JP2005240799A5 - - Google Patents

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Publication number
JP2005240799A5
JP2005240799A5 JP2005017775A JP2005017775A JP2005240799A5 JP 2005240799 A5 JP2005240799 A5 JP 2005240799A5 JP 2005017775 A JP2005017775 A JP 2005017775A JP 2005017775 A JP2005017775 A JP 2005017775A JP 2005240799 A5 JP2005240799 A5 JP 2005240799A5
Authority
JP
Japan
Prior art keywords
bearing
turbojet
drive shaft
attached
fan rotor
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.)
Granted
Application number
JP2005017775A
Other languages
English (en)
Japanese (ja)
Other versions
JP4541170B2 (ja
JP2005240799A (ja
Filing date
Publication date
Priority claimed from FR0401146A external-priority patent/FR2866069A1/fr
Application filed filed Critical
Publication of JP2005240799A publication Critical patent/JP2005240799A/ja
Publication of JP2005240799A5 publication Critical patent/JP2005240799A5/ja
Application granted granted Critical
Publication of JP4541170B2 publication Critical patent/JP4541170B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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JP2005017775A 2004-02-06 2005-01-26 第１および第２の軸受により支持される駆動シャフトに固定されるファンを有するターボファンエンジン Expired - Lifetime JP4541170B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0401146A FR2866069A1 (fr) 2004-02-06 2004-02-06 Turboreacteur a soufflante solidaire d'un arbre d'entrainement supporte par un premier et un deuxieme paliers

Publications (3)

Publication Number Publication Date
JP2005240799A JP2005240799A (ja) 2005-09-08
JP2005240799A5 true JP2005240799A5 (enExample) 2007-11-01
JP4541170B2 JP4541170B2 (ja) 2010-09-08

Family

ID=34673905

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005017775A Expired - Lifetime JP4541170B2 (ja) 2004-02-06 2005-01-26 第１および第２の軸受により支持される駆動シャフトに固定されるファンを有するターボファンエンジン

Country Status (11)

Country Link
US (1) US7322181B2 (enExample)
EP (1) EP1561907B1 (enExample)
JP (1) JP4541170B2 (enExample)
CN (1) CN1707070A (enExample)
BR (1) BRPI0500246B8 (enExample)
CA (1) CA2495979C (enExample)
DE (1) DE602005000003T2 (enExample)
ES (1) ES2259438T3 (enExample)
FR (1) FR2866069A1 (enExample)
RU (1) RU2361100C2 (enExample)
UA (1) UA86575C2 (enExample)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2866069A1 (fr) * 2004-02-06 2005-08-12 Snecma Moteurs Turboreacteur a soufflante solidaire d'un arbre d'entrainement supporte par un premier et un deuxieme paliers
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
US7100358B2 (en) * 2004-07-16 2006-09-05 Pratt & Whitney Canada Corp. Turbine exhaust case and method of making
US7730715B2 (en) * 2006-05-15 2010-06-08 United Technologies Corporation Fan frame
US7950236B2 (en) * 2006-09-11 2011-05-31 Pratt & Whitney Canada Corp. Exhaust duct and tail cone attachment of aircraft engines
FR2923543B1 (fr) * 2007-11-13 2009-12-18 Snecma Fixation d'un palier supportant un rotor sur une turbomachine
FR2925123A1 (fr) * 2007-12-14 2009-06-19 Snecma Sa Etancheite de fixation de support de palier dans une turbomachine
US8845277B2 (en) 2010-05-24 2014-09-30 United Technologies Corporation Geared turbofan engine with integral gear and bearing supports
FR2960907B1 (fr) * 2010-06-02 2012-07-27 Snecma Palier de roulement pour turboreacteur d'aeronef equipe de moyens ameliores de retention axiale de sa bague exterieure
FR2965298B1 (fr) * 2010-09-28 2012-09-28 Snecma Moteur a turbine a gaz comprenant des moyens de retention axiale d'une soufflante dudit moteur
US9995174B2 (en) 2010-10-12 2018-06-12 United Technologies Corporation Planetary gear system arrangement with auxiliary oil system
FR2966200B1 (fr) * 2010-10-13 2016-02-12 Turbomeca Architecture de turbine a gaz, en particulier de turbomoteur, sans palier dans la zone inter-turbines
FR2966208B1 (fr) * 2010-10-13 2012-12-28 Snecma Boitier de liaison entre un arbre d'entrainement de soufflante de moteur et un palier de roulement
GB2494178B (en) * 2011-09-02 2013-07-31 Rolls Royce Plc A catcher ring assembly
SG11201404964XA (en) * 2012-03-23 2014-10-30 United Technologies Corp Planetary gear system arrangement with auxiliary oil system
US10001028B2 (en) 2012-04-23 2018-06-19 General Electric Company Dual spring bearing support housing
US9115598B2 (en) 2012-06-05 2015-08-25 United Technologies Corporation Front bearing support for a fan drive gear system
FR2992702B1 (fr) 2012-06-28 2014-07-04 Eurocopter France Dispositif d'accouplement par aboutement d'un arbre de transmission supercritique, pour l'entrainement d'un rotor de giravion notamment
FR3013760B1 (fr) * 2013-11-26 2015-12-25 Snecma Dispositif pour le centrage et le guidage en rotation d'un arbre de turbomachine comprenant des moyens ameliores de retention de bague exterieure de palier
GB201704984D0 (en) * 2017-03-29 2017-05-10 Rolls Royce Plc Mitigation of effects of fan blade off in a gas turbine engine
FR3071546B1 (fr) 2017-09-25 2019-09-13 Safran Aircraft Engines Retention axiale de l'arbre de soufflante dans un moteur a turbine a gaz
US11028778B2 (en) 2018-09-27 2021-06-08 Pratt & Whitney Canada Corp. Engine with start assist
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
FR3118989B1 (fr) * 2021-01-21 2023-03-03 Safran Aircraft Engines Couronne de ventilation du support de palier arrière d'une turbomachine d'aéronef
RU210513U1 (ru) * 2022-01-25 2022-04-18 Публичное Акционерное Общество "Одк-Сатурн" Устройство для защиты газотурбинного двигателя при обрыве лопатки компрессора низкого давления

