JP2000145403A5 - - Google Patents

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Publication number
JP2000145403A5
JP2000145403A5 JP1999205496A JP20549699A JP2000145403A5 JP 2000145403 A5 JP2000145403 A5 JP 2000145403A5 JP 1999205496 A JP1999205496 A JP 1999205496A JP 20549699 A JP20549699 A JP 20549699A JP 2000145403 A5 JP2000145403 A5 JP 2000145403A5
Authority
JP
Japan
Prior art keywords
inner band
air
rotor
turbine nozzle
outlet hole
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.)
Withdrawn
Application number
JP1999205496A
Other languages
English (en)
Japanese (ja)
Other versions
JP2000145403A (ja
Filing date
Publication date
Priority claimed from US09/119,914 external-priority patent/US6065928A/en
Application filed filed Critical
Publication of JP2000145403A publication Critical patent/JP2000145403A/ja
Publication of JP2000145403A5 publication Critical patent/JP2000145403A5/ja
Withdrawn legal-status Critical Current

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JP11205496A 1998-07-22 1999-07-21 パ―ジ空気回路を有するタ―ビンノズル Withdrawn JP2000145403A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/119914 1998-07-22
US09/119,914 US6065928A (en) 1998-07-22 1998-07-22 Turbine nozzle having purge air circuit

Publications (2)

Publication Number Publication Date
JP2000145403A JP2000145403A (ja) 2000-05-26
JP2000145403A5 true JP2000145403A5 (cg-RX-API-DMAC7.html) 2006-09-07

Family

ID=22387152

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11205496A Withdrawn JP2000145403A (ja) 1998-07-22 1999-07-21 パ―ジ空気回路を有するタ―ビンノズル

Country Status (4)

Country Link
US (1) US6065928A (cg-RX-API-DMAC7.html)
EP (1) EP0974733B1 (cg-RX-API-DMAC7.html)
JP (1) JP2000145403A (cg-RX-API-DMAC7.html)
DE (1) DE69926574T2 (cg-RX-API-DMAC7.html)

