DE69401357T2 - Zahnradantriebs-system für einen schaufelantrieb - Google Patents

Zahnradantriebs-system für einen schaufelantrieb

Info

Publication number
DE69401357T2
DE69401357T2 DE69401357T DE69401357T DE69401357T2 DE 69401357 T2 DE69401357 T2 DE 69401357T2 DE 69401357 T DE69401357 T DE 69401357T DE 69401357 T DE69401357 T DE 69401357T DE 69401357 T2 DE69401357 T2 DE 69401357T2
Authority
DE
Germany
Prior art keywords
drive
shovel
gear
drive system
gear drive
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.)
Expired - Lifetime
Application number
DE69401357T
Other languages
English (en)
Other versions
DE69401357D1 (de
Inventor
Albert Mckibbin
Jon Burno
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69401357D1 publication Critical patent/DE69401357D1/de
Application granted granted Critical
Publication of DE69401357T2 publication Critical patent/DE69401357T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/20Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H1/00Toothed gearings for conveying rotary motion
    • F16H1/28Toothed gearings for conveying rotary motion with gears having orbital motion
    • F16H1/2809Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet-wheels
    • F16H1/2836Toothed 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H1/00Toothed gearings for conveying rotary motion
    • F16H1/28Toothed gearings for conveying rotary motion with gears having orbital motion
    • F16H1/2809Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet-wheels
    • F16H1/2827Toothed 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 planet carrier, e.g. relative to its shaft
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
DE69401357T 1993-06-11 1994-06-08 Zahnradantriebs-system für einen schaufelantrieb Expired - Lifetime DE69401357T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/075,827 US5466198A (en) 1993-06-11 1993-06-11 Geared drive system for a bladed propulsor
PCT/US1994/006507 WO1994029614A1 (en) 1993-06-11 1994-06-08 Geared drive system for a bladed propulsor

Publications (2)

Publication Number Publication Date
DE69401357D1 DE69401357D1 (de) 1997-02-13
DE69401357T2 true DE69401357T2 (de) 1997-07-24

Family

ID=22128237

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69401357T Expired - Lifetime DE69401357T2 (de) 1993-06-11 1994-06-08 Zahnradantriebs-system für einen schaufelantrieb

Country Status (5)

Country Link
US (1) US5466198A (de)
EP (1) EP0701669B1 (de)
JP (1) JP3497509B2 (de)
DE (1) DE69401357T2 (de)
WO (1) WO1994029614A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015118669B4 (de) 2015-10-30 2023-03-16 Rolls-Royce Deutschland Ltd & Co Kg Strahltriebwerk mit einem Bläser und mit einer Turbineneinrichtung

