IT1250861B - Riduttore di velocita' epicicloidale atto ad essere inserito nella trasmissione tra una turbina a gas ed il compressore d'aria di un motore aeronautico. - Google Patents
Riduttore di velocita' epicicloidale atto ad essere inserito nella trasmissione tra una turbina a gas ed il compressore d'aria di un motore aeronautico.Info
- Publication number
- IT1250861B IT1250861B ITTO910871A ITTO910871A IT1250861B IT 1250861 B IT1250861 B IT 1250861B IT TO910871 A ITTO910871 A IT TO910871A IT TO910871 A ITTO910871 A IT TO910871A IT 1250861 B IT1250861 B IT 1250861B
- Authority
- IT
- Italy
- Prior art keywords
- satellite
- transmission
- gas turbine
- air compressor
- speed reducer
- 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
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H1/2809—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet-wheels
- F16H1/2836—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet-wheels by allowing limited movement of the planets relative to the planet carrier or by using free floating planets
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Retarders (AREA)
- General Details Of Gearings (AREA)
Abstract
Il riduttore comprende una ruota dentata solare (5) collegata con la turbina, un organo portasatelliti (6) atto a sopportare una pluralità di ruote dentate satelliti (7) ingrananti con la ruota dentata solare e con una corona dentata (8) fissata all'incastellatura del motore; in base all'invenzione l'organo portasatelliti (6) comprende un primo elemento di forma sostanzialmente anulare (10) il quale è provvisto di coppie di sedi (11) per perni (13) su ciascuno dei quali ruota una delle ruote dentate satelliti (7), un secondo elemento (17) collegato al compressore è provvisto di una pluralità di bracci assiali (18) ciascuno dei quali è atto ad inserirsi in una cavità (16) del primo elemento e mezzi di collegamento (19) atti a collegare l'estremità di ciascuno dei bracci suddetti ad una zona (20) del primo elemento (10) la quale è posizionata sostanzialmente alla stessa distanza dalle due sedi (11) di ciascuno di dette coppie di sedi.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITTO910871A IT1250861B (it) | 1991-11-12 | 1991-11-12 | Riduttore di velocita' epicicloidale atto ad essere inserito nella trasmissione tra una turbina a gas ed il compressore d'aria di un motore aeronautico. |
US07/975,414 US5391125A (en) | 1991-11-12 | 1992-11-12 | Epicyclic speed reducer designed for fitment to the transmission between the gas turbine and air compressor of an aircraft engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITTO910871A IT1250861B (it) | 1991-11-12 | 1991-11-12 | Riduttore di velocita' epicicloidale atto ad essere inserito nella trasmissione tra una turbina a gas ed il compressore d'aria di un motore aeronautico. |
Publications (3)
Publication Number | Publication Date |
---|---|
ITTO910871A0 ITTO910871A0 (it) | 1991-11-12 |
ITTO910871A1 ITTO910871A1 (it) | 1993-05-12 |
IT1250861B true IT1250861B (it) | 1995-04-21 |
Family
ID=11409714
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ITTO910871A IT1250861B (it) | 1991-11-12 | 1991-11-12 | Riduttore di velocita' epicicloidale atto ad essere inserito nella trasmissione tra una turbina a gas ed il compressore d'aria di un motore aeronautico. |
Country Status (2)
Country | Link |
---|---|
US (1) | US5391125A (it) |
IT (1) | IT1250861B (it) |
Families Citing this family (64)
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SE519200C2 (sv) * | 2001-06-05 | 2003-01-28 | Volvo Aero Corp | Gasturbinanordning med ett arrangemang för drivning av en eller flera hjälpapparater |
