JP2005009496A5 - - Google Patents

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Publication number
JP2005009496A5
JP2005009496A5 JP2004180420A JP2004180420A JP2005009496A5 JP 2005009496 A5 JP2005009496 A5 JP 2005009496A5 JP 2004180420 A JP2004180420 A JP 2004180420A JP 2004180420 A JP2004180420 A JP 2004180420A JP 2005009496 A5 JP2005009496 A5 JP 2005009496A5
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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
Application number
JP2004180420A
Other languages
Japanese (ja)
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JP4597588B2 (ja
JP2005009496A (ja
Filing date
Publication date
Priority claimed from US10/465,328 external-priority patent/US7108479B2/en
Application filed filed Critical
Publication of JP2005009496A publication Critical patent/JP2005009496A/ja
Publication of JP2005009496A5 publication Critical patent/JP2005009496A5/ja
Application granted granted Critical
Publication of JP4597588B2 publication Critical patent/JP4597588B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2004180420A 2003-06-19 2004-06-18 タービンノズルに冷却流体を供給するための方法及び装置 Expired - Fee Related JP4597588B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/465,328 US7108479B2 (en) 2003-06-19 2003-06-19 Methods and apparatus for supplying cooling fluid to turbine nozzles

Publications (3)

Publication Number Publication Date
JP2005009496A JP2005009496A (ja) 2005-01-13
JP2005009496A5 true JP2005009496A5 (enExample) 2007-08-02
JP4597588B2 JP4597588B2 (ja) 2010-12-15

Family

ID=33418226

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004180420A Expired - Fee Related JP4597588B2 (ja) 2003-06-19 2004-06-18 タービンノズルに冷却流体を供給するための方法及び装置

Country Status (4)

Country Link
US (1) US7108479B2 (enExample)
EP (1) EP1489265B1 (enExample)
JP (1) JP4597588B2 (enExample)
CN (1) CN100359142C (enExample)