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US6554566B1 (en) 2001-10-26 2003-04-29 General Electric Company Turbine shroud cooling hole diffusers and related method
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ATE328191T1 (de) * 2002-04-02 2006-06-15 Man Turbo Ag Vorrichtung zur abdichtung in turbomaschinen
ITMI20021219A1 (it) * 2002-06-05 2003-12-05 Nuovo Pignone Spa Dispositivo di supporto semplificato per ugelli di uno stadio di una turbina a gas
US6884023B2 (en) * 2002-09-27 2005-04-26 United Technologies Corporation Integral swirl knife edge injection assembly
FR2851288B1 (fr) * 2003-02-14 2006-07-28 Snecma Moteurs Dispositif de refroidissement de disques de turbines
JP3977780B2 (ja) * 2003-06-20 2007-09-19 株式会社日立製作所 ガスタービン
FR2856729B1 (fr) 2003-06-30 2005-09-23 Snecma Moteurs Aubes refroidies de moteur a turbine a gaz.
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US8206101B2 (en) * 2008-06-16 2012-06-26 General Electric Company Windward cooled turbine nozzle
US8137067B2 (en) * 2008-11-05 2012-03-20 General Electric Company Turbine with interrupted purge flow
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US8353668B2 (en) * 2009-02-18 2013-01-15 United Technologies Corporation Airfoil insert having a tab extending away from the body defining a portion of outlet periphery
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US10337404B2 (en) * 2010-03-08 2019-07-02 General Electric Company Preferential cooling of gas turbine nozzles
US8608436B2 (en) 2010-08-31 2013-12-17 General Electric Company Tapered collet connection of rotor components
US8944751B2 (en) * 2012-01-09 2015-02-03 General Electric Company Turbine nozzle cooling assembly
US8864445B2 (en) * 2012-01-09 2014-10-21 General Electric Company Turbine nozzle assembly methods
US20130323009A1 (en) * 2012-05-31 2013-12-05 Mark Kevin Bowen Methods and apparatus for cooling rotary components within a steam turbine
US9194237B2 (en) * 2012-09-10 2015-11-24 General Electric Company Serpentine cooling of nozzle endwall
DE102013209746B4 (de) * 2013-05-27 2014-12-18 MTU Aero Engines AG Turbinenstufe mit einer Ausblasanordnung und Verfahren zum Ausblasen einer Sperrgasströmung
CN105378226B (zh) * 2013-07-19 2017-11-10 通用电气公司 带有冲击挡板的涡轮喷嘴
WO2015030926A1 (en) * 2013-08-30 2015-03-05 United Technologies Corporation Baffle for gas turbine engine vane
US9771816B2 (en) 2014-05-07 2017-09-26 General Electric Company Blade cooling circuit feed duct, exhaust duct, and related cooling structure
US9638045B2 (en) * 2014-05-28 2017-05-02 General Electric Company Cooling structure for stationary blade
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EP3112592B1 (en) * 2015-07-02 2019-06-19 Ansaldo Energia Switzerland AG Gas turbine blade
US9909436B2 (en) 2015-07-16 2018-03-06 General Electric Company Cooling structure for stationary blade
US10253986B2 (en) * 2015-09-08 2019-04-09 General Electric Company Article and method of forming an article
US9970299B2 (en) * 2015-09-16 2018-05-15 General Electric Company Mixing chambers for turbine wheel space cooling
US10352245B2 (en) 2015-10-05 2019-07-16 General Electric Company Windage shield system and method of suppressing resonant acoustic noise
US10125632B2 (en) 2015-10-20 2018-11-13 General Electric Company Wheel space purge flow mixing chamber
US10132195B2 (en) 2015-10-20 2018-11-20 General Electric Company Wheel space purge flow mixing chamber
US10030538B2 (en) 2015-11-05 2018-07-24 General Electric Company Gas turbine engine with a vane having a cooling air turning nozzle
FR3044038B1 (fr) * 2015-11-19 2019-08-30 Safran Helicopter Engines Aube equipee d'un systeme de refroidissement, distributeur et turbomachine associes
WO2017125289A1 (en) * 2016-01-19 2017-07-27 Siemens Aktiengesellschaft Aerofoil arrangement
US10519873B2 (en) * 2016-04-06 2019-12-31 General Electric Company Air bypass system for rotor shaft cooling
DE102016222608A1 (de) 2016-11-17 2018-05-17 MTU Aero Engines AG Dichtungsanordnung für eine Leitschaufelanordnung einer Gasturbine
US20190234235A1 (en) * 2018-01-31 2019-08-01 United Technologies Corporation Vane flow diverter
US10677071B2 (en) * 2018-04-19 2020-06-09 Raytheon Technologies Corporation Turbine vane for gas turbine engine
US10837293B2 (en) 2018-07-19 2020-11-17 General Electric Company Airfoil with tunable cooling configuration
US11255267B2 (en) * 2018-10-31 2022-02-22 Raytheon Technologies Corporation Method of cooling a gas turbine and apparatus
JP6745012B1 (ja) * 2019-10-31 2020-08-26 三菱日立パワーシステムズ株式会社 タービン翼及びこれを備えたガスタービン
US11525397B2 (en) * 2020-09-01 2022-12-13 General Electric Company Gas turbine component with ejection circuit for removing debris from cooling air supply
US20250327406A1 (en) * 2022-11-03 2025-10-23 General Electric Company Turbine nozzle or blade with impingement cooling structure having thermal flex elements

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US4288201A (en) * 1979-09-14 1981-09-08 United Technologies Corporation Vane cooling structure
US4962640A (en) * 1989-02-06 1990-10-16 Westinghouse Electric Corp. Apparatus and method for cooling a gas turbine vane
US5207556A (en) * 1992-04-27 1993-05-04 General Electric Company Airfoil having multi-passage baffle
US5217348A (en) * 1992-09-24 1993-06-08 United Technologies Corporation Turbine vane assembly with integrally cast cooling fluid nozzle
US5358374A (en) * 1993-07-21 1994-10-25 General Electric Company Turbine nozzle backflow inhibitor
WO1996015357A1 (en) * 1994-11-10 1996-05-23 Westinghouse Electric Corporation Gas turbine vane with a cooled inner shroud
US5645397A (en) * 1995-10-10 1997-07-08 United Technologies Corporation Turbine vane assembly with multiple passage cooled vanes
FR2743391B1 (fr) * 1996-01-04 1998-02-06 Snecma Aube refrigeree de distributeur de turbine
US5749701A (en) * 1996-10-28 1998-05-12 General Electric Company Interstage seal assembly for a turbine
FR2771446B1 (fr) * 1997-11-27 1999-12-31 Snecma Aube de distributeur de turbine refroidie

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