US6964155B2 (en) * | 2002-12-30 | 2005-11-15 | United Technologies Corporation | Turbofan engine comprising an spicyclic transmission having bearing journals |
EP1606535A1 (de) * | 2003-03-25 | 2005-12-21 | Klaus Plath | Getriebevorrichtung |
FR2853382B1 (fr) * | 2003-04-04 | 2006-04-28 | Hispano Suiza Sa | Systeme de liaison souple entre un porte-satellites et le support fixe dans un reducteur de vitesse |
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US20120213628A1 (en) | 2006-08-15 | 2012-08-23 | Mccune Michael E | Gas turbine engine with geared architecture |
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US8708863B2 (en) * | 2006-08-15 | 2014-04-29 | United Technologies Corporation | Epicyclic gear train |
JP4380699B2 (ja) * | 2006-12-28 | 2009-12-09 | トヨタ自動車株式会社 | 遊星歯車装置および自動変速機 |
US7621843B2 (en) * | 2007-01-17 | 2009-11-24 | General Electric Company | Apparatus for restraining axial movement of a ring gear in a gearbox for a wind turbine |
ES2376960T3 (es) * | 2007-10-22 | 2012-03-21 | Vestas Wind Systems A/S | Etapa de engranajes epicicloidales para una caja de engranajes de turbina eólica, caja de engranajes de turbina eólica y turbina eólica |
CN101903650A (zh) * | 2007-12-20 | 2010-12-01 | 维斯塔斯风力***集团公司 | 用于风轮机齿轮箱的行星齿轮级、风轮机齿轮箱与风轮机 |
FI122381B (fi) * | 2008-01-03 | 2011-12-30 | Moventas Oy | Planeettavaihde |
US8246503B2 (en) * | 2009-06-10 | 2012-08-21 | United Technologies Corporation | Epicyclic gear system with improved lubrication system |
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US8333678B2 (en) * | 2009-06-26 | 2012-12-18 | United Technologies Corporation | Epicyclic gear system with load share reduction |
US8672801B2 (en) * | 2009-11-30 | 2014-03-18 | United Technologies Corporation | Mounting system for a planetary gear train in a gas turbine engine |
US8900083B2 (en) | 2011-04-27 | 2014-12-02 | United Technologies Corporation | Fan drive gear system integrated carrier and torque frame |
US8777793B2 (en) | 2011-04-27 | 2014-07-15 | United Technologies Corporation | Fan drive planetary gear system integrated carrier and torque frame |
US20130269479A1 (en) * | 2012-04-11 | 2013-10-17 | General Electric Company | Gearbox and support apparatus for gearbox carrier |
FR2991421B1 (fr) * | 2012-05-30 | 2015-07-31 | Snecma | Reducteur a train epicycloidal avec axes de satellites montes sur roulements |
US9328818B2 (en) | 2012-09-21 | 2016-05-03 | United Technologies Corporation | Gear carrier flex mount lubrication |
US8657714B1 (en) * | 2012-09-28 | 2014-02-25 | General Electric Company | Journal bearing and method of facilitating hydrodynamic oil flow, load capacity and optimization of bearing performance |
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US8857149B1 (en) | 2013-08-26 | 2014-10-14 | United Technologies Corporation | Torque connector lubrication scuppers |
FR3011901B1 (fr) | 2013-10-10 | 2017-02-10 | Hispano-Suiza | Porte-satellites pour un reducteur de vitesse a train epicycloidal |
EP3097324B1 (en) | 2014-01-20 | 2019-04-03 | United Technologies Corporation | Lightweight journal support pin |
CA2889542A1 (en) * | 2014-04-30 | 2015-10-30 | Ge Avio S.R.L. | Epyciclic transmission provided with a lubricating system |
FR3036763B1 (fr) * | 2015-05-27 | 2017-05-26 | Hispano-Suiza | Reducteur a train epicycloidal |
US10443708B2 (en) | 2015-06-23 | 2019-10-15 | United Technologies Corporation | Journal bearing for rotating gear carrier |
ITUB20152131A1 (it) * | 2015-07-13 | 2017-01-13 | Fondazione St Italiano Tecnologia | Riduttore di velocita' rotazionale |
