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DE60112696D1 - Kompensation des Axialschubs eines Turbofans mittels eines Reduktionsgetriebes - Google Patents

Kompensation des Axialschubs eines Turbofans mittels eines Reduktionsgetriebes

Info

Publication number
DE60112696D1
DE60112696D1 DE60112696T DE60112696T DE60112696D1 DE 60112696 D1 DE60112696 D1 DE 60112696D1 DE 60112696 T DE60112696 T DE 60112696T DE 60112696 T DE60112696 T DE 60112696T DE 60112696 D1 DE60112696 D1 DE 60112696D1
Authority
DE
Germany
Prior art keywords
compensation
reduction gearbox
axial thrust
turbo fan
turbo
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
DE60112696T
Other languages
English (en)
Other versions
DE60112696T2 (de
Inventor
Samuel Raymond Ger Becquerelle
Daniel Victor Marcel Ville
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.)
Safran Transmission Systems SAS
Original Assignee
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Publication of DE60112696D1 publication Critical patent/DE60112696D1/de
Application granted granted Critical
Publication of DE60112696T2 publication Critical patent/DE60112696T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/12—Combinations with mechanical gearing
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S74/00—Machine element or mechanism
    • Y10S74/05—Gas turbine with gearing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Retarders (AREA)
DE60112696T 2000-12-07 2001-12-06 Kompensation des Axialschubs eines Turbofans mittels eines Reduktionsgetriebes Expired - Lifetime DE60112696T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0015892A FR2817912B1 (fr) 2000-12-07 2000-12-07 Reducteur reprenant les efforts axiaux generes par la soufflante d'un turboreacteur
FR0015892 2000-12-07

Publications (2)

Publication Number Publication Date
DE60112696D1 true DE60112696D1 (de) 2005-09-22
DE60112696T2 DE60112696T2 (de) 2006-06-08

Family

ID=8857349

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60112696T Expired - Lifetime DE60112696T2 (de) 2000-12-07 2001-12-06 Kompensation des Axialschubs eines Turbofans mittels eines Reduktionsgetriebes

Country Status (7)

Country Link
US (1) US6622473B2 (de)
EP (1) EP1213445B1 (de)
JP (1) JP3990564B2 (de)
CA (1) CA2364124C (de)
DE (1) DE60112696T2 (de)
FR (1) FR2817912B1 (de)
RU (1) RU2219361C2 (de)