Families Citing this family (223)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE29609794U1 (de) * 1996-06-03 1996-08-22 Aerodyn Gmbh Getriebe-Generator-Kombination
FI108959B (fi) 1998-06-18 2002-04-30 Valmet Voimansiirto Oy Tuulivoimalan planeettavaihteisto
DE19844843B4 (de) * 1998-09-30 2006-02-09 Mtu Aero Engines Gmbh Planetengetriebe
US6223616B1 (en) * 1999-12-22 2001-05-01 United Technologies Corporation Star gear system with lubrication circuit and lubrication method therefor
US6663530B2 (en) * 2001-12-14 2003-12-16 Pratt & Whitney Canada Corp. Zero twist carrier
US6964155B2 (en) * 2002-12-30 2005-11-15 United Technologies Corporation Turbofan engine comprising an spicyclic transmission having bearing journals
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
DE10334459A1 (de) * 2003-07-29 2005-03-17 Zf Friedrichshafen Ag Führungsscheibenverbund eines Planetenträgers für ein Planetengetriebe
US7104918B2 (en) * 2003-07-29 2006-09-12 Pratt & Whitney Canada Corp. Compact epicyclic gear carrier
US7883314B2 (en) * 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
EP1831520B1 (de) 2004-12-01 2009-02-25 United Technologies Corporation Tip-turbinentriebwerk und entsprechendes betriebsverfahren
WO2006059989A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine support structure
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
WO2006060001A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Fan rotor assembly for a tip turbine engine
US8083030B2 (en) * 2004-12-01 2011-12-27 United Technologies Corporation Gearbox lubrication supply system for a tip engine
EP1831530B1 (de) * 2004-12-01 2009-02-25 United Technologies Corporation Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
WO2006059969A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
DE602004023769D1 (de) 2004-12-01 2009-12-03 United Technologies Corp Gestapelte ringförmige bauteile für turbinenmotoren
EP1828547B1 (de) 2004-12-01 2011-11-30 United Technologies Corporation Turbofantriebwerk mit einer Mehrzahl von einzeln steuerbaren Einlassleitschaufeln und zugehöriges Steuerverfahren
EP1831519B1 (de) 2004-12-01 2010-08-04 United Technologies Corporation Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
US7631480B2 (en) * 2004-12-01 2009-12-15 United Technologies Corporation Modular tip turbine engine
WO2006060012A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
EP1828545A2 (de) 2004-12-01 2007-09-05 United Technologies Corporation Ringförmiger turbinenringrotor
US7874163B2 (en) * 2004-12-01 2011-01-25 United Technologies Corporation Starter generator system for a tip turbine engine
DE602004016059D1 (de) 2004-12-01 2008-10-02 United Technologies Corp Tip-turbinentriebwerk mit wärmetauscher
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
EP1825112B1 (de) * 2004-12-01 2013-10-23 United Technologies Corporation Freigetragene tipturbinentriebwerk
US7607286B2 (en) * 2004-12-01 2009-10-27 United Technologies Corporation Regenerative turbine blade and vane cooling for a tip turbine engine
US8757959B2 (en) * 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
US7980054B2 (en) 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
EP1825177B1 (de) 2004-12-01 2012-01-25 United Technologies Corporation Aufblasbares ablassventil für eine turbomaschine und verfahren zur steuerung von ablassluft
WO2006059996A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
WO2006059975A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Peripheral combustor for tip turbine engine
US8468795B2 (en) 2004-12-01 2013-06-25 United Technologies Corporation Diffuser aspiration for a tip turbine engine
WO2006060005A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
US7887296B2 (en) * 2004-12-01 2011-02-15 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
EP1825117B1 (de) * 2004-12-01 2012-06-13 United Technologies Corporation Turbinentriebwerk mit von einem differentialgetriebe angetriebenem fan und verdichter
US9845727B2 (en) * 2004-12-01 2017-12-19 United Technologies Corporation Tip turbine engine composite tailcone
WO2006059992A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Inducer for a fan blade of a tip turbine engine
DE602004032186D1 (de) * 2004-12-01 2011-05-19 United Technologies Corp Turbinenschaufelgruppe eines Fanrotors sowie Verfahren zur Montage einer solchen Gruppe
WO2006059981A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Hydraulic seal for a gearbox of a tip turbine engine
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
US8033092B2 (en) * 2004-12-01 2011-10-11 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006060000A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
US7959406B2 (en) * 2004-12-01 2011-06-14 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
WO2006059987A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Particle separator for tip turbine engine
