CN103857881B - 用于冷却燃气涡轮机转子叶片的方法和装置 - Google Patents

用于冷却燃气涡轮机转子叶片的方法和装置 Download PDF

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Publication number
CN103857881B
CN103857881B CN201280047834.7A CN201280047834A CN103857881B CN 103857881 B CN103857881 B CN 103857881B CN 201280047834 A CN201280047834 A CN 201280047834A CN 103857881 B CN103857881 B CN 103857881B
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CN
China
Prior art keywords
chamber
flow communication
downcomer
airfoil
impingement
Prior art date
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Active
Application number
CN201280047834.7A
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English (en)
Chinese (zh)
Other versions
CN103857881A (zh
Inventor
S.M.莫尔特
S.R.布拉斯菲尔德
R.W.詹德里克斯
C.M.威廉斯
R.S.温斯特拉普
M.W.马鲁斯科
M.E.斯特格米勒
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General Electric Co
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General Electric Co
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Publication date
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Publication of CN103857881A publication Critical patent/CN103857881A/zh
Application granted granted 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
    • F01D5/187—Convection 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
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade
    • Y10T29/49341—Hollow blade with cooling passage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201280047834.7A 2011-09-30 2012-09-11 用于冷却燃气涡轮机转子叶片的方法和装置 Active CN103857881B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/250345 2011-09-30
US13/250,345 US9033652B2 (en) 2011-09-30 2011-09-30 Method and apparatus for cooling gas turbine rotor blades
PCT/US2012/054563 WO2013048715A1 (en) 2011-09-30 2012-09-11 Method and apparatus for cooling gas turbine rotor blades

Publications (2)

Publication Number Publication Date
CN103857881A CN103857881A (zh) 2014-06-11
CN103857881B true CN103857881B (zh) 2016-06-01

Family

ID=46968365

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201280047834.7A Active CN103857881B (zh) 2011-09-30 2012-09-11 用于冷却燃气涡轮机转子叶片的方法和装置

Country Status (6)

Country Link
US (1) US9033652B2 (https=)
EP (1) EP2761138A1 (https=)
JP (1) JP6165740B2 (https=)
CN (1) CN103857881B (https=)
CA (1) CA2848867C (https=)
WO (1) WO2013048715A1 (https=)

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US9995148B2 (en) 2012-10-04 2018-06-12 General Electric Company Method and apparatus for cooling gas turbine and rotor blades
US9581028B1 (en) * 2014-02-24 2017-02-28 Florida Turbine Technologies, Inc. Small turbine stator vane with impingement cooling insert
EP2993301B1 (en) * 2014-08-28 2024-01-17 RTX Corporation Gas turbine engine structure, gas turbine engine and method for passing a coolant through a flow path in a gas turbine engine
US10029299B2 (en) 2015-07-09 2018-07-24 General Electric Company Three-dimensional manufacturing methods and systems for turbine components
US10030526B2 (en) * 2015-12-21 2018-07-24 General Electric Company Platform core feed for a multi-wall blade
US20170234141A1 (en) * 2016-02-16 2017-08-17 General Electric Company Airfoil having crossover holes
US10480327B2 (en) * 2017-01-03 2019-11-19 General Electric Company Components having channels for impingement cooling
FR3067388B1 (fr) * 2017-04-10 2020-01-17 Safran Aube a circuit de refroidissement perfectionne
US10570748B2 (en) 2018-01-10 2020-02-25 United Technologies Corporation Impingement cooling arrangement for airfoils
US10837293B2 (en) * 2018-07-19 2020-11-17 General Electric Company Airfoil with tunable cooling configuration
US10934854B2 (en) * 2018-09-11 2021-03-02 General Electric Company CMC component cooling cavities
US12123319B2 (en) * 2020-12-30 2024-10-22 Ge Infrastructure Technology Llc Cooling circuit having a bypass conduit for a turbomachine component

