DE60116987D1 - Vorrichtung zum Zentrieren eines Rohres in einer Turbinenwelle - Google Patents

Vorrichtung zum Zentrieren eines Rohres in einer Turbinenwelle

Info

Publication number
DE60116987D1
DE60116987D1 DE60116987T DE60116987T DE60116987D1 DE 60116987 D1 DE60116987 D1 DE 60116987D1 DE 60116987 T DE60116987 T DE 60116987T DE 60116987 T DE60116987 T DE 60116987T DE 60116987 D1 DE60116987 D1 DE 60116987D1
Authority
DE
Germany
Prior art keywords
shaft
centering
expand
sheath
component
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
DE60116987T
Other languages
English (en)
Other versions
DE60116987T2 (de
Inventor
Christophe Emile Galand
Jean-Luc Soupizon
Jean-Bernard Vache
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 Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE60116987D1 publication Critical patent/DE60116987D1/de
Application granted granted Critical
Publication of DE60116987T2 publication Critical patent/DE60116987T2/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • A Measuring Device Byusing Mechanical Method (AREA)
  • Ultra Sonic Daignosis Equipment (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
DE60116987T 2000-11-30 2001-11-29 Vorrichtung zum Zentrieren eines Rohres in einer Turbinenwelle Expired - Lifetime DE60116987T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0015473A FR2817289B1 (fr) 2000-11-30 2000-11-30 Dispositif de centrage d'un tube dans un arbre de turbine
FR0015473 2000-11-30

Publications (2)

Publication Number Publication Date
DE60116987D1 true DE60116987D1 (de) 2006-04-13
DE60116987T2 DE60116987T2 (de) 2006-09-21

Family

ID=8857050

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60116987T Expired - Lifetime DE60116987T2 (de) 2000-11-30 2001-11-29 Vorrichtung zum Zentrieren eines Rohres in einer Turbinenwelle

Country Status (11)

Country Link
US (1) US7004725B2 (de)
EP (1) EP1225322B1 (de)
JP (1) JP4043944B2 (de)
CN (1) CN1250868C (de)
AT (1) ATE317060T1 (de)
CA (1) CA2430285C (de)
DE (1) DE60116987T2 (de)
ES (1) ES2253342T3 (de)
FR (1) FR2817289B1 (de)
RU (1) RU2249702C2 (de)
WO (1) WO2002044538A2 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2872218B1 (fr) * 2004-06-29 2006-09-29 Snecma Moteurs Sa Tube de degazage pour arbre basse-pression de turbomachine
US7197877B2 (en) * 2004-08-04 2007-04-03 Siemens Power Generation, Inc. Support system for a pilot nozzle of a turbine engine
FR2888897B1 (fr) * 2005-07-21 2007-10-19 Snecma Dispositif d'amortissement des vibrations d'un anneau de retention axiale des aubes de soufflante d'une turbomachine
GB0701609D0 (en) 2007-01-29 2007-03-07 Boc Group Plc Vacuum pump
EP1970533A1 (de) * 2007-03-12 2008-09-17 Siemens Aktiengesellschaft Turbine mit mindestens einem Rotor bestehend aus Rotorscheiben und einen Zuganker
EP1970532A1 (de) * 2007-03-12 2008-09-17 Siemens Aktiengesellschaft Läufer einer thermischen Strömungsmaschine sowie Gasturbine
FR2926604B1 (fr) * 2008-01-23 2010-03-26 Snecma Centrage d'une piece a l'interieur d'un arbre de rotor dans une turbomachine
US8215919B2 (en) * 2008-02-22 2012-07-10 Hamilton Sundstrand Corporation Curved tooth coupling for a miniature gas turbine engine
BR112012024037B1 (pt) * 2010-03-26 2020-09-01 Snecma Tubo dito de desgaseificação para a orientação de um fluxo de gás em um turborreator, turborreator e método de montagem de um tubo dito de desgaseificação para a orientação de um fluxo de gás dentro de um eixo rotativo oco de um turborreator
CN102005855B (zh) * 2010-12-16 2012-11-14 中国人民解放军91872部队 中空轴电机
CN102720542B (zh) * 2012-06-11 2014-09-03 东方电气集团东方汽轮机有限公司 一种汽轮机转子
FR2997996B1 (fr) 2012-11-12 2015-01-09 Snecma Support de tube d'evacuation d'air dans une turbomachine
FR3008135B1 (fr) * 2013-07-08 2017-05-26 Snecma Centrage d'une piece a l'interieur d'un arbre de rotor dans une turbomachine
KR101509382B1 (ko) * 2014-01-15 2015-04-07 두산중공업 주식회사 댐핑 클램프를 구비한 가스 터빈
JP6183564B2 (ja) * 2014-11-14 2017-08-23 株式会社Ihi ジェットエンジン
JP6455179B2 (ja) * 2015-01-26 2019-01-23 株式会社Ihi センターベントチューブ調芯機構及びセンターベントチューブ支持装置
FR3058480B1 (fr) * 2016-11-07 2018-12-07 Safran Aircraft Engines Support assurant une liaison complete entre un arbre turbine et un tube de degazage d'un turboreacteur
US11162457B2 (en) * 2017-08-11 2021-11-02 General Electric Company Turbine fan system and method
EP3693559A4 (de) 2017-10-02 2021-01-27 Ihi Corporation Stützvorrichtung für ein zentrales entlüftungsrohr für ein turbofantriebwerk
FR3094031B1 (fr) * 2019-03-18 2021-05-14 Safran Aircraft Engines Ensemble pour une turbomachine
FR3126459A1 (fr) * 2021-08-31 2023-03-03 Safran Aircraft Engines Turboréacteur d’aéronef comprenant un arbre de turboréacteur et un raidisseur d’arbre.

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2222494A (en) * 1938-12-14 1940-11-19 Scovill Manufacturing Co Slotted spider member
US2554368A (en) * 1944-08-23 1951-05-22 United Aircraft Corp Turbine rotor cooling
US3556676A (en) * 1968-08-28 1971-01-19 Igor Konstantinovich Gorbunov Liquid-cooling system of gas turbine rotors
US4872767A (en) * 1985-04-03 1989-10-10 General Electric Company Bearing support
US5603574A (en) * 1987-05-29 1997-02-18 Kmc, Inc. Fluid dampened support having variable stiffness and damping
US5073036A (en) * 1990-03-30 1991-12-17 Rockwell International Corporation Hydrostatic bearing for axial/radial support
DE19757945B4 (de) * 1997-12-27 2006-11-30 Alstom Rotor für thermische Turbomaschine

Also Published As

Publication number Publication date
RU2249702C2 (ru) 2005-04-10
US7004725B2 (en) 2006-02-28
CA2430285C (fr) 2008-10-07
EP1225322A1 (de) 2002-07-24
ES2253342T3 (es) 2006-06-01
CN1395649A (zh) 2003-02-05
US20040025494A1 (en) 2004-02-12
EP1225322B1 (de) 2006-02-01
WO2002044538A3 (fr) 2002-08-01
CN1250868C (zh) 2006-04-12
DE60116987T2 (de) 2006-09-21
CA2430285A1 (fr) 2002-06-06
FR2817289A1 (fr) 2002-05-31
JP2004514841A (ja) 2004-05-20
FR2817289B1 (fr) 2003-01-31
WO2002044538A2 (fr) 2002-06-06
ATE317060T1 (de) 2006-02-15
JP4043944B2 (ja) 2008-02-06

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Legal Events

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8364 No opposition during term of opposition