JP2007064216A5 - - Google Patents

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Publication number
JP2007064216A5
JP2007064216A5 JP2006227434A JP2006227434A JP2007064216A5 JP 2007064216 A5 JP2007064216 A5 JP 2007064216A5 JP 2006227434 A JP2006227434 A JP 2006227434A JP 2006227434 A JP2006227434 A JP 2006227434A JP 2007064216 A5 JP2007064216 A5 JP 2007064216A5
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JP
Japan
Prior art keywords
journal
module
shaft
heating
temperature
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JP2006227434A
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English (en)
Japanese (ja)
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JP4861770B2 (ja
JP2007064216A (ja
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Priority claimed from FR0552577A external-priority patent/FR2890110B1/fr
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Publication of JP2007064216A publication Critical patent/JP2007064216A/ja
Publication of JP2007064216A5 publication Critical patent/JP2007064216A5/ja
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Publication of JP4861770B2 publication Critical patent/JP4861770B2/ja
Active legal-status Critical Current
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JP2006227434A 2005-08-26 2006-08-24 ターボ機械組み立て方法 Active JP4861770B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0552577 2005-08-26
FR0552577A FR2890110B1 (fr) 2005-08-26 2005-08-26 Procede d'assemblage d'une turbomachine

Publications (3)

Publication Number Publication Date
JP2007064216A JP2007064216A (ja) 2007-03-15
JP2007064216A5 true JP2007064216A5 (enExample) 2009-09-17
JP4861770B2 JP4861770B2 (ja) 2012-01-25

Family

ID=36354013

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006227434A Active JP4861770B2 (ja) 2005-08-26 2006-08-24 ターボ機械組み立て方法

Country Status (7)

Country Link
US (1) US7594324B2 (enExample)
EP (1) EP1757777B1 (enExample)
JP (1) JP4861770B2 (enExample)
CA (1) CA2557104C (enExample)
DE (1) DE602006003149D1 (enExample)
FR (1) FR2890110B1 (enExample)
RU (1) RU2415275C2 (enExample)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2889981B1 (fr) 2005-08-26 2007-11-02 Snecma Dispositif de chauffage d'une piece cylindrique, utilisation dans l'assemblage d'un palier inter-arbres dans une turbomachine.
US8347500B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitney Canada Corp. Method of assembly and disassembly of a gas turbine mid turbine frame
US20100132377A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Fabricated itd-strut and vane ring for gas turbine engine
US8061969B2 (en) * 2008-11-28 2011-11-22 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8091371B2 (en) * 2008-11-28 2012-01-10 Pratt & Whitney Canada Corp. Mid turbine frame for gas turbine engine
US8099962B2 (en) * 2008-11-28 2012-01-24 Pratt & Whitney Canada Corp. Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine
US20100132371A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8245518B2 (en) * 2008-11-28 2012-08-21 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8347635B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitey Canada Corp. Locking apparatus for a radial locator for gas turbine engine mid turbine frame
FR2944558B1 (fr) * 2009-04-17 2014-05-02 Snecma Moteur a turbine a gaz double corps pourvu d'un palier de turbine bp supplementaire.
CN102330605B (zh) * 2011-09-05 2013-06-26 沈阳黎明航空发动机(集团)有限责任公司 一种转子与前后支承组合装配的重型燃机装配方法
FR2990239B1 (fr) * 2012-05-02 2015-10-30 Snecma Procede de devissage avant d'un ecrou de liaison dans un turboreacteur a double corps, outillage de devissage
FR2990238B1 (fr) * 2012-05-02 2015-10-30 Snecma Procede de devissage arriere d'un ecrou de liaison dans un turboreacteur a double corps, outillage de devissage
FR2990242B1 (fr) 2012-05-02 2014-06-13 Snecma Procede de demontage d'un turboreacteur
FR3024493B1 (fr) * 2014-07-29 2019-04-19 Safran Aircraft Engines Element de turbomachine comprenant un joint d'etancheite entre un stator et un rotor, et procede de montage
FR3024492B1 (fr) 2014-07-29 2019-08-23 Safran Aircraft Engines Element comprenant un stator et un rotor de turbomachine avec un joint d'etancheite et test de ce joint
WO2016198216A1 (en) * 2015-05-07 2016-12-15 Nuovo Pignone Tecnologie Srl Assembly/disassembly apparatus for flanged mechanical device and assembly/disassembly method for flanged mechanical devices
RU2659694C2 (ru) * 2016-12-28 2018-07-03 Акционерное общество "ОДК-Авиадвигатель" Силовая свободная турбина
FR3068078B1 (fr) 2017-06-27 2021-06-25 Safran Aircraft Engines Dispositif et procede pour l'assemblage d'une turbomachine
FR3068390B1 (fr) * 2017-06-28 2019-07-19 Safran Aircraft Engines Dispositif pour l'assemblage d'une turbomachine, et procede utilisant le dispositif
FR3072137B1 (fr) * 2017-10-06 2020-07-24 Safran Aircraft Engines Dispositif pour l'assemblage d'une turbomachine, et procede utilisant le dispositif
CN109268211B (zh) * 2018-11-29 2019-10-11 河北思达歌数据科技投资有限公司 一种自适应风力发电装置
CN109209786B (zh) * 2018-11-29 2019-10-29 绍兴市亚索新能源科技有限公司 一种风力发电机组故障检测方法
CN111946460B (zh) * 2020-08-10 2022-08-05 中国人民解放军第五七一九工厂 用于航空发动机风扇组合件装配的导正装置及装配方法
CN115415786A (zh) * 2022-08-30 2022-12-02 北京动力机械研究所 一种人机协同的涡扇发动机核心机装配系统与装配方法