EP1825126B1 (de) 2004-12-01 2011-02-16 United Technologies Corporation Übergangskanal mit mitteln zur strömungsvektorbeeinflussung bei einer gasturbine
US8365511B2 (en) * 2004-12-01 2013-02-05 United Technologies Corporation Tip turbine engine integral case, vane, mount and mixer
WO2006060013A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
US7937927B2 (en) * 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
WO2006062497A1 (en) * 2004-12-04 2006-06-15 United Technologies Corporation Tip turbine engine mount
US8267826B2 (en) 2005-03-15 2012-09-18 United Technologies Corporation Uninterruptible oil supply in planetary system
US9194255B2 (en) 2006-07-05 2015-11-24 United Technologies Corporation Oil baffle for gas turbine fan drive gear system
US7926260B2 (en) * 2006-07-05 2011-04-19 United Technologies Corporation Flexible shaft for gas turbine engine
US8585538B2 (en) * 2006-07-05 2013-11-19 United Technologies Corporation Coupling system for a star gear train in a gas turbine engine
US8667688B2 (en) * 2006-07-05 2014-03-11 United Technologies Corporation Method of assembly for gas turbine fan drive gear system
US7704178B2 (en) 2006-07-05 2010-04-27 United Technologies Corporation Oil baffle for gas turbine fan drive gear system
US9976437B2 (en) 2006-08-15 2018-05-22 United Technologies Corporation Epicyclic gear train
US10107231B2 (en) 2006-08-15 2018-10-23 United Technologies Corporation Gas turbine engine with geared architecture
US8708863B2 (en) 2006-08-15 2014-04-29 United Technologies Corporation Epicyclic gear train
US8858388B2 (en) 2006-08-15 2014-10-14 United Technologies Corporation Gas turbine engine gear train
US8753243B2 (en) * 2006-08-15 2014-06-17 United Technologies Corporation Ring gear mounting arrangement with oil scavenge scheme
US8939864B2 (en) 2006-08-15 2015-01-27 United Technologies Corporation Gas turbine engine lubrication
US20120213628A1 (en) 2006-08-15 2012-08-23 Mccune Michael E Gas turbine engine with geared architecture
US8104262B2 (en) 2006-10-12 2012-01-31 United Technologies Corporation Dual function cascade integrated variable area fan nozzle and thrust reverser
US7849668B2 (en) * 2006-10-25 2010-12-14 United Technologies Corporation Rotor brake and windmilling lubrication system for geared turbofan engine
US20080273961A1 (en) 2007-03-05 2008-11-06 Rosenkrans William E Flutter sensing and control system for a gas turbine engine
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
US9701415B2 (en) 2007-08-23 2017-07-11 United Technologies Corporation Gas turbine engine with axial movable fan variable area nozzle
US9957918B2 (en) 2007-08-28 2018-05-01 United Technologies Corporation Gas turbine engine front architecture
US20140157754A1 (en) 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US8205432B2 (en) * 2007-10-03 2012-06-26 United Technologies Corporation Epicyclic gear train for turbo fan engine
US10151248B2 (en) 2007-10-03 2018-12-11 United Technologies Corporation Dual fan gas turbine engine and gear train
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
EP2238346B1 (de) * 2007-12-20 2011-05-25 Vestas Wind Systems A/s Planetengetriebestufe für ein windturbinengetriebe, windturbinengetriebe und windturbine
US8348803B2 (en) * 2008-04-17 2013-01-08 Kawasaki Jukogyo Kabushiki Kaisha Planetary reduction gear apparatus
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
DE102008063044B4 (de) * 2008-12-23 2012-01-05 Aerodyn Engineering Gmbh Planetengetriebe
US9885313B2 (en) 2009-03-17 2018-02-06 United Technologes Corporation Gas turbine engine bifurcation located fan variable area nozzle
CA2682454C (en) 2009-04-14 2013-11-26 Kawasaki Jukogyo Kabushiki Kaisha Planetary reduction gear apparatus
US8689538B2 (en) 2009-09-09 2014-04-08 The Boeing Company Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan
JP4975081B2 (ja) * 2009-10-30 2012-07-11 川崎重工業株式会社 遊星歯車減速装置
US8672801B2 (en) * 2009-11-30 2014-03-18 United Technologies Corporation Mounting system for a planetary gear train in a gas turbine engine
IT1401662B1 (it) 2010-08-27 2013-08-02 Nuova Pignone S R L Dispositivo espansore multistadio assiale con ingranaggi, sistema e metodo.
US9995174B2 (en) 2010-10-12 2018-06-12 United Technologies Corporation Planetary gear system arrangement with auxiliary oil system
US8813469B2 (en) 2010-10-12 2014-08-26 United Technologies Corporation Planetary gear system arrangement with auxiliary oil system
US10605167B2 (en) 2011-04-15 2020-03-31 United Technologies Corporation Gas turbine engine front center body architecture
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
US9239012B2 (en) 2011-06-08 2016-01-19 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US9631558B2 (en) 2012-01-03 2017-04-25 United Technologies Corporation Geared architecture for high speed and small volume fan drive turbine