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1152115A (en) * 1967-10-06 1969-05-14 Rolls Royce Rotary Bladed Fluid Flow Machine, e.g. a Fan Lift Engine
SU1354834A1 (ru) * 1984-07-25 1990-11-15 Предприятие П/Я А-1469 Опора ротора двухкаскадного газотурбинного двигател
SU1471675A1 (ru) * 1986-09-29 1997-01-10 Н.К. Рязанцев Газотурбинный двигатель периодического горения
US5237817A (en) * 1992-02-19 1993-08-24 Sundstrand Corporation Gas turbine engine having low cost speed reduction drive
US5433584A (en) * 1994-05-05 1995-07-18 Pratt & Whitney Canada, Inc. Bearing support housing
FR2773586B1 (fr) * 1998-01-09 2000-02-11 Snecma Turbomachine a freinage mutuel d'arbres concentriques
US6331078B1 (en) * 1998-12-23 2001-12-18 United Technologies Corporation Turbine engine bearing
US6491497B1 (en) * 2000-09-22 2002-12-10 General Electric Company Method and apparatus for supporting rotor assemblies during unbalances
FR2817912B1 (fr) * 2000-12-07 2003-01-17 Hispano Suiza Sa Reducteur reprenant les efforts axiaux generes par la soufflante d'un turboreacteur
US6428269B1 (en) * 2001-04-18 2002-08-06 United Technologies Corporation Turbine engine bearing support
FR2831624A1 (fr) * 2001-10-31 2003-05-02 Snecma Moteurs Systeme decoupleur pour l'arbre d'une soufflante de turboreacteur
US6877950B2 (en) * 2001-11-29 2005-04-12 Pratt & Whitney Canada Corp. Method and device for minimizing oil consumption in a gas turbine engine
US6619030B1 (en) * 2002-03-01 2003-09-16 General Electric Company Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
US6684626B1 (en) * 2002-07-30 2004-02-03 General Electric Company Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
US6846158B2 (en) * 2002-09-06 2005-01-25 General Electric Company Method and apparatus for varying the critical speed of a shaft
US7097412B2 (en) * 2003-02-14 2006-08-29 United Technologies Corporation Turbine engine bearing support
US7370467B2 (en) * 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
FR2866069A1 (fr) * 2004-02-06 2005-08-12 Snecma Moteurs Turboreacteur a soufflante solidaire d'un arbre d'entrainement supporte par un premier et un deuxieme paliers
FR2866073B1 (fr) * 2004-02-11 2006-07-28 Snecma Moteurs Turboreacteur ayant deux soufflantes contrarotatives solidaires d'un compresseur a basse pression contrarotatif
FR2871517B1 (fr) * 2004-06-11 2006-09-01 Snecma Moteurs Sa Turbomachine avec moyens de retenue axiale du rotor
FR2874238B1 (fr) * 2004-08-12 2006-12-01 Snecma Moteurs Sa Turbomachine a soufflantes contrarotatives

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