ATE342431T1 - Kühlung eines turbinenleitapparat-segments - Google Patents

Kühlung eines turbinenleitapparat-segments

Info

Publication number
ATE342431T1
ATE342431T1 AT00306463T AT00306463T ATE342431T1 AT E342431 T1 ATE342431 T1 AT E342431T1 AT 00306463 T AT00306463 T AT 00306463T AT 00306463 T AT00306463 T AT 00306463T AT E342431 T1 ATE342431 T1 AT E342431T1
Authority
AT
Austria
Prior art keywords
intake duct
outer band
flange portion
airfoil
vanes
Prior art date
Application number
AT00306463T
Other languages
German (de)
English (en)
Inventor
Daniel Edward Demers
Aureen Cyr Currin
Mark Douglas Gledhill
Gene Chen-Fu Tsai
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Application granted granted Critical
Publication of ATE342431T1 publication Critical patent/ATE342431T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/128—Nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AT00306463T 1999-11-30 2000-07-28 Kühlung eines turbinenleitapparat-segments ATE342431T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/451,279 US6227798B1 (en) 1999-11-30 1999-11-30 Turbine nozzle segment band cooling

Publications (1)

Publication Number Publication Date
ATE342431T1 true ATE342431T1 (de) 2006-11-15

Family

ID=23791568

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00306463T ATE342431T1 (de) 1999-11-30 2000-07-28 Kühlung eines turbinenleitapparat-segments

Country Status (6)

Country Link
US (1) US6227798B1 (https=)
EP (1) EP1106787B1 (https=)
JP (1) JP4509325B2 (https=)
AT (1) ATE342431T1 (https=)
DE (1) DE60031226T2 (https=)
ES (1) ES2273648T3 (https=)

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US7008185B2 (en) * 2003-02-27 2006-03-07 General Electric Company Gas turbine engine turbine nozzle bifurcated impingement baffle
US6932568B2 (en) * 2003-02-27 2005-08-23 General Electric Company Turbine nozzle segment cantilevered mount
US7052231B2 (en) * 2003-04-28 2006-05-30 General Electric Company Methods and apparatus for injecting fluids in gas turbine engines
US6843637B1 (en) 2003-08-04 2005-01-18 General Electric Company Cooling circuit within a turbine nozzle and method of cooling a turbine nozzle
US7140835B2 (en) * 2004-10-01 2006-11-28 General Electric Company Corner cooled turbine nozzle
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US7588412B2 (en) * 2005-07-28 2009-09-15 General Electric Company Cooled shroud assembly and method of cooling a shroud
US7360988B2 (en) * 2005-12-08 2008-04-22 General Electric Company Methods and apparatus for assembling turbine engines
FR2899281B1 (fr) * 2006-03-30 2012-08-10 Snecma Dispositif de refroidissement d'un carter de turbine d'une turbomachine
US7806650B2 (en) * 2006-08-29 2010-10-05 General Electric Company Method and apparatus for fabricating a nozzle segment for use with turbine engines
FR2906846B1 (fr) * 2006-10-06 2008-12-26 Snecma Sa Canal de transition entre deux etages de turbine
US7798775B2 (en) * 2006-12-21 2010-09-21 General Electric Company Cantilevered nozzle with crowned flange to improve outer band low cycle fatigue
US8096755B2 (en) * 2006-12-21 2012-01-17 General Electric Company Crowned rails for supporting arcuate components
WO2009153108A2 (de) * 2008-05-26 2009-12-23 Alstom Technology Ltd. Gasturbine mit einer leitschaufel
US8206101B2 (en) * 2008-06-16 2012-06-26 General Electric Company Windward cooled turbine nozzle
DE102008033560A1 (de) * 2008-07-17 2010-01-21 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk mit verstellbaren Leitschaufeln
US8555645B2 (en) * 2008-07-21 2013-10-15 General Electric Company Fuel nozzle centerbody and method of assembling the same
FR2979573B1 (fr) * 2011-09-07 2017-04-21 Snecma Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs
US9062562B2 (en) 2008-11-28 2015-06-23 Herakles Composite material turbomachine engine blade or vane, compressor stator segment or turbine nozzle segment incorporating such vanes and method for manufacturing same
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US9045992B2 (en) 2010-06-28 2015-06-02 Herakles Turbomachine blades or vanes having complementary even/odd geometry
US9033673B2 (en) 2010-06-28 2015-05-19 Herakles Turbomachine blade or vane having complementary asymmetrical geometry
US9039350B2 (en) 2012-01-09 2015-05-26 General Electric Company Impingement cooling system for use with contoured surfaces
US9011079B2 (en) 2012-01-09 2015-04-21 General Electric Company Turbine nozzle compartmentalized cooling system
US9133724B2 (en) 2012-01-09 2015-09-15 General Electric Company Turbomachine component including a cover plate
US8864445B2 (en) 2012-01-09 2014-10-21 General Electric Company Turbine nozzle assembly methods
US9011078B2 (en) 2012-01-09 2015-04-21 General Electric Company Turbine vane seal carrier with slots for cooling and assembly
US8944751B2 (en) 2012-01-09 2015-02-03 General Electric Company Turbine nozzle cooling assembly
ES2731206T3 (es) 2012-03-12 2019-11-14 MTU Aero Engines AG Turbina de gas, álabe director para la carcasa de una turbina de gas, así como procedimiento para la fabricación de un álabe director
US9289826B2 (en) * 2012-09-17 2016-03-22 Honeywell International Inc. Turbine stator airfoil assemblies and methods for their manufacture
FR3003295B1 (fr) * 2013-03-14 2017-12-22 Snecma Dispositif collecteur d'etancheite pour turbomachine, procede d'assemblage
US9982560B2 (en) * 2015-01-16 2018-05-29 United Technologies Corporation Cooling feed orifices
US10018062B2 (en) 2015-07-02 2018-07-10 United Technologies Corporation Axial transfer tube
GB2551777B (en) 2016-06-30 2018-09-12 Rolls Royce Plc A stator vane arrangement and a method of casting a stator vane arrangement
US10519811B2 (en) * 2016-10-04 2019-12-31 United Technologies Corporation Flange heat shield
US10697313B2 (en) 2017-02-01 2020-06-30 General Electric Company Turbine engine component with an insert
US10301953B2 (en) * 2017-04-13 2019-05-28 General Electric Company Turbine nozzle with CMC aft Band
US11428124B2 (en) 2018-11-21 2022-08-30 Raytheon Technologies Corporation Flange stress-reduction features
US11517969B2 (en) * 2019-01-24 2022-12-06 General Electric Company Weld-brazing techniques
WO2023147119A1 (en) * 2022-01-28 2023-08-03 Raytheon Technologies Corporation Cooled vane with forward rail for gas turbine engine
WO2023147117A1 (en) * 2022-01-28 2023-08-03 Raytheon Technologies Corporation Cooled vane with forward rail for gas turbine engine

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FR2540937B1 (fr) * 1983-02-10 1987-05-22 Snecma Anneau pour un rotor de turbine d'une turbomachine
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Also Published As

Publication number Publication date
JP4509325B2 (ja) 2010-07-21
US6227798B1 (en) 2001-05-08
ES2273648T3 (es) 2007-05-16
EP1106787A3 (en) 2004-03-17
EP1106787B1 (en) 2006-10-11
EP1106787A2 (en) 2001-06-13
DE60031226D1 (de) 2006-11-23
DE60031226T2 (de) 2007-08-23
JP2001152806A (ja) 2001-06-05

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Legal Events

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