DE60043719D1 - Schaufelspitzenkühlung - Google Patents

Schaufelspitzenkühlung

Info

Publication number
DE60043719D1
DE60043719D1 DE60043719T DE60043719T DE60043719D1 DE 60043719 D1 DE60043719 D1 DE 60043719D1 DE 60043719 T DE60043719 T DE 60043719T DE 60043719 T DE60043719 T DE 60043719T DE 60043719 D1 DE60043719 D1 DE 60043719D1
Authority
DE
Germany
Prior art keywords
blade tip
tip cooling
cooling
blade
tip
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
DE60043719T
Other languages
English (en)
Inventor
Victor Hugo Silva Correia
Robert Francis Manning
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60043719D1 publication Critical patent/DE60043719D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • F01D5/186—Film 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
    • F01D5/187—Convection 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
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling
    • 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)
DE60043719T 1999-08-23 2000-07-05 Schaufelspitzenkühlung Expired - Lifetime DE60043719D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/379,023 US6164914A (en) 1999-08-23 1999-08-23 Cool tip blade

Publications (1)

Publication Number Publication Date
DE60043719D1 true DE60043719D1 (de) 2010-03-11

Family

ID=23495498

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60043719T Expired - Lifetime DE60043719D1 (de) 1999-08-23 2000-07-05 Schaufelspitzenkühlung

Country Status (4)

Country Link
US (1) US6164914A (de)
EP (1) EP1079072B1 (de)
JP (1) JP4636657B2 (de)
DE (1) DE60043719D1 (de)

Families Citing this family (118)

