DE60021658D1 - Hinterkantenkühlung einer Turbinenschaufel - Google Patents

Hinterkantenkühlung einer Turbinenschaufel

Info

Publication number
DE60021658D1
DE60021658D1 DE60021658T DE60021658T DE60021658D1 DE 60021658 D1 DE60021658 D1 DE 60021658D1 DE 60021658 T DE60021658 T DE 60021658T DE 60021658 T DE60021658 T DE 60021658T DE 60021658 D1 DE60021658 D1 DE 60021658D1
Authority
DE
Germany
Prior art keywords
trailing edge
turbine blade
edge cooling
cooling
turbine
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
DE60021658T
Other languages
English (en)
Other versions
DE60021658T2 (de
Inventor
Stephen Kin-Keung Tung
Donald Clinton Weldon
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 DE60021658D1 publication Critical patent/DE60021658D1/de
Publication of DE60021658T2 publication Critical patent/DE60021658T2/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
    • F01D5/187—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
    • F01D5/18—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
    • 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
    • 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
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2212—Improvement of heat transfer by creating turbulence
    • 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
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • 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
DE60021658T 1999-06-01 2000-05-31 Hinterkantenkühlung einer Turbinenschaufel Expired - Lifetime DE60021658T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US323327 1989-03-14
US09/323,327 US6241466B1 (en) 1999-06-01 1999-06-01 Turbine airfoil breakout cooling

Publications (2)

Publication Number Publication Date
DE60021658D1 true DE60021658D1 (de) 2005-09-08
DE60021658T2 DE60021658T2 (de) 2006-05-24

Family

ID=23258728

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60021658T Expired - Lifetime DE60021658T2 (de) 1999-06-01 2000-05-31 Hinterkantenkühlung einer Turbinenschaufel

Country Status (4)

Country Link
US (1) US6241466B1 (de)
EP (1) EP1057971B1 (de)
JP (1) JP4572396B2 (de)
DE (1) DE60021658T2 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002221005A (ja) * 2001-01-26 2002-08-09 Ishikawajima Harima Heavy Ind Co Ltd 冷却タービン翼
US6609891B2 (en) 2001-08-30 2003-08-26 General Electric Company Turbine airfoil for gas turbine engine
US6551062B2 (en) 2001-08-30 2003-04-22 General Electric Company Turbine airfoil for gas turbine engine
US6551063B1 (en) * 2001-12-20 2003-04-22 General Electric Company Foil formed structure for turbine airfoil trailing edge
US6602047B1 (en) * 2002-02-28 2003-08-05 General Electric Company Methods and apparatus for cooling gas turbine nozzles
US7762775B1 (en) 2007-05-31 2010-07-27 Florida Turbine Technologies, Inc. Turbine airfoil with cooled thin trailing edge
DE102007029367A1 (de) * 2007-06-26 2009-01-02 Rolls-Royce Deutschland Ltd & Co Kg Schaufel mit Tangentialstrahlerzeugung am Profil
US8257035B2 (en) * 2007-12-05 2012-09-04 Siemens Energy, Inc. Turbine vane for a gas turbine engine
US8016563B1 (en) * 2007-12-21 2011-09-13 Florida Turbine Technologies, Inc. Turbine blade with tip turn cooling
US8172534B2 (en) * 2009-01-21 2012-05-08 General Electric Company Turbine blade or vane with improved cooling
US9422816B2 (en) * 2009-06-26 2016-08-23 United Technologies Corporation Airfoil with hybrid drilled and cutback trailing edge
US20110268583A1 (en) * 2010-04-30 2011-11-03 General Electric Company Airfoil trailing edge and method of manufacturing the same
US8608429B2 (en) * 2010-05-28 2013-12-17 General Electric Company System and method for enhanced turbine wake mixing via fluidic-generated vortices
EP2489836A1 (de) 2011-02-21 2012-08-22 Karlsruher Institut für Technologie Kühlbares Bauteil
US9228437B1 (en) * 2012-03-22 2016-01-05 Florida Turbine Technologies, Inc. Turbine airfoil with pressure side trailing edge cooling slots
US9039370B2 (en) 2012-03-29 2015-05-26 Solar Turbines Incorporated Turbine nozzle
US9435208B2 (en) 2012-04-17 2016-09-06 General Electric Company Components with microchannel cooling
EP2682565B8 (de) * 2012-07-02 2016-09-21 General Electric Technology GmbH Gekühlte Schaufel für eine Gasturbine
JP6203423B2 (ja) 2014-03-05 2017-09-27 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ 弓形ベーン用のタービン翼冷却システム
JP6347893B2 (ja) 2014-07-24 2018-06-27 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ 翼長方向に延びる流れブロッカを備えるタービン翼冷却システム
US10641113B2 (en) 2015-04-08 2020-05-05 United Technologies Corporation Airfoils
US10301954B2 (en) * 2016-01-08 2019-05-28 General Electric Company Turbine airfoil trailing edge cooling passage
US10443407B2 (en) * 2016-02-15 2019-10-15 General Electric Company Accelerator insert for a gas turbine engine airfoil
US10605095B2 (en) * 2016-05-11 2020-03-31 General Electric Company Ceramic matrix composite airfoil cooling
US11519277B2 (en) 2021-04-15 2022-12-06 General Electric Company Component with cooling passage for a turbine engine
CN114991878B (zh) * 2022-05-30 2023-07-07 哈尔滨工业大学 一种涡轮压力侧半劈缝冷却海豹胡须尾缘叶片及成型方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4353679A (en) * 1976-07-29 1982-10-12 General Electric Company Fluid-cooled element
US4314442A (en) * 1978-10-26 1982-02-09 Rice Ivan G Steam-cooled blading with steam thermal barrier for reheat gas turbine combined with steam turbine
US4545197A (en) * 1978-10-26 1985-10-08 Rice Ivan G Process for directing a combustion gas stream onto rotatable blades of a gas turbine
US4303374A (en) 1978-12-15 1981-12-01 General Electric Company Film cooled airfoil body
US4601638A (en) 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
US5102299A (en) * 1986-11-10 1992-04-07 The United States Of America As Represented By The Secretary Of The Air Force Airfoil trailing edge cooling configuration
GB2221979B (en) * 1988-08-17 1992-03-25 Rolls Royce Plc A combustion chamber for a gas turbine engine
US5368441A (en) 1992-11-24 1994-11-29 United Technologies Corporation Turbine airfoil including diffusing trailing edge pedestals
US5458461A (en) * 1994-12-12 1995-10-17 General Electric Company Film cooled slotted wall

Also Published As

Publication number Publication date
DE60021658T2 (de) 2006-05-24
EP1057971B1 (de) 2005-08-03
US6241466B1 (en) 2001-06-05
JP4572396B2 (ja) 2010-11-04
EP1057971A1 (de) 2000-12-06
JP2000356105A (ja) 2000-12-26

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