KR102066390B1 - 유로 형성판, 이것을 구비하는 유로 형성조 부재 및 정익, 가스 터빈, 유로 형성판의 제조 방법, 및 유로 형성판의 개조 방법 - Google Patents

유로 형성판, 이것을 구비하는 유로 형성조 부재 및 정익, 가스 터빈, 유로 형성판의 제조 방법, 및 유로 형성판의 개조 방법 Download PDF

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KR102066390B1
KR102066390B1 KR1020187014381A KR20187014381A KR102066390B1 KR 102066390 B1 KR102066390 B1 KR 102066390B1 KR 1020187014381 A KR1020187014381 A KR 1020187014381A KR 20187014381 A KR20187014381 A KR 20187014381A KR 102066390 B1 KR102066390 B1 KR 102066390B1
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shelf
flow path
plate
circumferential
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KR20180071347A (ko
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다다카즈 사카구치
히로시 시미즈
신지 요시다
요시오 후쿠이
마사미츠 구와바라
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미츠비시 히타치 파워 시스템즈 가부시키가이샤
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    • 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
    • F01D5/187—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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified therefor
    • 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
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • F05D2240/81—Cooled platforms
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
KR1020187014381A 2015-11-27 2016-11-17 유로 형성판, 이것을 구비하는 유로 형성조 부재 및 정익, 가스 터빈, 유로 형성판의 제조 방법, 및 유로 형성판의 개조 방법 Active KR102066390B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JPJP-P-2015-232100 2015-11-27
JP2015232100A JP6587251B2 (ja) 2015-11-27 2015-11-27 流路形成板、これを備える流路形成組部材及び静翼、ガスタービン、流路形成板の製造方法、並びに流路形成板の改造方法
PCT/JP2016/084080 WO2017090502A1 (ja) 2015-11-27 2016-11-17 流路形成板、これを備える流路形成部材及び静翼、ガスタービン、流路形成板の製造方法、並びに流路形成板の改造方法

Publications (2)

Publication Number Publication Date
KR20180071347A KR20180071347A (ko) 2018-06-27
KR102066390B1 true KR102066390B1 (ko) 2020-01-15

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KR1020187014381A Active KR102066390B1 (ko) 2015-11-27 2016-11-17 유로 형성판, 이것을 구비하는 유로 형성조 부재 및 정익, 가스 터빈, 유로 형성판의 제조 방법, 및 유로 형성판의 개조 방법

Country Status (7)

Country Link
US (1) US10704394B2 (enExample)
EP (1) EP3361054B1 (enExample)
JP (1) JP6587251B2 (enExample)
KR (1) KR102066390B1 (enExample)
CN (1) CN108291450B (enExample)
TW (1) TWI605187B (enExample)
WO (1) WO2017090502A1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10975721B2 (en) * 2016-01-12 2021-04-13 Pratt & Whitney Canada Corp. Cooled containment case using internal plenum
DE112018002030T5 (de) 2017-05-15 2020-01-16 Ngk Insulators, Ltd. Partikelzähler
US11131212B2 (en) 2017-12-06 2021-09-28 Raytheon Technologies Corporation Gas turbine engine cooling component
US10648351B2 (en) * 2017-12-06 2020-05-12 United Technologies Corporation Gas turbine engine cooling component
KR102207971B1 (ko) 2019-06-21 2021-01-26 두산중공업 주식회사 터빈 베인, 및 이를 포함하는 터빈
JP6799702B1 (ja) * 2020-03-19 2020-12-16 三菱パワー株式会社 静翼及びガスタービン
RU2735972C1 (ru) * 2020-05-10 2020-11-11 Владимир Дмитриевич Куликов Система воздушно-жидкостного охлаждения лопаток ступеней турбины турбореактивного двигателя
JP6963701B1 (ja) * 2021-02-01 2021-11-10 三菱パワー株式会社 ガスタービン静翼およびガスタービン
US12173619B2 (en) 2022-05-02 2024-12-24 Siemens Energy Global GmbH & Co. KG Turbine component having platform cooling circuit
US12305532B2 (en) * 2022-11-16 2025-05-20 Mitsubishi Heavy Industries, Ltd. Cooling method and structure of vane of gas turbine

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003083001A (ja) * 2001-09-13 2003-03-19 Hitachi Ltd ガスタービン及びその静翼
US20100129196A1 (en) * 2008-11-26 2010-05-27 Alstom Technologies Ltd. Llc Cooled gas turbine vane assembly

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE755567A (fr) * 1969-12-01 1971-02-15 Gen Electric Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe
US4321119A (en) 1979-11-07 1982-03-23 Gelman Sciences, Inc. Buffer composition and method for the electrophoretic separation of proteins
US4693667A (en) 1980-04-29 1987-09-15 Teledyne Industries, Inc. Turbine inlet nozzle with cooling means
US5634766A (en) * 1994-08-23 1997-06-03 General Electric Co. Turbine stator vane segments having combined air and steam cooling circuits
JP3181216B2 (ja) 1996-02-23 2001-07-03 三菱重工業株式会社 ガスタービン静翼
JP2851577B2 (ja) 1996-02-26 1999-01-27 三菱重工業株式会社 ガスタービン静翼シュラウドにおける冷却空気流路の加工方法
JP4698847B2 (ja) * 2001-01-19 2011-06-08 三菱重工業株式会社 ガスタービン分割環
US7416391B2 (en) 2006-02-24 2008-08-26 General Electric Company Bucket platform cooling circuit and method
EP2282012B1 (en) 2009-07-03 2015-11-25 Alstom Technology Ltd Method for replacing a cover plate of a guide vane of a gas turbine
US8684664B2 (en) * 2010-09-30 2014-04-01 General Electric Company Apparatus and methods for cooling platform regions of turbine rotor blades
US8517667B1 (en) 2010-11-22 2013-08-27 Florida Turbine Technologies, Inc. Turbine vane with counter flow cooling passages
US9080458B2 (en) * 2011-08-23 2015-07-14 United Technologies Corporation Blade outer air seal with multi impingement plate assembly
EP2971532A4 (en) * 2013-03-15 2016-11-16 United Technologies Corp ADDITIVE FOR THE MANUFACTURE OF DEFLECTORS, COVERS AND MATRICES
JP5676040B1 (ja) * 2014-06-30 2015-02-25 三菱日立パワーシステムズ株式会社 静翼、これを備えているガスタービン、静翼の製造方法、及び静翼の改造方法
EP3232002A1 (en) * 2016-04-11 2017-10-18 Rolls-Royce Corporation Impingement plate with stress relief feature

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003083001A (ja) * 2001-09-13 2003-03-19 Hitachi Ltd ガスタービン及びその静翼
US20100129196A1 (en) * 2008-11-26 2010-05-27 Alstom Technologies Ltd. Llc Cooled gas turbine vane assembly

Also Published As

Publication number Publication date
JP2017096234A (ja) 2017-06-01
TW201732144A (zh) 2017-09-16
EP3361054B1 (en) 2020-03-04
EP3361054A1 (en) 2018-08-15
US20180347369A1 (en) 2018-12-06
US10704394B2 (en) 2020-07-07
KR20180071347A (ko) 2018-06-27
EP3361054A4 (en) 2018-12-12
JP6587251B2 (ja) 2019-10-09
CN108291450A (zh) 2018-07-17
CN108291450B (zh) 2020-11-06
WO2017090502A1 (ja) 2017-06-01
TWI605187B (zh) 2017-11-11

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