JP6526019B2 - 減速ターボ機械の羽根組の回転装置のための遊星歯車減速装置 - Google Patents

減速ターボ機械の羽根組の回転装置のための遊星歯車減速装置 Download PDF

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JP6526019B2
JP6526019B2 JP2016545300A JP2016545300A JP6526019B2 JP 6526019 B2 JP6526019 B2 JP 6526019B2 JP 2016545300 A JP2016545300 A JP 2016545300A JP 2016545300 A JP2016545300 A JP 2016545300A JP 6526019 B2 JP6526019 B2 JP 6526019B2
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Prior art keywords
joint
planetary gear
constant velocity
blades
ball transmission
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Japanese (ja)
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JP2017503960A (ja
Inventor
キュルリエ オーギュスタン
キュルリエ オーギュスタン
ミシェル パトリク クリスチャン オストリュイ ジュリアン
ミシェル パトリク クリスチャン オストリュイ ジュリアン
ブーデビザ テウフィク
ブーデビザ テウフィク
アラン シャリエ ジル
アラン シャリエ ジル
Original Assignee
サフラン エアークラフト エンジンズ
サフラン エアークラフト エンジンズ
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    • 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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/16—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts
    • F16D3/20—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members
    • F16D3/22—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members the rolling members being balls, rollers, or the like, guided in grooves or sockets in both coupling parts
    • F16D3/223—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members the rolling members being balls, rollers, or the like, guided in grooves or sockets in both coupling parts the rolling members being guided in grooves in both coupling parts
    • 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
    • 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

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Retarders (AREA)
JP2016545300A 2014-01-07 2014-12-24 減速ターボ機械の羽根組の回転装置のための遊星歯車減速装置 Active JP6526019B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1450080 2014-01-07
FR1450080A FR3016189B1 (fr) 2014-01-07 2014-01-07 Dispositif de reduction epicycloidal pour l'entrainement en rotation des ensembles de pales d'une turbomachine a reducteur
PCT/FR2014/053553 WO2015104474A1 (fr) 2014-01-07 2014-12-24 Dispositif de réduction épicycloïdal pour l'entraînement en rotation des ensembles de pales d'une turbomachine a réducteur

Publications (2)

Publication Number Publication Date
JP2017503960A JP2017503960A (ja) 2017-02-02
JP6526019B2 true JP6526019B2 (ja) 2019-06-05

Family

ID=50729601

Family Applications (1)

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JP2016545300A Active JP6526019B2 (ja) 2014-01-07 2014-12-24 減速ターボ機械の羽根組の回転装置のための遊星歯車減速装置

Country Status (9)

Country Link
US (1) US10495005B2 (enExample)
EP (1) EP3092396B1 (enExample)
JP (1) JP6526019B2 (enExample)
CN (1) CN105899794B (enExample)
BR (1) BR112016015768B1 (enExample)
CA (1) CA2936046C (enExample)
FR (1) FR3016189B1 (enExample)
RU (1) RU2673639C2 (enExample)
WO (1) WO2015104474A1 (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11339723B2 (en) * 2012-10-01 2022-05-24 Raytheon Technologies Corporation Geared turbofan high gearbox power density
FR3041990B1 (fr) * 2015-10-05 2019-03-22 Safran Aircraft Engines Ensemble de propulsion d'un aeronef
US10801442B2 (en) * 2017-02-08 2020-10-13 General Electric Company Counter rotating turbine with reversing reduction gear assembly
DE102017008674A1 (de) * 2017-09-15 2019-03-21 Rolls-Royce Deutschland Ltd & Co Kg Planetengetriebe
FR3072749B1 (fr) * 2017-10-24 2020-01-03 Safran Transmission Systems Train d'engrenages epicycloidal
FR3081959B1 (fr) * 2018-06-05 2020-07-17 Safran Transmission Systems Procede d'assemblage d'un reducteur et installation de mise en oeuvre du procede
EP3587773B1 (en) * 2018-06-27 2022-06-08 Rolls-Royce plc Gas turbine
US11174916B2 (en) 2019-03-21 2021-11-16 Pratt & Whitney Canada Corp. Aircraft engine reduction gearbox
FR3098548B1 (fr) * 2019-07-08 2022-07-15 Safran Trans Systems Reducteur mecanique pour une turbomachine d’aeronef
US11268453B1 (en) 2021-03-17 2022-03-08 Pratt & Whitney Canada Corp. Lubrication system for aircraft engine reduction gearbox
FR3125018B1 (fr) * 2021-07-06 2024-05-10 Safran Aircraft Engines Système de propulsion d’aéronef à ingestion de couche limite
US11852080B1 (en) * 2022-08-05 2023-12-26 General Electric Company Gearbox assembly

