CN102536333B - 涡轮机翼型构件 - Google Patents

涡轮机翼型构件 Download PDF

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Publication number
CN102536333B
CN102536333B CN201210012813.3A CN201210012813A CN102536333B CN 102536333 B CN102536333 B CN 102536333B CN 201210012813 A CN201210012813 A CN 201210012813A CN 102536333 B CN102536333 B CN 102536333B
Authority
CN
China
Prior art keywords
airfoil
chamber
cooling
fluid
component
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 - Fee Related
Application number
CN201210012813.3A
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English (en)
Chinese (zh)
Other versions
CN102536333A (zh
Inventor
G·M·伊策尔
A·O·本森
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
Publication of CN102536333A publication Critical patent/CN102536333A/zh
Application granted granted Critical
Publication of CN102536333B publication Critical patent/CN102536333B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F01D5/182—Transpiration cooling
    • F01D5/183—Blade walls being porous
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/612—Foam
    • 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)
CN201210012813.3A 2011-01-03 2012-01-04 涡轮机翼型构件 Expired - Fee Related CN102536333B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/983400 2011-01-03
US12/983,400 US8807944B2 (en) 2011-01-03 2011-01-03 Turbomachine airfoil component and cooling method therefor

Publications (2)

Publication Number Publication Date
CN102536333A CN102536333A (zh) 2012-07-04
CN102536333B true CN102536333B (zh) 2015-11-25

Family

ID=46273416

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210012813.3A Expired - Fee Related CN102536333B (zh) 2011-01-03 2012-01-04 涡轮机翼型构件

Country Status (5)

Country Link
US (1) US8807944B2 (enExample)
JP (1) JP6006935B2 (enExample)
CN (1) CN102536333B (enExample)
DE (1) DE102011057071A1 (enExample)
FR (1) FR2970031B1 (enExample)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008016979A2 (en) 2006-08-02 2008-02-07 Liquidpiston, Inc. Hybrid cycle rotary engine
CN102203384A (zh) 2008-08-04 2011-09-28 流体活塞有限公司 等容加热发动机和方法
US8523524B2 (en) * 2010-03-25 2013-09-03 General Electric Company Airfoil cooling hole flag region
US9328623B2 (en) * 2011-10-05 2016-05-03 General Electric Company Turbine system
JP6230383B2 (ja) * 2013-11-21 2017-11-15 三菱日立パワーシステムズ株式会社 蒸気タービンの静翼と蒸気タービン
CN104110275B (zh) * 2014-07-02 2016-01-13 北京航空航天大学 一种基于多孔介质和超临界状态流体循环的先进涡轮冷却方法
US9835087B2 (en) * 2014-09-03 2017-12-05 General Electric Company Turbine bucket
EP3268585B1 (en) 2015-03-10 2023-07-19 LiquidPiston, Inc. High power density and efficiency epitrochoidal rotary engine
US10508554B2 (en) 2015-10-27 2019-12-17 General Electric Company Turbine bucket having outlet path in shroud
US10156145B2 (en) * 2015-10-27 2018-12-18 General Electric Company Turbine bucket having cooling passageway
US9885243B2 (en) 2015-10-27 2018-02-06 General Electric Company Turbine bucket having outlet path in shroud
US10731472B2 (en) * 2016-05-10 2020-08-04 General Electric Company Airfoil with cooling circuit
US10605095B2 (en) 2016-05-11 2020-03-31 General Electric Company Ceramic matrix composite airfoil cooling
US10415397B2 (en) 2016-05-11 2019-09-17 General Electric Company Ceramic matrix composite airfoil cooling
US20170328213A1 (en) * 2016-05-12 2017-11-16 General Electric Company Engine component wall with a cooling circuit
US10450950B2 (en) * 2016-10-26 2019-10-22 General Electric Company Turbomachine blade with trailing edge cooling circuit
US10883371B1 (en) 2019-06-21 2021-01-05 Rolls-Royce Plc Ceramic matrix composite vane with trailing edge radial cooling
US11427330B2 (en) * 2019-11-15 2022-08-30 General Electric Company System and method for cooling a leading edge of a high speed vehicle
FR3115079B1 (fr) * 2020-10-12 2022-10-14 Safran Aircraft Engines Aube en materiau composite comprenant un bouclier de bord d’attaque, turbomachine comprenant l’aube
CN116642381B (zh) * 2023-06-14 2025-10-31 中铝材料应用研究院有限公司 飞行体冷却装置