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US6929445B2 (en) 2003-10-22 2005-08-16 General Electric Company Split flow turbine nozzle
US20070151257A1 (en) * 2006-01-05 2007-07-05 Maier Mark S Method and apparatus for enabling engine turn down
FR2914017B1 (fr) * 2007-03-20 2011-07-08 Snecma Dispositif d'etancheite pour un circuit de refroidissement, carter inter-turbine en etant equipe et turboreacteur les comportant
US8100633B2 (en) * 2008-03-11 2012-01-24 United Technologies Corp. Cooling air manifold splash plates and gas turbines engine systems involving such splash plates
US8092146B2 (en) * 2009-03-26 2012-01-10 Pratt & Whitney Canada Corp. Active tip clearance control arrangement for gas turbine engine
US8371810B2 (en) * 2009-03-26 2013-02-12 General Electric Company Duct member based nozzle for turbine
GB2469490B (en) * 2009-04-16 2012-03-07 Rolls Royce Plc Turbine casing cooling
JP4841678B2 (ja) * 2010-04-15 2011-12-21 川崎重工業株式会社 ガスタービンのタービン静翼
US9011079B2 (en) * 2012-01-09 2015-04-21 General Electric Company Turbine nozzle compartmentalized cooling system
US8864445B2 (en) * 2012-01-09 2014-10-21 General Electric Company Turbine nozzle assembly methods
US20130283814A1 (en) * 2012-04-25 2013-10-31 General Electric Company Turbine cooling system
WO2014009074A1 (de) * 2012-07-12 2014-01-16 Siemens Aktiengesellschaft Turbinenschaufel für eine gasturbine
US9927123B2 (en) * 2013-10-24 2018-03-27 United Technologies Corporation Fluid transport system having divided transport tube
DE112013007581B4 (de) 2013-11-08 2025-08-28 General Electric Technology Gmbh Turbomaschinenabgasgehäuse
US10001013B2 (en) * 2014-03-06 2018-06-19 General Electric Company Turbine rotor blades with platform cooling arrangements
GB201408543D0 (en) * 2014-05-14 2014-06-25 Rolls Royce Plc Distributor device for cooling air within an engine
US10436113B2 (en) * 2014-09-19 2019-10-08 United Technologies Corporation Plate for metering flow
US20160102566A1 (en) * 2014-10-13 2016-04-14 Pw Power Systems, Inc. Power turbine air strut
US10260356B2 (en) * 2016-06-02 2019-04-16 General Electric Company Nozzle cooling system for a gas turbine engine
US10739002B2 (en) * 2016-12-19 2020-08-11 General Electric Company Fluidic nozzle assembly for a turbine engine
EP3574207B1 (en) * 2017-01-24 2020-05-13 Voith Patent GmbH Runner for a hydraulic turbine or pump
US10876407B2 (en) * 2017-02-16 2020-12-29 General Electric Company Thermal structure for outer diameter mounted turbine blades
US11480057B2 (en) * 2017-10-24 2022-10-25 Raytheon Technologies Corporation Airfoil cooling circuit
US10648351B2 (en) 2017-12-06 2020-05-12 United Technologies Corporation Gas turbine engine cooling component
US11131212B2 (en) 2017-12-06 2021-09-28 Raytheon Technologies Corporation Gas turbine engine cooling component
US10738637B2 (en) * 2017-12-22 2020-08-11 Raytheon Technologies Corporation Airflow deflector and assembly
US10837293B2 (en) 2018-07-19 2020-11-17 General Electric Company Airfoil with tunable cooling configuration
US10968746B2 (en) * 2018-09-14 2021-04-06 Raytheon Technologies Corporation Serpentine turn cover for gas turbine stator vane assembly
US20200362704A1 (en) 2019-05-17 2020-11-19 Solar Turbines Incorporated Nozzle segment
US11698005B2 (en) * 2020-02-07 2023-07-11 Raytheon Technologies Corporation Flow diverter for mid-turbine frame cooling air delivery
US20220316352A1 (en) * 2021-03-31 2022-10-06 Raytheon Technologies Corporation Flow diverter for mid-turbine frame cooling air delivery
GB202216827D0 (en) * 2022-11-11 2022-12-28 Rolls Royce Plc A method of manufacturing a turbine component

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Publication number Priority date Publication date Assignee Title
US2896906A (en) * 1956-03-26 1959-07-28 William J Durkin Turbine cooling air metering system
US4126405A (en) 1976-12-16 1978-11-21 General Electric Company Turbine nozzle
US4251185A (en) 1978-05-01 1981-02-17 Caterpillar Tractor Co. Expansion control ring for a turbine shroud assembly
US4355952A (en) * 1979-06-29 1982-10-26 Westinghouse Electric Corp. Combustion turbine vane assembly
US4551064A (en) * 1982-03-05 1985-11-05 Rolls-Royce Limited Turbine shroud and turbine shroud assembly
US4492517A (en) 1983-01-06 1985-01-08 General Electric Company Segmented inlet nozzle for gas turbine, and methods of installation
US5197852A (en) 1990-05-31 1993-03-30 General Electric Company Nozzle band overhang cooling
US5165847A (en) * 1991-05-20 1992-11-24 General Electric Company Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines
US5224818A (en) * 1991-11-01 1993-07-06 General Electric Company Air transfer bushing
US5645397A (en) * 1995-10-10 1997-07-08 United Technologies Corporation Turbine vane assembly with multiple passage cooled vanes
JP3238344B2 (ja) * 1997-02-20 2001-12-10 三菱重工業株式会社 ガスタービン静翼
FR2766517B1 (fr) * 1997-07-24 1999-09-03 Snecma Dispositif de ventilation d'un anneau de turbomachine
FR2819010B1 (fr) * 2001-01-04 2004-05-28 Snecma Moteurs Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux
US6431820B1 (en) 2001-02-28 2002-08-13 General Electric Company Methods and apparatus for cooling gas turbine engine blade tips

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