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Publication number Priority date Publication date Assignee Title
GB817490A (en) * 1956-05-04 1959-07-29 W H Allen Sons & Company Ltd Improvements in and relating to flexible couplings for transmitting or restraining torque especially in planetary or epicyclic gearing
US3352178A (en) * 1965-11-15 1967-11-14 Gen Motors Corp Planetary gearing
US5116293A (en) * 1990-02-14 1992-05-26 Dana Corporation Four wheel drive transfer case with cv joint angled front output shaft
RU2056002C1 (ru) * 1991-01-08 1996-03-10 Григорий Павлович Павлов Планетарный механизм
JP3465120B2 (ja) 1994-08-23 2003-11-10 日本車輌製造株式会社 遊星ローラ式変速機構を用いた動力伝達装置
JPH11190397A (ja) 1997-12-26 1999-07-13 Nissan Motor Co Ltd エンジンのロール振動低減装置
DE19828562B4 (de) * 1998-06-26 2005-09-08 Mtu Aero Engines Gmbh Triebwerk mit gegenläufig drehenden Rotoren
FR2817912B1 (fr) * 2000-12-07 2003-01-17 Hispano Suiza Sa Reducteur reprenant les efforts axiaux generes par la soufflante d'un turboreacteur
US6666102B2 (en) * 2002-05-16 2003-12-23 Sikorsky Aircraft Corporation Flexible bearing arrangement for double helical pinion
FR2866068B1 (fr) * 2004-02-06 2006-07-07 Snecma Moteurs Turboreacteur a soufflante solidaire d'un arbre d'entrainement supporte par un premier et un deuxieme paliers
US7726113B2 (en) * 2005-10-19 2010-06-01 General Electric Company Gas turbine engine assembly and methods of assembling same
US7591754B2 (en) * 2006-03-22 2009-09-22 United Technologies Corporation Epicyclic gear train integral sun gear coupling design
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FR2940247B1 (fr) * 2008-12-19 2011-01-21 Snecma Systeme d'helices contrarotatives entrainees par un train epicycloidal offrant une repartition de couple equilibree entre les deux helices
FR2942284B1 (fr) * 2009-02-16 2011-03-04 Snecma Lubrification et refroidissement d'un reducteur a train d'engrenages epicycloidal
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Also Published As

Publication number Publication date
RU2016132494A3 (enExample) 2018-09-28
EP3092396A1 (fr) 2016-11-16
JP2017503960A (ja) 2017-02-02
CA2936046A1 (fr) 2015-07-16
BR112016015768B1 (pt) 2022-05-10
US10495005B2 (en) 2019-12-03
EP3092396B1 (fr) 2019-09-18
CA2936046C (fr) 2022-04-12
US20160326964A1 (en) 2016-11-10
BR112016015768A2 (enExample) 2017-08-08
FR3016189A1 (fr) 2015-07-10
CN105899794A (zh) 2016-08-24
RU2016132494A (ru) 2018-02-16
WO2015104474A1 (fr) 2015-07-16
FR3016189B1 (fr) 2018-09-28
CN105899794B (zh) 2018-03-13
RU2673639C2 (ru) 2018-11-28

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