BR112017022476A2 - redutor com trem de engrenagens epicicloidal para uma turbomáquina - Google Patents
redutor com trem de engrenagens epicicloidal para uma turbomáquinaInfo
- Publication number
- BR112017022476A2 BR112017022476A2 BR112017022476-3A BR112017022476A BR112017022476A2 BR 112017022476 A2 BR112017022476 A2 BR 112017022476A2 BR 112017022476 A BR112017022476 A BR 112017022476A BR 112017022476 A2 BR112017022476 A2 BR 112017022476A2
- Authority
- BR
- Brazil
- Prior art keywords
- axis
- turbomachine
- gearbox
- planetary
- gear train
- Prior art date
Links
Classifications
-
- 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
- F16H57/08—General details of gearing of gearings with members having orbital motion
- F16H57/082—Planet carriers
-
- 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
- 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
- F02K3/025—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 by-pass flow being at least partly used to create an independent thrust component
-
- 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
- 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
- F16H57/048—Type of gearings to be lubricated, cooled or heated
- F16H57/0482—Gearings 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/324—Application in turbines in gas turbines to drive unshrouded, low solidity propeller
-
- 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
- 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
- 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
- F16H57/08—General details of gearing of gearings with members having orbital motion
- F16H2057/085—Bearings for orbital gears
-
- 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)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Details Of Gearings (AREA)
- Retarders (AREA)
Abstract
a invenção se refere a um redutor (11) com trem epicicloidal para uma turbomáquina (1), em especial de aeronave, que compreende um eixo planetário (15) de eixo a de rotação, uma coroa (19) de eixo a que se estende em torno do dito eixo planetário (15), satélites (18) distribuídos em torno do dito eixo a, que são engrenados com a dita coroa (19) e o eixo planetário (15), e um suporte-satélites que compreende, por um lado, membros de suporte (21) de mancais (23a, 23b) dos satélites (18a, 18b), de eixos de rotação b, que são regularmente distribuídos em torno do eixo a, e por outro lado, uma peça (38) que retém cada membro de suporte (21) substancialmente por seu meio de acordo com seu eixo b, caracterizado pelo fato de que os ditos membros (21) de suporte são formados de uma só peça com meios (45, 46, 41) de alimentação com óleo de lubrificação dos ditos mancais (23a, 23b). ela também se refere a um processo de montagem do dito redutor.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1553675A FR3035375B1 (fr) | 2015-04-23 | 2015-04-23 | Reducteur a train d'engrenages epicycloidal pour une turbomachine. |
FR1553675 | 2015-04-23 | ||
PCT/FR2016/050943 WO2017005997A2 (fr) | 2015-04-23 | 2016-04-21 | Reducteur a train d'engrenages epicycloïdal pour une turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112017022476A2 true BR112017022476A2 (pt) | 2018-07-10 |
BR112017022476B1 BR112017022476B1 (pt) | 2022-12-06 |
Family
ID=53524814
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112017022476-3A BR112017022476B1 (pt) | 2015-04-23 | 2016-04-21 | Redutor com trem de engrenagens epicicloidal para uma turbomáquina, turbomáquina e processo de realização de um redutor |
Country Status (9)
Country | Link |
---|---|
US (1) | US10302187B2 (pt) |
EP (1) | EP3286457B1 (pt) |
JP (1) | JP6768699B2 (pt) |
CN (1) | CN107532518B (pt) |
BR (1) | BR112017022476B1 (pt) |
CA (1) | CA2982888C (pt) |
FR (1) | FR3035375B1 (pt) |
RU (1) | RU2704516C2 (pt) |
WO (1) | WO2017005997A2 (pt) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2898464C (en) * | 2013-01-18 | 2017-10-10 | Craig Miller Kuhne | Engine architecture with reverse rotation integral drive and vaneless turbine |
US10801442B2 (en) * | 2017-02-08 | 2020-10-13 | General Electric Company | Counter rotating turbine with reversing reduction gear assembly |
DE102017108332A1 (de) * | 2017-04-19 | 2018-10-25 | Rolls-Royce Deutschland Ltd & Co Kg | Getriebevorrichtung mit wenigstens einem gegenüber einer Gehäuseeinrichtung drehenden Bauteil |
CN107178426B (zh) * | 2017-06-07 | 2019-04-26 | 南昌航空大学 | 一种蓄功调速齿轮传动涡轮发动机 |
FR3074552B1 (fr) * | 2017-12-06 | 2019-11-22 | Safran Transmission Systems | Couronne de reducteur de vitesse a train planetaire de turbomachine |
DE102018101723A1 (de) * | 2018-01-25 | 2019-07-25 | Rolls-Royce Deutschland Ltd & Co Kg | Vorrichtung und Flugtriebwerk mit einer Vorrichtung |