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US6036441A (en) * 1998-11-16 2000-03-14 General Electric Company Series impingement cooled airfoil
US20060222495A1 (en) * 2005-03-29 2006-10-05 Siemens Westinghouse Power Corporation Turbine blade cooling system with bifurcated mid-chord cooling chamber
US20060222494A1 (en) * 2005-03-29 2006-10-05 Siemens Westinghouse Power Corporation Turbine blade leading edge cooling system
US20100104419A1 (en) * 2006-08-01 2010-04-29 Siemens Power Generation, Inc. Turbine airfoil with near wall inflow chambers
US8016564B1 (en) * 2009-04-09 2011-09-13 Florida Turbine Technologies, Inc. Turbine blade with leading edge impingement cooling

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US4270883A (en) 1977-04-20 1981-06-02 The Garrett Corporation Laminated airfoil
GB2246174B (en) * 1982-06-29 1992-04-15 Rolls Royce A cooled aerofoil for a gas turbine engine
US5484258A (en) 1994-03-01 1996-01-16 General Electric Company Turbine airfoil with convectively cooled double shell outer wall
US5702232A (en) 1994-12-13 1997-12-30 United Technologies Corporation Cooled airfoils for a gas turbine engine
US5931638A (en) 1997-08-07 1999-08-03 United Technologies Corporation Turbomachinery airfoil with optimized heat transfer
US6220817B1 (en) 1997-11-17 2001-04-24 General Electric Company AFT flowing multi-tier airfoil cooling circuit
US6431832B1 (en) * 2000-10-12 2002-08-13 Solar Turbines Incorporated Gas turbine engine airfoils with improved cooling
FR2829174B1 (fr) 2001-08-28 2006-01-20 Snecma Moteurs Perfectionnement apportes aux circuits de refroidissement pour aube de turbine a gaz
US7104757B2 (en) 2003-07-29 2006-09-12 Siemens Aktiengesellschaft Cooled turbine blade
US7097426B2 (en) 2004-04-08 2006-08-29 General Electric Company Cascade impingement cooled airfoil
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US7303376B2 (en) 2005-12-02 2007-12-04 Siemens Power Generation, Inc. Turbine airfoil with outer wall cooling system and inner mid-chord hot gas receiving cavity
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US7534089B2 (en) * 2006-07-18 2009-05-19 Siemens Energy, Inc. Turbine airfoil with near wall multi-serpentine cooling channels
US7866948B1 (en) * 2006-08-16 2011-01-11 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall impingement and vortex cooling
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US7568887B1 (en) * 2006-11-16 2009-08-04 Florida Turbine Technologies, Inc. Turbine blade with near wall spiral flow serpentine cooling circuit
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US7624787B2 (en) 2006-12-06 2009-12-01 General Electric Company Disposable insert, and use thereof in a method for manufacturing an airfoil
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US7857589B1 (en) * 2007-09-21 2010-12-28 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall cooling
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Publication number Priority date Publication date Assignee Title
US6036441A (en) * 1998-11-16 2000-03-14 General Electric Company Series impingement cooled airfoil
US20060222495A1 (en) * 2005-03-29 2006-10-05 Siemens Westinghouse Power Corporation Turbine blade cooling system with bifurcated mid-chord cooling chamber
US20060222494A1 (en) * 2005-03-29 2006-10-05 Siemens Westinghouse Power Corporation Turbine blade leading edge cooling system
US20100104419A1 (en) * 2006-08-01 2010-04-29 Siemens Power Generation, Inc. Turbine airfoil with near wall inflow chambers
US8016564B1 (en) * 2009-04-09 2011-09-13 Florida Turbine Technologies, Inc. Turbine blade with leading edge impingement cooling

Also Published As

Publication number Publication date
WO2013048715A1 (en) 2013-04-04
US20130081408A1 (en) 2013-04-04
US9033652B2 (en) 2015-05-19
CA2848867A1 (en) 2013-04-04
CA2848867C (en) 2017-08-08
JP2014528538A (ja) 2014-10-27
JP6165740B2 (ja) 2017-07-19
EP2761138A1 (en) 2014-08-06
CN103857881A (zh) 2014-06-11

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