BR112016015768B1 - Dispositivo de engrenagem epicíclico para acionar a rotação de pelo menos um primeiro conjunto de pás de uma turbomáquina - Google Patents

Dispositivo de engrenagem epicíclico para acionar a rotação de pelo menos um primeiro conjunto de pás de uma turbomáquina Download PDF

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Publication number
BR112016015768B1
BR112016015768B1 BR112016015768-0A BR112016015768A BR112016015768B1 BR 112016015768 B1 BR112016015768 B1 BR 112016015768B1 BR 112016015768 A BR112016015768 A BR 112016015768A BR 112016015768 B1 BR112016015768 B1 BR 112016015768B1
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BR
Brazil
Prior art keywords
joint
blades
satellite
ball transmission
constant speed
Prior art date
Application number
BR112016015768-0A
Other languages
English (en)
Portuguese (pt)
Other versions
BR112016015768A2 (https=
Inventor
Augustin Curlier
Julien Michel Patrick Christian Austruy
Tewfik Boudebiza
Gilles Alain Charier
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BR112016015768A2 publication Critical patent/BR112016015768A2/pt
Publication of BR112016015768B1 publication Critical patent/BR112016015768B1/pt

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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
    • 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)
BR112016015768-0A 2014-01-07 2014-12-24 Dispositivo de engrenagem epicíclico para acionar a rotação de pelo menos um primeiro conjunto de pás de uma turbomáquina BR112016015768B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
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
FR1450080 2014-01-07
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
BR112016015768A2 BR112016015768A2 (https=) 2017-08-08
BR112016015768B1 true BR112016015768B1 (pt) 2022-05-10

Family

ID=50729601

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016015768-0A BR112016015768B1 (pt) 2014-01-07 2014-12-24 Dispositivo de engrenagem epicíclico para acionar a rotação de pelo menos um primeiro conjunto de pás de uma turbomáquina

Country Status (9)

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

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2904250A4 (en) * 2012-10-01 2015-10-21 United Technologies Corp HIGH POWER TRANSMISSION POWER DENSITY OF A DOUBLE-FLOW GEAR TURBOFACTOR
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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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
BE1017140A3 (nl) 2006-05-15 2008-03-04 Hansen Transmissions Int Drukkam voor een tandwieloverbrenging.
US7694505B2 (en) * 2006-07-31 2010-04-13 General Electric Company Gas turbine engine assembly and method of assembling same
US8753243B2 (en) * 2006-08-15 2014-06-17 United Technologies Corporation Ring gear mounting arrangement with oil scavenge scheme
US20090062058A1 (en) * 2007-08-27 2009-03-05 Kimes John W Plantary Transmission Having Double Helical Teeth
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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
FR2943035B1 (fr) * 2009-03-11 2012-09-28 Snecma Dispositif d'entrainement d'une paire d'helices contrarotives par un train epycycloidal
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US8720306B2 (en) * 2012-01-31 2014-05-13 United Technologies Corporation Turbine engine gearbox

Also Published As

Publication number Publication date
RU2016132494A3 (https=) 2018-09-28
FR3016189A1 (fr) 2015-07-10
CN105899794A (zh) 2016-08-24
CA2936046C (fr) 2022-04-12
EP3092396A1 (fr) 2016-11-16
JP6526019B2 (ja) 2019-06-05
US20160326964A1 (en) 2016-11-10
US10495005B2 (en) 2019-12-03
RU2016132494A (ru) 2018-02-16
RU2673639C2 (ru) 2018-11-28
BR112016015768A2 (https=) 2017-08-08
WO2015104474A1 (fr) 2015-07-16
EP3092396B1 (fr) 2019-09-18
CA2936046A1 (fr) 2015-07-16
FR3016189B1 (fr) 2018-09-28
JP2017503960A (ja) 2017-02-02
CN105899794B (zh) 2018-03-13

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 24/12/2014, OBSERVADAS AS CONDICOES LEGAIS