US9410608B2 (en) 2011-06-08 2016-08-09 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US9909505B2 (en) 2011-07-05 2018-03-06 United Technologies Corporation Efficient, low pressure ratio propulsor for gas turbine engines
US9506422B2 (en) 2011-07-05 2016-11-29 United Technologies Corporation Efficient, low pressure ratio propulsor for gas turbine engines
US9938898B2 (en) 2011-07-29 2018-04-10 United Technologies Corporation Geared turbofan bearing arrangement
ITTO20111007A1 (it) * 2011-11-03 2013-05-04 Avio Spa Rotismo epicicloidale
EP2610461B1 (de) 2011-12-30 2019-10-23 United Technologies Corporation Turbinenmotor
US9416677B2 (en) 2012-01-10 2016-08-16 United Technologies Corporation Gas turbine engine forward bearing compartment architecture
US20130186058A1 (en) 2012-01-24 2013-07-25 William G. Sheridan Geared turbomachine fan and compressor rotation
US10400629B2 (en) 2012-01-31 2019-09-03 United Technologies Corporation Gas turbine engine shaft bearing configuration
US9394852B2 (en) 2012-01-31 2016-07-19 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
US8869508B2 (en) 2012-01-31 2014-10-28 United Technologies Corporation Gas turbine engine variable area fan nozzle control
US10415468B2 (en) 2012-01-31 2019-09-17 United Technologies Corporation Gas turbine engine buffer system
US20130192198A1 (en) 2012-01-31 2013-08-01 Lisa I. Brilliant Compressor flowpath
US20130192251A1 (en) 2012-01-31 2013-08-01 Peter M. Munsell Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
US8863491B2 (en) 2012-01-31 2014-10-21 United Technologies Corporation Gas turbine engine shaft bearing configuration
US20150345426A1 (en) 2012-01-31 2015-12-03 United Technologies Corporation Geared turbofan gas turbine engine architecture
US8720306B2 (en) 2012-01-31 2014-05-13 United Technologies Corporation Turbine engine gearbox
US9169781B2 (en) 2012-01-31 2015-10-27 United Technologies Corporation Turbine engine gearbox
US20130192191A1 (en) 2012-01-31 2013-08-01 Frederick M. Schwarz Gas turbine engine with high speed low pressure turbine section and bearing support features
US8935913B2 (en) 2012-01-31 2015-01-20 United Technologies Corporation Geared turbofan gas turbine engine architecture
US10113434B2 (en) 2012-01-31 2018-10-30 United Technologies Corporation Turbine blade damper seal
US20150192070A1 (en) 2012-01-31 2015-07-09 United Technologies Corporation Geared turbofan gas turbine engine architecture
US20130192240A1 (en) 2012-01-31 2013-08-01 Peter M. Munsell Buffer system for a gas turbine engine
US9835052B2 (en) 2012-01-31 2017-12-05 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section and bearing support features
US10724431B2 (en) 2012-01-31 2020-07-28 Raytheon Technologies Corporation Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
US10287914B2 (en) 2012-01-31 2019-05-14 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section and bearing support features
US10107191B2 (en) 2012-02-29 2018-10-23 United Technologies Corporation Geared gas turbine engine with reduced fan noise
EP3855003B1 (de) * 2012-03-23 2022-09-28 Raytheon Technologies Corporation Planetengetriebesystemanordnung mit hilfsölsystem
US8961112B2 (en) 2012-03-26 2015-02-24 United Technologies Corporation Torque frame bushing arrangement for gas turbine engine fan drive gear system
US8790075B2 (en) 2012-03-30 2014-07-29 United Technologies Corporation Gas turbine engine geared architecture axial retention arrangement
US10125693B2 (en) 2012-04-02 2018-11-13 United Technologies Corporation Geared turbofan engine with power density range
US8585536B2 (en) 2012-04-02 2013-11-19 Hamilton Sundstrand Corporation Gear carrier frame
US10138809B2 (en) 2012-04-02 2018-11-27 United Technologies Corporation Geared turbofan engine with a high ratio of thrust to turbine volume
US20130255275A1 (en) * 2012-04-02 2013-10-03 Frederick M. Schwarz Geared turbofan engine with power density range
US20130269479A1 (en) * 2012-04-11 2013-10-17 General Electric Company Gearbox and support apparatus for gearbox carrier
JP5915352B2 (ja) * 2012-04-19 2016-05-11 トヨタ自動車株式会社 変速機を備えたターボプロップ/ファン型ジェットエンジン
US8484942B1 (en) 2012-05-30 2013-07-16 United Technologies Corporation Planetary gear system arrangement with auxiliary oil system
US8572943B1 (en) 2012-05-31 2013-11-05 United Technologies Corporation Fundamental gear system architecture
US20150308351A1 (en) 2012-05-31 2015-10-29 United Technologies Corporation Fundamental gear system architecture
US9267389B2 (en) 2012-06-05 2016-02-23 United Technologies Corporation Geared architecture carrier torque frame assembly
US8727935B2 (en) 2012-07-30 2014-05-20 United Technologies Corporation Fan drive gear system torque frame pin retainer
US9328818B2 (en) * 2012-09-21 2016-05-03 United Technologies Corporation Gear carrier flex mount lubrication
US8807916B2 (en) 2012-09-27 2014-08-19 United Technologies Corporation Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
