwerk
JP5568596B2 (ja) * 2012-05-30 2014-08-06 川崎重工業株式会社 航空機用エンジンのギヤボックス一体型発電装置
US20180283281A1 (en) * 2017-03-31 2018-10-04 Hamilton Sundstrand Corporation Accessory gearboxes
US10599165B2 (en) * 2017-11-15 2020-03-24 Hamilton Sundstrand Corporation Governor and inversion pump drive gear

Also Published As

Publication number Publication date
US20240052789A1 (en) 2024-02-15
FR3118483A1 (fr) 2022-07-01
CN116745512A (zh) 2023-09-12
WO2022144514A1 (fr) 2022-07-07
EP4267839A1 (fr) 2023-11-01

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