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3695778A (en) * 1970-09-18 1972-10-03 Trw Inc Turbine blade
US4314794A (en) * 1979-10-25 1982-02-09 Westinghouse Electric Corp. Transpiration cooled blade for a gas turbine engine
US5577884A (en) * 1984-03-14 1996-11-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Structure for a stationary cooled turbine vane
CN1527922A (zh) * 2001-07-13 2004-09-08 涡轮机组和燃烧涡轮机的可冷却段

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55109704A (en) * 1979-02-19 1980-08-23 Hitachi Ltd Gas-turbine blade capable of being cooled
GB2042648B (en) * 1979-02-24 1983-05-05 Rolls Royce Gas turbine engine hollow blades
JPH0740642Y2 (ja) * 1986-04-17 1995-09-20 三菱重工業株式会社 ガスタービン動翼への冷却空気供給構造
US5464322A (en) * 1994-08-23 1995-11-07 General Electric Company Cooling circuit for turbine stator vane trailing edge
DE10024302A1 (de) * 2000-05-17 2001-11-22 Alstom Power Nv Verfahren zur Herstellung eines thermisch belasteten Gussteils
EP1186748A1 (de) * 2000-09-05 2002-03-13 Siemens Aktiengesellschaft Laufschaufel für eine Strömungsmaschine sowie Strömungsmaschine
US6981846B2 (en) * 2003-03-12 2006-01-03 Florida Turbine Technologies, Inc. Vortex cooling of turbine blades
US7144220B2 (en) * 2004-07-30 2006-12-05 United Technologies Corporation Investment casting
US7422417B2 (en) * 2005-05-05 2008-09-09 Florida Turbine Technologies, Inc. Airfoil with a porous fiber metal layer
US7500828B2 (en) * 2005-05-05 2009-03-10 Florida Turbine Technologies, Inc. Airfoil having porous metal filled cavities
EP1847696A1 (de) * 2006-04-21 2007-10-24 Siemens Aktiengesellschaft Bauteil für eine gestufte Verbrennung in einer Gasturbine und entsprechende Gasturbine.
US20070274854A1 (en) 2006-05-23 2007-11-29 General Electric Company Method of making metallic composite foam components
US7488156B2 (en) * 2006-06-06 2009-02-10 Siemens Energy, Inc. Turbine airfoil with floating wall mechanism and multi-metering diffusion technique
US7905016B2 (en) 2007-04-10 2011-03-15 Siemens Energy, Inc. System for forming a gas cooled airfoil for use in a turbine engine
US20100008759A1 (en) * 2008-07-10 2010-01-14 General Electric Company Methods and apparatuses for providing film cooling to turbine components
US8052378B2 (en) * 2009-03-18 2011-11-08 General Electric Company Film-cooling augmentation device and turbine airfoil incorporating the same
US20100239409A1 (en) * 2009-03-18 2010-09-23 General Electric Company Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3695778A (en) * 1970-09-18 1972-10-03 Trw Inc Turbine blade
US4314794A (en) * 1979-10-25 1982-02-09 Westinghouse Electric Corp. Transpiration cooled blade for a gas turbine engine
US5577884A (en) * 1984-03-14 1996-11-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Structure for a stationary cooled turbine vane
CN1527922A (zh) * 2001-07-13 2004-09-08 涡轮机组和燃烧涡轮机的可冷却段

Also Published As

Publication number Publication date
JP2012140946A (ja) 2012-07-26
US20120171047A1 (en) 2012-07-05
FR2970031A1 (fr) 2012-07-06
CN102536333A (zh) 2012-07-04
JP6006935B2 (ja) 2016-10-12
DE102011057071A1 (de) 2012-08-30
FR2970031B1 (fr) 2016-01-08
US8807944B2 (en) 2014-08-19

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