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 |
FR3084429B1 (fr) * | 2018-07-26 | 2020-11-13 | Safran Trans Systems | Dispositif du type reducteur ou differentiel pour une turbomachine d'aeronef |
FR3086343B1 (fr) * | 2018-09-24 | 2020-09-04 | Safran Aircraft Engines | Turbomachine a reducteur pour un aeronef |
FR3088979B1 (fr) * | 2018-11-23 | 2021-06-18 | Safran Trans Systems | Porte-satellites pour un reducteur mecanique de turbomachine d’aeronef |
FR3092884B1 (fr) * | 2019-02-20 | 2022-12-16 | Safran Trans Systems | Ensemble a reducteur planetaire pour une turbomachine |
CN111609093A (zh) * | 2019-02-25 | 2020-09-01 | 通用电气公司 | 飞行器发动机动力齿轮箱的薄缘行星齿轮的设备和系统 |
FR3093550B1 (fr) * | 2019-03-07 | 2021-02-19 | Safran Aircraft Engines | Reducteur mecanique de turbomachine d’aeronef |
FR3096744B1 (fr) * | 2019-06-03 | 2022-01-14 | Safran Aircraft Engines | Ensemble de support et de guidage d’un arbre d’entrainement de turbomachine d’aeronef |
FR3097011B1 (fr) * | 2019-06-06 | 2022-02-18 | Safran Aircraft Engines | Reducteur planetaire pour une turbomachine d’aeronef |
FR3098562B1 (fr) * | 2019-07-08 | 2021-06-11 | Safran Trans Systems | Couvercle de canalisation d’huile et reducteur mecanique de turbomachine d’aeronef comportant un tel couvercle |
FR3098877B1 (fr) * | 2019-07-16 | 2023-03-17 | Safran Trans Systems | Collecteur d’huile pour un reducteur mecanique de turbomachine d’aeronef |
FR3103240B1 (fr) * | 2019-11-15 | 2022-07-15 | Safran Aircraft Engines | Rouet pour un porte-satellites de reducteur de vitesse a train epicycloïdal de turbomachine |
FR3104193B1 (fr) * | 2019-12-10 | 2021-10-29 | Safran Aircraft Engines | Recuperation d’huile de lubrification d’un reducteur de turbomachine d’aeronef |
CN113123871B (zh) * | 2021-04-21 | 2022-04-22 | 南京航空航天大学 | 一种带箍喷气自驱动和叶尖涡轮驱动的对转桨扇发动机 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
FR2962109B1 (fr) * | 2010-07-05 | 2013-04-12 | Snecma | Turbomoteur a helices non carenees |
ITBO20100109U1 (it) * | 2010-10-29 | 2012-04-30 | Bonfiglioli Riduttori Spa | Riduttore epicicloidale |
FR2979121B1 (fr) * | 2011-08-18 | 2013-09-06 | Snecma | Dispositif de transmission mecanique pour l'entrainement en rotation des helices contrarotatives d'un turbopropulseur a double helice. |
FR2987417B1 (fr) * | 2012-02-23 | 2014-03-28 | Snecma | Dispositif de recuperation de l'huile de lubrification d'un reducteur epicycloidal. |
CN104169546B (zh) * | 2012-02-23 | 2017-05-03 | 斯奈克玛 | 用于从行星减速齿轮中回收润滑油的装置 |
GB201210146D0 (en) * | 2012-06-08 | 2012-07-25 | Rolls Royce Plc | Oil scavenge arrangement |
ES2623180T3 (es) * | 2012-09-04 | 2017-07-10 | Safran Transmission Systems | Reductor de tren epicicloidal, especialmente para turbomáquina |
FR3009594B1 (fr) * | 2013-08-08 | 2016-12-09 | Snecma | Reducteur a train epicycloidal avec canalisations de transfert de fluide, et turbomachine a helice(s) pour aeronef avec un tel reducteur |
RU2528236C1 (ru) * | 2013-08-27 | 2014-09-10 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Планетарно-дифференциальный редуктор |
US9038779B2 (en) * | 2013-08-30 | 2015-05-26 | United Technologies Corporation | Geared architecture gas turbine engine with oil scavenge |
-
2015
- 2015-04-23 FR FR1553675A patent/FR3035375B1/fr not_active Expired - Fee Related
-
2016
- 2016-04-21 CN CN201680022665.XA patent/CN107532518B/zh active Active
- 2016-04-21 CA CA2982888A patent/CA2982888C/fr active Active
- 2016-04-21 EP EP16725185.9A patent/EP3286457B1/fr active Active
- 2016-04-21 JP JP2017554569A patent/JP6768699B2/ja active Active
- 2016-04-21 BR BR112017022476-3A patent/BR112017022476B1/pt active IP Right Grant
- 2016-04-21 RU RU2017136708A patent/RU2704516C2/ru active
- 2016-04-21 WO PCT/FR2016/050943 patent/WO2017005997A2/fr active Application Filing
- 2016-04-21 US US15/567,493 patent/US10302187B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
WO2017005997A3 (fr) | 2017-03-23 |
US10302187B2 (en) | 2019-05-28 |
CN107532518B (zh) | 2019-09-10 |
CN107532518A (zh) | 2018-01-02 |
RU2704516C2 (ru) | 2019-10-29 |
EP3286457A2 (fr) | 2018-02-28 |
CA2982888A1 (fr) | 2017-01-12 |
RU2017136708A3 (pt) | 2019-09-30 |
JP6768699B2 (ja) | 2020-10-14 |
FR3035375B1 (fr) | 2018-07-27 |
BR112017022476B1 (pt) | 2022-12-06 |
FR3035375A1 (fr) | 2016-10-28 |
EP3286457B1 (fr) | 2020-02-12 |
JP2018516331A (ja) | 2018-06-21 |
US20180163850A1 (en) | 2018-06-14 |
WO2017005997A2 (fr) | 2017-01-12 |
CA2982888C (fr) | 2023-07-18 |
RU2017136708A (ru) | 2019-05-23 |
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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 21/04/2016, OBSERVADAS AS CONDICOES LEGAIS |