JP6001862B2 - タービン部品用の湾曲冷却通路 - Google Patents

タービン部品用の湾曲冷却通路 Download PDF

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Publication number
JP6001862B2
JP6001862B2 JP2012004728A JP2012004728A JP6001862B2 JP 6001862 B2 JP6001862 B2 JP 6001862B2 JP 2012004728 A JP2012004728 A JP 2012004728A JP 2012004728 A JP2012004728 A JP 2012004728A JP 6001862 B2 JP6001862 B2 JP 6001862B2
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JP
Japan
Prior art keywords
airfoil
cooling
curved
passages
cooling passages
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.)
Active
Application number
JP2012004728A
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English (en)
Japanese (ja)
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JP2012149641A5 (enExample
JP2012149641A (ja
Inventor
ベンジャミン・ポール・レーシー
ブライアン・ピーター・アーネス
ヴィクター・ジョン・モルガン
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 JP2012149641A publication Critical patent/JP2012149641A/ja
Publication of JP2012149641A5 publication Critical patent/JP2012149641A5/ja
Application granted granted Critical
Publication of JP6001862B2 publication Critical patent/JP6001862B2/ja
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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
    • F01D5/186—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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2012004728A 2011-01-14 2012-01-13 タービン部品用の湾曲冷却通路 Active JP6001862B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/006,914 US8753083B2 (en) 2011-01-14 2011-01-14 Curved cooling passages for a turbine component
US13/006,914 2011-01-14

Publications (3)

Publication Number Publication Date
JP2012149641A JP2012149641A (ja) 2012-08-09
JP2012149641A5 JP2012149641A5 (enExample) 2015-02-26
JP6001862B2 true JP6001862B2 (ja) 2016-10-05

Family

ID=46397768

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012004728A Active JP6001862B2 (ja) 2011-01-14 2012-01-13 タービン部品用の湾曲冷却通路

Country Status (5)

Country Link
US (1) US8753083B2 (enExample)
JP (1) JP6001862B2 (enExample)
CN (1) CN102606221B (enExample)
DE (1) DE102012100266B4 (enExample)
FR (1) FR2970502B1 (enExample)

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US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
US10190420B2 (en) * 2015-02-10 2019-01-29 United Technologies Corporation Flared crossovers for airfoils
US10502066B2 (en) * 2015-05-08 2019-12-10 United Technologies Corporation Turbine engine component including an axially aligned skin core passage interrupted by a pedestal
US10099284B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having a catalyzed internal passage defined therein
US9579714B1 (en) 2015-12-17 2017-02-28 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
US10118217B2 (en) 2015-12-17 2018-11-06 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10099276B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having an internal passage defined therein
US9968991B2 (en) 2015-12-17 2018-05-15 General Electric Company Method and assembly for forming components having internal passages using a lattice structure
US10137499B2 (en) 2015-12-17 2018-11-27 General Electric Company Method and assembly for forming components having an internal passage defined therein
US10150158B2 (en) 2015-12-17 2018-12-11 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10099283B2 (en) 2015-12-17 2018-10-16 General Electric Company Method and assembly for forming components having an internal passage defined therein
US9987677B2 (en) 2015-12-17 2018-06-05 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10046389B2 (en) 2015-12-17 2018-08-14 General Electric Company Method and assembly for forming components having internal passages using a jacketed core
US10286450B2 (en) 2016-04-27 2019-05-14 General Electric Company Method and assembly for forming components using a jacketed core
US10335853B2 (en) 2016-04-27 2019-07-02 General Electric Company Method and assembly for forming components using a jacketed core
US10436048B2 (en) * 2016-08-12 2019-10-08 General Electric Comapny Systems for removing heat from turbine components
US20180179899A1 (en) * 2016-12-22 2018-06-28 General Electric Company Method and apparatus for brazed engine components
US10760430B2 (en) 2017-05-31 2020-09-01 General Electric Company Adaptively opening backup cooling pathway
US11041389B2 (en) 2017-05-31 2021-06-22 General Electric Company Adaptive cover for cooling pathway by additive manufacture
US10704399B2 (en) 2017-05-31 2020-07-07 General Electric Company Adaptively opening cooling pathway
US10927680B2 (en) 2017-05-31 2021-02-23 General Electric Company Adaptive cover for cooling pathway by additive manufacture
US10837291B2 (en) * 2017-11-17 2020-11-17 General Electric Company Turbine engine with component having a cooled tip
US10830053B2 (en) * 2017-11-20 2020-11-10 General Electric Company Engine component cooling hole
US10570750B2 (en) 2017-12-06 2020-02-25 General Electric Company Turbine component with tip rail cooling passage
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CN113153446B (zh) * 2021-04-15 2022-08-02 中国航发湖南动力机械研究所 一种涡轮导向器及具有其的大膨胀比向心涡轮
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GB2638477A (en) * 2024-02-26 2025-08-27 Siemens Energy Global Gmbh & Co Kg Airfoil for turbine vane or turbine blade of an axial gas turbine

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Also Published As

Publication number Publication date
CN102606221B (zh) 2015-07-15
CN102606221A (zh) 2012-07-25
US20120183412A1 (en) 2012-07-19
FR2970502B1 (fr) 2019-12-13
DE102012100266A1 (de) 2012-07-19
FR2970502A1 (fr) 2012-07-20
US8753083B2 (en) 2014-06-17
JP2012149641A (ja) 2012-08-09
DE102012100266B4 (de) 2025-03-20

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