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DE19963099B4 (de) * 1999-12-24 2014-01-02 Alstom Technology Ltd. Kühlluftbohrungen in Gasturbinenkomponenten
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US6554575B2 (en) * 2001-09-27 2003-04-29 General Electric Company Ramped tip shelf blade
US6837687B2 (en) * 2001-12-20 2005-01-04 General Electric Company Foil formed structure for turbine airfoil
US6634860B2 (en) * 2001-12-20 2003-10-21 General Electric Company Foil formed structure for turbine airfoil tip
US6652235B1 (en) * 2002-05-31 2003-11-25 General Electric Company Method and apparatus for reducing turbine blade tip region temperatures
US6672829B1 (en) 2002-07-16 2004-01-06 General Electric Company Turbine blade having angled squealer tip
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US6790005B2 (en) * 2002-12-30 2004-09-14 General Electric Company Compound tip notched blade
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US6824359B2 (en) * 2003-01-31 2004-11-30 United Technologies Corporation Turbine blade
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US6991430B2 (en) * 2003-04-07 2006-01-31 General Electric Company Turbine blade with recessed squealer tip and shelf
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US6905309B2 (en) * 2003-08-28 2005-06-14 General Electric Company Methods and apparatus for reducing vibrations induced to compressor airfoils
US6923616B2 (en) * 2003-09-02 2005-08-02 General Electric Company Methods and apparatus for cooling gas turbine engine rotor assemblies
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US7600972B2 (en) * 2003-10-31 2009-10-13 General Electric Company Methods and apparatus for cooling gas turbine engine rotor assemblies
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US20100135822A1 (en) * 2008-11-28 2010-06-03 Remo Marini Turbine blade for a gas turbine engine
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US8123481B1 (en) * 2009-06-17 2012-02-28 Florida Turbine Technologies, Inc. Turbine blade with dual serpentine cooling
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US8673397B2 (en) 2010-11-10 2014-03-18 General Electric Company Methods of fabricating and coating a component
US9249491B2 (en) 2010-11-10 2016-02-02 General Electric Company Components with re-entrant shaped cooling channels and methods of manufacture
US8753071B2 (en) 2010-12-22 2014-06-17 General Electric Company Cooling channel systems for high-temperature components covered by coatings, and related processes
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US8601691B2 (en) 2011-04-27 2013-12-10 General Electric Company Component and methods of fabricating a coated component using multiple types of fillers
CN102182518B (zh) * 2011-06-08 2013-09-04 河南科技大学 一种涡轮冷却叶片
US9249672B2 (en) 2011-09-23 2016-02-02 General Electric Company Components with cooling channels and methods of manufacture
US9249670B2 (en) * 2011-12-15 2016-02-02 General Electric Company Components with microchannel cooling
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US9091177B2 (en) * 2012-03-14 2015-07-28 United Technologies Corporation Shark-bite tip shelf cooling configuration
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US9284845B2 (en) 2012-04-05 2016-03-15 United Technologies Corporation Turbine airfoil tip shelf and squealer pocket cooling
US9435208B2 (en) 2012-04-17 2016-09-06 General Electric Company Components with microchannel cooling
US9243503B2 (en) 2012-05-23 2016-01-26 General Electric Company Components with microchannel cooled platforms and fillets and methods of manufacture
DE102013109116A1 (de) 2012-08-27 2014-03-27 General Electric Company (N.D.Ges.D. Staates New York) Bauteil mit Kühlkanälen und Verfahren zur Herstellung
US8974859B2 (en) 2012-09-26 2015-03-10 General Electric Company Micro-channel coating deposition system and method for using the same
US9546554B2 (en) 2012-09-27 2017-01-17 Honeywell International Inc. Gas turbine engine components with blade tip cooling
US9238265B2 (en) 2012-09-27 2016-01-19 General Electric Company Backstrike protection during machining of cooling features
US9242294B2 (en) 2012-09-27 2016-01-26 General Electric Company Methods of forming cooling channels using backstrike protection
US9200521B2 (en) 2012-10-30 2015-12-01 General Electric Company Components with micro cooled coating layer and methods of manufacture
US9562436B2 (en) 2012-10-30 2017-02-07 General Electric Company Components with micro cooled patterned coating layer and methods of manufacture
US10655473B2 (en) * 2012-12-13 2020-05-19 United Technologies Corporation Gas turbine engine turbine blade leading edge tip trench cooling
US8920123B2 (en) 2012-12-14 2014-12-30 Siemens Aktiengesellschaft Turbine blade with integrated serpentine and axial tip cooling circuits
US9003657B2 (en) 2012-12-18 2015-04-14 General Electric Company Components with porous metal cooling and methods of manufacture
US10502065B2 (en) 2013-06-17 2019-12-10 United Technologies Corporation Gas turbine engine component with rib support
US9856739B2 (en) * 2013-09-18 2018-01-02 Honeywell International Inc. Turbine blades with tip portions having converging cooling holes
US9879544B2 (en) 2013-10-16 2018-01-30 Honeywell International Inc. Turbine rotor blades with improved tip portion cooling holes
US9816389B2 (en) 2013-10-16 2017-11-14 Honeywell International Inc. Turbine rotor blades with tip portion parapet wall cavities
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US9777574B2 (en) * 2014-08-18 2017-10-03 Siemens Energy, Inc. Method for repairing a gas turbine engine blade tip
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US9995147B2 (en) 2015-02-11 2018-06-12 United Technologies Corporation Blade tip cooling arrangement
EP3088673B1 (de) * 2015-04-28 2017-11-01 Siemens Aktiengesellschaft Laufschaufel für eine gasturbine, zugehöriger rotor, gasturbine und kraftwerksanlage
US10107108B2 (en) 2015-04-29 2018-10-23 General Electric Company Rotor blade having a flared tip
US9976424B2 (en) * 2015-07-02 2018-05-22 General Electric Company Turbine blade
JP6565105B2 (ja) * 2015-09-29 2019-08-28 三菱日立パワーシステムズ株式会社 動翼及びこれを備えるガスタービン
US10156145B2 (en) * 2015-10-27 2018-12-18 General Electric Company Turbine bucket having cooling passageway
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US20180161853A1 (en) * 2016-12-13 2018-06-14 General Electric Company Integrated casting core-shell structure with floating tip plenum
US11021967B2 (en) * 2017-04-03 2021-06-01 General Electric Company Turbine engine component with a core tie hole
JP6947851B2 (ja) 2017-05-30 2021-10-13 シーメンス アクティエンゲゼルシャフト スキーラ先端を備えるタービンブレードおよび高密度酸化物分散強化層
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CN111852575A (zh) * 2020-07-27 2020-10-30 北京全四维动力科技有限公司 涡轮转子叶片及包括其的燃气轮机
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Also Published As

Publication number Publication date
EP1079072B1 (de) 2010-01-20
JP4636657B2 (ja) 2011-02-23
EP1079072A2 (de) 2001-02-28
JP2001073704A (ja) 2001-03-21
EP1079072A3 (de) 2004-01-02
US6164914A (en) 2000-12-26

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