US10066734B2 (en) | 2015-12-07 | 2018-09-04 | United Technologies Corporation | Gear driven gas turbine engine assembly |
US10006520B2 (en) * | 2016-08-31 | 2018-06-26 | General Electric Company | System for regulating stresses in ring gears |
FR3071024B1 (fr) * | 2017-09-12 | 2021-02-19 | Safran Trans Systems | Pivot pour palier lisse |
DE102017008675A1 (de) * | 2017-09-15 | 2019-03-21 | Rolls-Royce Deutschland Ltd & Co Kg | Planetengetriebevorrichtung für eine Strömungmaschine |
FR3073915B1 (fr) * | 2017-11-17 | 2019-10-25 | Safran Transmission Systems | Cage de reducteur de vitesse a train planetaire ou epicycloidal de turbomachine |
DE102018106564B4 (de) * | 2018-03-20 | 2024-03-21 | Rolls-Royce Deutschland Ltd & Co Kg | Planetengetriebe, Gasturbinentriebwerk mit Planetengetriebe und Verfahren zum Herstellen eines Planetengetriebes |
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DE102018106864A1 (de) * | 2018-03-22 | 2019-09-26 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zum Zusammenbau eines Planetengetriebes, ein Planetenträger und ein Flugzeugtriebwerk |
US10683773B2 (en) | 2018-05-25 | 2020-06-16 | Pratt & Whitney Canada Corp. | Planetary gearbox having compliant journal bearings |
FR3084428B1 (fr) * | 2018-07-26 | 2020-09-11 | Safran Trans Systems | Cage de reducteur de vitesse a train planetaire ou epicycloidal de turbomachine |
DE102018122535B4 (de) * | 2018-09-14 | 2024-03-21 | Rolls-Royce Deutschland Ltd & Co Kg | Planetengetriebevorrichtung und Gasturbinentriebwerk |
US10851671B2 (en) | 2019-03-29 | 2020-12-01 | Pratt & Whitney Canada Corp. | Bending stiffening feature used for compliant journal bearing |
GB202005025D0 (en) | 2020-04-06 | 2020-05-20 | Rolls Royce Plc | Gearboxes for aircraft gas turbine engines |
GB202005028D0 (en) | 2020-04-06 | 2020-05-20 | Rolls Royce Plc | Gearboxes for aircraft gas turbine engines |
GB202005033D0 (en) | 2020-04-06 | 2020-05-20 | Rolls Royce Plc | Gearboxes for aircraft gas turbine engines |
GB202005022D0 (en) * | 2020-04-06 | 2020-05-20 | Rolls Royce Plc | Gearboxes for aircraft gas turbine engines |
DE102021115337A1 (de) | 2021-06-14 | 2022-12-15 | Rolls-Royce Deutschland Ltd & Co Kg | Planetengetriebe eines Gasturbinetriebwerkes |
FR3125568B1 (fr) * | 2021-07-24 | 2023-07-14 | Safran Trans Systems | Pivot pour réducteur mécanique de turbomachine |
US11680525B2 (en) * | 2021-08-20 | 2023-06-20 | Pratt & Whitney Canada Corp. | Lubricant filter for a turbine engine |
DE102021122413A1 (de) | 2021-08-30 | 2023-03-02 | Rolls-Royce Deutschland Ltd & Co Kg | Planetengetriebe und Verfahren zum Betreiben eines Planetengetriebes sowie Gasturbinentriebwerk mit wenigstens zwei Zentralwellen und mit einem Planetengetriebe |
FR3132554B1 (fr) * | 2022-02-08 | 2024-03-22 | Safran Trans Systems | Reducteur de vitesse pour une turbomachine d’aeronef |
FR3139607A1 (fr) * | 2022-09-09 | 2024-03-15 | Safran Transmission Systems | Palier lisse pour un reducteur mecanique de turbomachine d’aeronef |
FR3143080A1 (fr) * | 2022-12-09 | 2024-06-14 | Safran Transmission Systems | Couronne pour un reducteur mecanique d’aeronef |
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-
1991
- 1991-11-12 IT ITTO910871A patent/IT1250861B/it active IP Right Grant
-
1992
- 1992-11-12 US US07/975,414 patent/US5391125A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5391125A (en) | 1995-02-21 |
ITTO910871A0 (it) | 1991-11-12 |
ITTO910871A1 (it) | 1993-05-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
0001 | Granted | ||
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19971127 |