US8753065B2 (en) 2012-09-27 2014-06-17 United Technologies Corporation Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
WO2014051672A1 (en) 2012-09-28 2014-04-03 United Technologies Corporation Split-zone flow metering t-tube
CA2886359C (en) 2012-10-08 2018-11-27 United Technologies Corporation Geared turbine engine with relatively lightweight propulsor module
EP2909460A4 (de) 2012-10-09 2016-07-20 United Technologies Corp Turbogebläsemotor mit verbesserter bedienbarkeit mit veränderlichen verdichterabschnittleitschaufeln
US9932933B2 (en) 2012-12-20 2018-04-03 United Technologies Corporation Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US9920653B2 (en) 2012-12-20 2018-03-20 United Technologies Corporation Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US8678743B1 (en) 2013-02-04 2014-03-25 United Technologies Corporation Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
US10436120B2 (en) 2013-02-06 2019-10-08 United Technologies Corporation Exhaust nozzle for an elongated gear turbofan with high bypass ratio
US9863326B2 (en) 2013-03-12 2018-01-09 United Technologies Corporation Flexible coupling for geared turbine engine
US10605172B2 (en) 2013-03-14 2020-03-31 United Technologies Corporation Low noise turbine for geared gas turbine engine
US11719161B2 (en) 2013-03-14 2023-08-08 Raytheon Technologies Corporation Low noise turbine for geared gas turbine engine
US10113481B2 (en) 2013-03-15 2018-10-30 United Technologies Corporation Turbofan engine bearing and gearbox arrangement
US10724479B2 (en) 2013-03-15 2020-07-28 United Technologies Corporation Thrust efficient turbofan engine
WO2015012923A2 (en) 2013-05-09 2015-01-29 United Technologies Corporation Turbofan engine front section
US10316758B2 (en) 2013-05-09 2019-06-11 United Technologies Corporation Turbofan engine front section
US9745862B2 (en) 2013-08-21 2017-08-29 United Technologies Corporation Reduced misalignment gear system
US8857149B1 (en) 2013-08-26 2014-10-14 United Technologies Corporation Torque connector lubrication scuppers
CN108423161A (zh) 2013-09-05 2018-08-21 空中客车营运有限公司 用于飞行器的起落架的驱动系统以及飞行器的起落架
JP6509868B2 (ja) 2013-09-05 2019-05-08 エアバス オペレーションズ リミテッドAirbus Operations Limited 着陸装置駆動システムのフレキシブルインターフェース
WO2015088619A2 (en) 2013-10-16 2015-06-18 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
EP3063385A4 (de) 2013-11-01 2017-07-12 United Technologies Corporation Getriebeturbolüfteranordnung mit geteilter kernleistung
US10502163B2 (en) 2013-11-01 2019-12-10 United Technologies Corporation Geared turbofan arrangement with core split power ratio
US8869504B1 (en) 2013-11-22 2014-10-28 United Technologies Corporation Geared turbofan engine gearbox arrangement
US10161409B2 (en) 2013-12-30 2018-12-25 United Technologies Corporation Fan drive gear system including a two-piece fan shaft with lubricant transfer leakage recapture
CN103742377A (zh) * 2014-01-07 2014-04-23 丁兴龙 定向力发生装置
EP3097324B1 (de) 2014-01-20 2019-04-03 United Technologies Corporation Leichte lagerzapfenstützbolzen
EP3108118B1 (de) 2014-02-19 2019-09-18 United Technologies Corporation Gasturbinenmotor-tragfläche
EP3108107B1 (de) 2014-02-19 2023-10-11 Raytheon Technologies Corporation Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterschaufeln
US10605259B2 (en) 2014-02-19 2020-03-31 United Technologies Corporation Gas turbine engine airfoil
WO2015175056A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015126774A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108119B1 (de) 2014-02-19 2023-10-04 RTX Corporation Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterlaufschaufeln
US10557477B2 (en) 2014-02-19 2020-02-11 United Technologies Corporation Gas turbine engine airfoil
US10570916B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
WO2015126454A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108121B1 (de) 2014-02-19 2023-09-06 Raytheon Technologies Corporation Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterschaufeln
WO2015126449A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
US10280843B2 (en) 2014-03-07 2019-05-07 United Technologies Corporation Geared turbofan with integral front support and carrier
US9879608B2 (en) 2014-03-17 2018-01-30 United Technologies Corporation Oil loss protection for a fan drive gear system
US11448123B2 (en) 2014-06-13 2022-09-20 Raytheon Technologies Corporation Geared turbofan architecture
US9976490B2 (en) 2014-07-01 2018-05-22 United Technologies Corporation Geared gas turbine engine with oil deaerator
US10060289B2 (en) 2014-07-29 2018-08-28 United Technologies Corporation Geared gas turbine engine with oil deaerator and air removal
US10221771B2 (en) 2014-09-24 2019-03-05 United Technologies Corporation Fan drive gear system
GB201417505D0 (en) 2014-10-03 2014-11-19 Rolls Royce Deutschland A gas turbine architecture