Family Cites Families (18)

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Publication number Priority date Publication date Assignee Title
US2756561A (en) * 1952-01-18 1956-07-31 Rolls Royce Gas turbine engine with axial-flow compressor and bearing means for supporting the compressor rotor
US2862356A (en) * 1954-07-16 1958-12-02 Rolls Royce Bearing arrangements for gas-turbine engines
US3909085A (en) * 1973-09-08 1975-09-30 Rolls Royce 1971 Ltd Preloaded bearings
SU549307A1 (ru) * 1975-06-20 1977-03-05 Украинский Заочный Политехнический Институт Способ соединени деталей типа вал-втулка
US4167809A (en) * 1977-11-10 1979-09-18 General Motors Corporation Hot air arbor extractor
US4283096A (en) * 1978-04-21 1981-08-11 United Technologies Corporation Intershaft bearing
FR2515734A1 (fr) * 1981-11-05 1983-05-06 Snecma Systeme d'ajustement du centrage d'une roue de turbomachine et turbomachine munie de moyens permettant l'application dudit systeme
FR2518650B1 (fr) * 1981-12-22 1986-05-30 Snecma Dispositif de pilotage des jeux d'un palier inter-arbres de turbomachine multi-corps
US4685286A (en) * 1984-05-02 1987-08-11 United Technologies Corporation Method of disassembly for a gas turbine engine
GB2177160A (en) * 1985-07-04 1987-01-14 Prime Mover Maintenance Limite Servicing gas turbines
FR2644843B1 (fr) * 1989-03-23 1991-05-24 Snecma Procede de montage de la turbine basse pression sur le corps haute pression d'une turbomachine a palier inter-arbres et outillages pour la mise en oeuvre du procede
US5201796A (en) * 1991-10-15 1993-04-13 United Technologies Corporation Gas turbine engine arrangement
US6491497B1 (en) * 2000-09-22 2002-12-10 General Electric Company Method and apparatus for supporting rotor assemblies during unbalances
JP2002303157A (ja) * 2001-04-05 2002-10-18 Ishikawajima Harima Heavy Ind Co Ltd 差動軸受構造
EP1310323B1 (de) * 2001-11-12 2011-03-30 Franz Haimer Maschinenbau KG Schrumpfvorrichtung für einen Werkzeughalter
US6910863B2 (en) * 2002-12-11 2005-06-28 General Electric Company Methods and apparatus for assembling a bearing assembly
FR2857708B1 (fr) * 2003-07-15 2005-09-23 Snecma Moteurs Dispositif perfectionne de fixation d'un arbre de moteur sur un support de palier
FR2858649B1 (fr) * 2003-08-05 2005-09-23 Snecma Moteurs Turbine basse-pression de turbomachine

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