JP2004052755A5 - - Google Patents
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- Publication number
- JP2004052755A5 JP2004052755A5 JP2003136744A JP2003136744A JP2004052755A5 JP 2004052755 A5 JP2004052755 A5 JP 2004052755A5 JP 2003136744 A JP2003136744 A JP 2003136744A JP 2003136744 A JP2003136744 A JP 2003136744A JP 2004052755 A5 JP2004052755 A5 JP 2004052755A5
- Authority
- JP
- Japan
- 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
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Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/196,454 US6742987B2 (en) | 2002-07-16 | 2002-07-16 | Cradle mounted turbine nozzle |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2004052755A JP2004052755A (ja) | 2004-02-19 |
JP2004052755A5 true JP2004052755A5 (ja) | 2006-06-22 |
JP4341294B2 JP4341294B2 (ja) | 2009-10-07 |
Family
ID=29780183
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2003136744A Expired - Fee Related JP4341294B2 (ja) | 2002-07-16 | 2003-05-15 | クレードル支持されたタービンノズル |
Country Status (3)
Country | Link |
---|---|
US (1) | US6742987B2 (ja) |
EP (1) | EP1382801A3 (ja) |
JP (1) | JP4341294B2 (ja) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7186085B2 (en) * | 2004-11-18 | 2007-03-06 | General Electric Company | Multiform film cooling holes |
US7249934B2 (en) | 2005-08-31 | 2007-07-31 | General Electric Company | Pattern cooled turbine airfoil |
US8038389B2 (en) | 2006-01-04 | 2011-10-18 | General Electric Company | Method and apparatus for assembling turbine nozzle assembly |
US7722314B2 (en) * | 2006-06-22 | 2010-05-25 | General Electric Company | Methods and systems for assembling a turbine |
US7798768B2 (en) * | 2006-10-25 | 2010-09-21 | Siemens Energy, Inc. | Turbine vane ID support |
FR2908153B1 (fr) * | 2006-11-07 | 2011-05-13 | Snecma | Dispositif d'accrochage d'un distributeur (8) d'une turbine, turbine les comportant, et moteur d'aeronef en etant equipe |
FR2911933B1 (fr) * | 2007-01-26 | 2009-05-01 | Snecma Sa | Dispositif d'assemblage de deux ensembles, par exemple pour stator de turbomachine |
FR2935428B1 (fr) * | 2008-08-26 | 2015-06-26 | Snecma | Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe |
US8226360B2 (en) * | 2008-10-31 | 2012-07-24 | General Electric Company | Crenelated turbine nozzle |
FR2944554B1 (fr) * | 2009-04-16 | 2014-06-13 | Snecma | Turbine haute-pression de turbomachine |
US8226361B2 (en) * | 2009-07-08 | 2012-07-24 | General Electric Company | Composite article and support frame assembly |
US8206096B2 (en) * | 2009-07-08 | 2012-06-26 | General Electric Company | Composite turbine nozzle |
FR2981980B1 (fr) * | 2011-10-26 | 2016-01-22 | Snecma | Procede de montage d'un aubage fixe d'une turbomachine, carter et turbomachine comportant au moins un aubage fixe monte sur ce carter |
FR3002272A1 (fr) * | 2013-02-19 | 2014-08-22 | Snecma | Secteur de distributeur a anti-rotation pour secteur adjacent |
US10662814B2 (en) * | 2014-11-03 | 2020-05-26 | Raytheon Technologies Corporation | Stator shroud systems |
EP3075959A1 (en) | 2015-03-31 | 2016-10-05 | Alstom Technology Ltd | Gas turbine comprising a combustor with a combustor outlet and a first row of rocking vanes |
US20170051619A1 (en) * | 2015-08-18 | 2017-02-23 | General Electric Company | Cmc nozzles with split endwalls for gas turbine engines |
US10570760B2 (en) * | 2017-04-13 | 2020-02-25 | General Electric Company | Turbine nozzle with CMC aft band |
FR3108140B1 (fr) | 2020-03-10 | 2022-05-13 | Safran Aircraft Engines | Module de turbomachine equipe d’un rotor de machine electrique |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2061396B (en) * | 1979-10-24 | 1983-05-18 | Rolls Royce | Turbine blade tip clearance control |
FR2473621A1 (fr) | 1980-01-10 | 1981-07-17 | Snecma | Aube de distributeur de turbine |
GB2170867B (en) | 1985-02-12 | 1988-12-07 | Rolls Royce | Improvements in or relating to gas turbine engines |
US4815933A (en) * | 1987-11-13 | 1989-03-28 | The United States Of America As Represented By The Secretary Of The Air Force | Nozzle flange attachment and sealing arrangement |
US5211536A (en) * | 1991-05-13 | 1993-05-18 | General Electric Company | Boltless turbine nozzle/stationary seal mounting |
US5271714A (en) * | 1992-07-09 | 1993-12-21 | General Electric Company | Turbine nozzle support arrangement |
US5372476A (en) | 1993-06-18 | 1994-12-13 | General Electric Company | Turbine nozzle support assembly |
US5839878A (en) * | 1996-09-30 | 1998-11-24 | United Technologies Corporation | Gas turbine stator vane |
US6095750A (en) * | 1998-12-21 | 2000-08-01 | General Electric Company | Turbine nozzle assembly |
ITMI991206A1 (it) * | 1999-05-31 | 2000-12-01 | Nuovo Pignone Spa | Dispositivo di supporto e bloccaggio per ugelli di uno stadio ad altapressione in turbine a gas |
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2002
- 2002-07-16 US US10/196,454 patent/US6742987B2/en not_active Expired - Fee Related
-
2003
- 2003-05-15 JP JP2003136744A patent/JP4341294B2/ja not_active Expired - Fee Related
- 2003-05-15 EP EP03253026A patent/EP1382801A3/en not_active Withdrawn