GB201417504D0 (en) * 2014-10-03 2014-11-19 Rolls Royce Deutschland A gas turbine architecture
US9879694B2 (en) 2015-02-03 2018-01-30 United Technologies Corporation Turbo-compressor with geared turbofan
US11067005B2 (en) 2015-02-03 2021-07-20 Raytheon Technologies Corporation Fan drive gear system
US9915225B2 (en) 2015-02-06 2018-03-13 United Technologies Corporation Propulsion system arrangement for turbofan gas turbine engine
US9470093B2 (en) 2015-03-18 2016-10-18 United Technologies Corporation Turbofan arrangement with blade channel variations
US10371168B2 (en) 2015-04-07 2019-08-06 United Technologies Corporation Modal noise reduction for gas turbine engine
US9874145B2 (en) 2015-04-27 2018-01-23 United Technologies Corporation Lubrication system for gas turbine engines
US10458270B2 (en) 2015-06-23 2019-10-29 United Technologies Corporation Roller bearings for high ratio geared turbofan engine
GB2542338B (en) 2015-09-10 2018-11-21 Rolls Royce Plc Gear trains
US20170089218A1 (en) * 2015-09-25 2017-03-30 General Electric Company Double row cylindrical roller bearing with high length to diameter ratio rollers
US10415429B2 (en) * 2015-09-25 2019-09-17 General Electric Company Planet gearbox with cylindrical roller bearing with high density roller packing
US10233773B2 (en) 2015-11-17 2019-03-19 United Technologies Corporation Monitoring system for non-ferrous metal particles
US10508562B2 (en) 2015-12-01 2019-12-17 United Technologies Corporation Geared turbofan with four star/planetary gear reduction
US10066734B2 (en) 2015-12-07 2018-09-04 United Technologies Corporation Gear driven gas turbine engine assembly
GB2548140B (en) * 2016-03-10 2019-05-29 Rolls Royce Plc Transmission system
FR3052213B1 (fr) * 2016-06-07 2018-05-18 Safran Transmission Systems Procede d'assemblage d'un porte-satellites
EP3263952B1 (de) * 2016-06-29 2019-11-27 Rolls-Royce Deutschland Ltd & Co KG Trägerstruktur für ein planetengetriebe, planetengetriebe und turbomaschine mit einem planetengetriebe
US10669948B2 (en) 2017-01-03 2020-06-02 Raytheon Technologies Corporation Geared turbofan with non-epicyclic gear reduction system
IT201700029839A1 (it) * 2017-03-17 2018-09-17 Ge Avio Srl Porta-satelliti per un rotismo epicicloidale e rotismo epicicloidale provvisto di tale porta-satelliti
US10738646B2 (en) 2017-06-12 2020-08-11 Raytheon Technologies Corporation Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section
US10662879B2 (en) 2017-08-08 2020-05-26 Pratt & Whitney Canada Corp. Epicyclic gear stage
FR3073915B1 (fr) 2017-11-17 2019-10-25 Safran Transmission Systems Cage de reducteur de vitesse a train planetaire ou epicycloidal de turbomachine
US10724445B2 (en) 2018-01-03 2020-07-28 Raytheon Technologies Corporation Method of assembly for fan drive gear system with rotating carrier
US10927944B2 (en) 2018-01-26 2021-02-23 Pratt & Whitney Canada Corp. Compact, twist controlled planet carrier and epicyclic gear train having same
US10760677B2 (en) 2018-01-31 2020-09-01 Pratt & Whitney Canada Corp. Epicyclic gear train with balanced carrier stiffness
DE102018106564B4 (de) * 2018-03-20 2024-03-21 Rolls-Royce Deutschland Ltd & Co Kg Planetengetriebe, Gasturbinentriebwerk mit Planetengetriebe und Verfahren zum Herstellen eines Planetengetriebes
DE102018106864A1 (de) * 2018-03-22 2019-09-26 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zum Zusammenbau eines Planetengetriebes, ein Planetenträger und ein Flugzeugtriebwerk
FR3084428B1 (fr) * 2018-07-26 2020-09-11 Safran Trans Systems Cage de reducteur de vitesse a train planetaire ou epicycloidal de turbomachine
US11092020B2 (en) 2018-10-18 2021-08-17 Raytheon Technologies Corporation Rotor assembly for gas turbine engines
DE102018222162A1 (de) * 2018-12-18 2020-06-18 Rolls-Royce Deutschland Ltd & Co Kg Belüftungs- und Löschvorrichtung für ein Gasturbinentriebwerk
US11105395B2 (en) * 2019-10-23 2021-08-31 Pratt & Whitney Canada Corp. Planetary gear assembly and method of operating same
US11781506B2 (en) 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines
EP4056469B1 (de) 2021-03-11 2023-05-24 Leonardo S.p.A. Schwebeflug-fähiges luftfahrzeug
FR3124565B1 (fr) 2021-06-24 2023-07-14 Safran Trans Systems Porte-satellites pour un reducteur de vitesse de turbomachine d’aeronef
FR3124564B1 (fr) 2021-06-24 2023-07-21 Safran Trans Systems Porte-satellites pour un reducteur de vitesse de turbomachine d’aeronef
US11754000B2 (en) 2021-07-19 2023-09-12 Rtx Corporation High and low spool configuration for a gas turbine engine
US11719245B2 (en) 2021-07-19 2023-08-08 Raytheon Technologies Corporation Compressor arrangement for a gas turbine engine
US11814968B2 (en) 2021-07-19 2023-11-14 Rtx Corporation Gas turbine engine with idle thrust ratio
FR3139612A1 (fr) * 2022-09-09 2024-03-15 Safran Transmission Systems Porte-satellites pour un reducteur de vitesse d’une turbomachine d’aeronef