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CN101395406B (zh) * 2006-03-06 2013-03-13 埃克森美孚上游研究公司 双端齿轮流体驱动起动器
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RU2347929C2 (ru) * 2007-02-26 2009-02-27 Открытое акционерное общество "Авиадвигатель" Газотурбинный двигатель сверхвысокой степени двухконтурности с биротативным вентилятором
RU2346172C2 (ru) * 2007-02-28 2009-02-10 Открытое акционерное общество "Авиадвигатель" Редуктор газотурбинного двигателя
US8127529B2 (en) * 2007-03-29 2012-03-06 United Technologies Corporation Variable area fan nozzle and thrust reverser
US8074440B2 (en) * 2007-08-23 2011-12-13 United Technologies Corporation Gas turbine engine with axial movable fan variable area nozzle
US9701415B2 (en) 2007-08-23 2017-07-11 United Technologies Corporation Gas turbine engine with axial movable fan variable area nozzle
US10167813B2 (en) * 2007-08-23 2019-01-01 United Technologies Corporation Gas turbine engine with fan variable area nozzle to reduce fan instability
US9494084B2 (en) 2007-08-23 2016-11-15 United Technologies Corporation Gas turbine engine with fan variable area nozzle for low fan pressure ratio
US20140157752A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157756A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157753A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157754A1 (en) 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140157755A1 (en) * 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US20140165534A1 (en) * 2007-09-21 2014-06-19 United Technologies Corporation Gas turbine engine compressor arrangement
US8511055B2 (en) 2009-05-22 2013-08-20 United Technologies Corporation Apparatus and method for providing damper liquid in a gas turbine
US8517672B2 (en) * 2010-02-23 2013-08-27 General Electric Company Epicyclic gearbox
US8845277B2 (en) 2010-05-24 2014-09-30 United Technologies Corporation Geared turbofan engine with integral gear and bearing supports
EP3659495B1 (de) 2011-09-13 2022-12-14 Dose Medical Corporation Intraokularer physiologischer sensor
US12331691B2 (en) 2011-12-27 2025-06-17 Rtx Corporation Gas turbine engine compressor arrangement
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
US9080461B2 (en) * 2012-02-02 2015-07-14 Pratt & Whitney Canada Corp. Fan and boost joint
FR2991421B1 (fr) * 2012-05-30 2015-07-31 Snecma Reducteur a train epicycloidal avec axes de satellites montes sur roulements
US9730638B2 (en) 2013-03-13 2017-08-15 Glaukos Corporation Intraocular physiological sensor
FR3016189B1 (fr) * 2014-01-07 2018-09-28 Safran Aircraft Engines Dispositif de reduction epicycloidal pour l'entrainement en rotation des ensembles de pales d'une turbomachine a reducteur
CN107407378B (zh) 2015-02-13 2021-08-20 伊顿康明斯自动变速技术有限责任公司 具有花键的双中间轴变速器
FR3034140B1 (fr) 2015-03-26 2018-09-07 Safran Aircraft Engines Turbomachine d’aeronef a reducteur planetaire ou epicycloidal
US9771871B2 (en) * 2015-07-07 2017-09-26 United Technologies Corporation FBO torque reducing feature in fan shaft
US9909451B2 (en) * 2015-07-09 2018-03-06 General Electric Company Bearing assembly for supporting a rotor shaft of a gas turbine engine
GB201516570D0 (en) * 2015-09-18 2015-11-04 Rolls Royce Plc A Shafting Arrangement
FR3051842B1 (fr) 2016-05-24 2019-06-14 Safran Helicopter Engines Turbomachine d'aeronef a reducteur epicycloidal
EP3296552B1 (de) * 2016-09-20 2019-06-05 Rolls-Royce Deutschland Ltd & Co KG Gasturbinenmotor mit einer getriebefanbaugruppe
EP3296525B1 (de) 2016-09-20 2019-11-27 Rolls-Royce Deutschland Ltd & Co KG Gasturbinenmotor mit getriebe-fan
EP3296524B1 (de) 2016-09-20 2019-02-27 Rolls-Royce Deutschland Ltd & Co KG Gasturbinenmotor mit getriebefananordnung
EP3296540B1 (de) 2016-09-20 2019-01-23 Rolls-Royce Deutschland Ltd & Co KG Gasturbinenmotor mit getriebefananordnung
US10954813B2 (en) * 2017-08-18 2021-03-23 Rolls-Royce Deutschland Ltd & Co Kg Planetary gearbox system and method for operating a planetary gearbox system
EP3444495A1 (de) 2017-08-18 2019-02-20 Rolls-Royce Deutschland Ltd & Co KG Mechanische kupplungsvorrichtung und verfahren zum betrieb einer mechanischen kupplungsvorrichtung
EP3587774B1 (de) 2018-06-27 2025-05-07 Rolls-Royce plc Gasturbine
FR3086348B1 (fr) * 2018-09-21 2020-12-04 Safran Aircraft Engines Turboreacteur a reducteur
FR3086343B1 (fr) 2018-09-24 2020-09-04 Safran Aircraft Engines Turbomachine a reducteur pour un aeronef
US11092020B2 (en) 2018-10-18 2021-08-17 Raytheon Technologies Corporation Rotor assembly for gas turbine engines
RU2717606C1 (ru) * 2018-11-22 2020-03-24 Аслан Солтамбекович Тедтоев Силовая установка летательного аппарата вертикального взлета и посадки, а также летательный аппарат вертикального взлета и посадки, содержащий указанную силовую установку
RU2717409C1 (ru) * 2018-11-30 2020-03-23 Аслан Солтамбекович Тедтоев Вертикально ориентированный турбореактивный двигатель силовой установки летательного аппарата вертикального взлета и посадки, силовая установка летательного аппарата вертикального взлета и посадки, а также летательный аппарат вертикального взлета и посадки
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Also Published As

Publication number Publication date
US20020069637A1 (en) 2002-06-13
EP1213445A1 (de) 2002-06-12
FR2817912B1 (fr) 2003-01-17
US6622473B2 (en) 2003-09-23
JP3990564B2 (ja) 2007-10-17
JP2002235604A (ja) 2002-08-23
CA2364124A1 (fr) 2002-06-07
DE60112696T2 (de) 2006-06-08
EP1213445B1 (de) 2005-08-17
FR2817912A1 (fr) 2002-06-14
RU2219361C2 (ru) 2003-12-20
CA2364124C (fr) 2010-04-13

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Legal Events

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8364 No opposition during term of opposition