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE289318C (de) *
US2547877A (en) * 1945-10-15 1951-04-03 Packard Motor Car Co Bearing support for gears
US2591743A (en) * 1948-11-23 1952-04-08 Gen Electric Cage construction for planetary gearing
GB691775A (en) * 1951-11-23 1953-05-20 Gen Electric Improvements in and relating to planetary gearing
US3227006A (en) * 1963-01-14 1966-01-04 Bell Aerospace Corp Power transmitting gear train
US3315547A (en) * 1963-09-26 1967-04-25 Simmering Graz Pauker Ag Epicyclic gears
GB1101131A (en) * 1964-02-07 1968-01-31 Nat Res Dev Improvements relating to gears
US3635103A (en) * 1968-12-24 1972-01-18 Siai Marchetti Spa Planetary reduction gearing
GB1367343A (en) * 1972-04-27 1974-09-18 Secr Defence Gearing
DE2619996C3 (de) * 1976-05-06 1979-03-22 Karl-Heinz Dr.-Ing. 6333 Braunfels Vatterott Leistungsverzweigendes Stirnradgetriebe mit Lastausgleich
US4430909A (en) * 1981-08-03 1984-02-14 Paccar Inc. Dual output stage for internal planetary gear winches
DE3267847D1 (en) * 1982-01-18 1986-01-16 Mavilor Syst Sa Transmission with orbital motion gears
JPS58163848A (ja) * 1982-03-24 1983-09-28 Ishikawajima Harima Heavy Ind Co Ltd 遊星歯車の軸芯調整装置

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015118669B4 (de) 2015-10-30 2023-03-16 Rolls-Royce Deutschland Ltd & Co Kg Strahltriebwerk mit einem Bläser und mit einer Turbineneinrichtung

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JPH08511605A (ja) 1996-12-03
DE69401357D1 (de) 1997-02-13
US5466198A (en) 1995-11-14
WO1994029614A1 (en) 1994-12-22
JP3497509B2 (ja) 2004-02-16
EP0701669A1 (de) 1996-03-20

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