WO2018164148A8 - タービン翼の冷却構造 - Google Patents

タービン翼の冷却構造 Download PDF

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Publication number
WO2018164148A8
WO2018164148A8 PCT/JP2018/008643 JP2018008643W WO2018164148A8 WO 2018164148 A8 WO2018164148 A8 WO 2018164148A8 JP 2018008643 W JP2018008643 W JP 2018008643W WO 2018164148 A8 WO2018164148 A8 WO 2018164148A8
Authority
WO
WIPO (PCT)
Prior art keywords
rib
lattice
ribs
pair
turbine airfoil
Prior art date
Application number
PCT/JP2018/008643
Other languages
English (en)
French (fr)
Other versions
WO2018164148A1 (ja
Inventor
智子 都留
克彦 石田
Original Assignee
川崎重工業株式会社
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 川崎重工業株式会社 filed Critical 川崎重工業株式会社
Priority to CN201880014035.7A priority Critical patent/CN110392769B/zh
Priority to GB1912921.2A priority patent/GB2574532B/en
Priority to DE112018001282.4T priority patent/DE112018001282B4/de
Publication of WO2018164148A1 publication Critical patent/WO2018164148A1/ja
Priority to US16/558,646 priority patent/US11578659B2/en
Publication of WO2018164148A8 publication Critical patent/WO2018164148A8/ja

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
    • 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
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • 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
    • 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
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/185—Two-dimensional patterned serpentine-like
    • 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
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/282—Three-dimensional patterned cubic pattern
    • 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

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)

Abstract

タービン翼（１）の冷却構造において、冷却通路（１７）に配置された第１リブ組（３３Ａ）および第２リブ組（３３Ｂ）とが互いに格子状に重ねられて構成されたラティス構造体（２３）であって、第１リブ組のリブ間に形成された流路（３７）と第２リブ組のリブ間に形成された流路（３７）とを互いに連通させるラティス連通部（２３ａ）を有するラティス構造体（２３）を設け、前記第１，第２リブ組（３３Ａ，３３Ｂ）が、それぞれ、冷却媒体（ＣＬ）の移動方向（Ｍ）に延びる仮想境界線（Ｌ）に対して互いに逆向きに傾斜し、かつ仮想境界線（Ｌ）上で互いに接する１対のリブからなるリブ壁（３５）を有しており、前記リブ壁（３５）を形成する各リブ（３１，３１）の両端部における２つのラティス連通部（２３ａ）の間に複数のラティス連通部が形成されている。
PCT/JP2018/008643 2017-03-10 2018-03-06 タービン翼の冷却構造 WO2018164148A1 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
CN201880014035.7A CN110392769B (zh) 2017-03-10 2018-03-06 涡轮叶片的冷却结构
GB1912921.2A GB2574532B (en) 2017-03-10 2018-03-06 Cooling structure for turbine airfoil
DE112018001282.4T DE112018001282B4 (de) 2017-03-10 2018-03-06 Kühlstruktur für eine Turbinenschaufel
US16/558,646 US11578659B2 (en) 2017-03-10 2019-09-03 Cooling structure for turbine airfoil

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2017045925A JP6906332B2 (ja) 2017-03-10 2017-03-10 タービン翼の冷却構造
JP2017-045925 2017-03-10

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US16/558,646 Continuation US11578659B2 (en) 2017-03-10 2019-09-03 Cooling structure for turbine airfoil

Publications (2)

Publication Number Publication Date
WO2018164148A1 WO2018164148A1 (ja) 2018-09-13
WO2018164148A8 true WO2018164148A8 (ja) 2019-09-06

Family

ID=63447838

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2018/008643 WO2018164148A1 (ja) 2017-03-10 2018-03-06 タービン翼の冷却構造

Country Status (6)

Country Link
US (1) US11578659B2 (ja)
JP (1) JP6906332B2 (ja)
CN (1) CN110392769B (ja)
DE (1) DE112018001282B4 (ja)
GB (1) GB2574532B (ja)
WO (1) WO2018164148A1 (ja)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021050688A (ja) * 2019-09-26 2021-04-01 川崎重工業株式会社 タービン翼
CN111335964B (zh) * 2020-03-09 2021-01-05 北京南方斯奈克玛涡轮技术有限公司 一种增材制造的发动机涡轮冷却叶片
CN113623010B (zh) * 2021-07-13 2022-11-29 哈尔滨工业大学 涡轮叶片

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4407632A (en) * 1981-06-26 1983-10-04 United Technologies Corporation Airfoil pedestaled trailing edge region cooling configuration
US5603606A (en) 1994-11-14 1997-02-18 Solar Turbines Incorporated Turbine cooling system
JP3035187B2 (ja) * 1995-05-09 2000-04-17 東北電力株式会社 ガスタービン中空冷却動翼
DE19634238A1 (de) * 1996-08-23 1998-02-26 Asea Brown Boveri Kühlbare Schaufel
SE512384C2 (sv) * 1998-05-25 2000-03-06 Abb Ab Komponent för en gasturbin
US6634858B2 (en) * 2001-06-11 2003-10-21 Alstom (Switzerland) Ltd Gas turbine airfoil
US6969233B2 (en) * 2003-02-27 2005-11-29 General Electric Company Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity
SE526847C2 (sv) * 2004-02-27 2005-11-08 Demag Delaval Ind Turbomachine En komponent som innefattar en ledskena eller ett rotorblad för en gasturbin
JP4957131B2 (ja) 2006-09-06 2012-06-20 株式会社Ｉｈｉ 冷却構造
US8556583B2 (en) * 2007-08-30 2013-10-15 Mitsubishi Heavy Industries, Ltd. Blade cooling structure of gas turbine
JP2009221995A (ja) * 2008-03-18 2009-10-01 Ihi Corp 高温部品の内面冷却構造
US8182203B2 (en) * 2009-03-26 2012-05-22 Mitsubishi Heavy Industries, Ltd. Turbine blade and gas turbine
EP2378073A1 (en) * 2010-04-14 2011-10-19 Siemens Aktiengesellschaft Blade or vane for a turbomachine
US20140328669A1 (en) * 2011-11-25 2014-11-06 Siemens Aktiengesellschaft Airfoil with cooling passages
US9004866B2 (en) * 2011-12-06 2015-04-14 Siemens Aktiengesellschaft Turbine blade incorporating trailing edge cooling design
JP6036424B2 (ja) * 2013-03-14 2016-11-30 株式会社Ihi 冷却促進構造
JP6064700B2 (ja) * 2013-03-14 2017-01-25 株式会社ジェイテクト 電磁クラッチ装置、四輪駆動車、電磁クラッチの制御方法、及び四輪駆動車の制御方法
WO2015147672A1 (en) * 2014-03-27 2015-10-01 Siemens Aktiengesellschaft Blade for a gas turbine and method of cooling the blade
GB2533315B (en) * 2014-12-16 2017-04-12 Rolls Royce Plc Cooling of engine components
JP2016125380A (ja) * 2014-12-26 2016-07-11 川崎重工業株式会社 タービン翼の冷却構造

Also Published As

Publication number Publication date
CN110392769B (zh) 2022-03-22
GB2574532A (en) 2019-12-11
GB201912921D0 (en) 2019-10-23
CN110392769A (zh) 2019-10-29
DE112018001282T5 (de) 2019-11-21
JP2018150827A (ja) 2018-09-27
DE112018001282B4 (de) 2023-02-16
US20200018235A1 (en) 2020-01-16
JP6906332B2 (ja) 2021-07-21
US11578659B2 (en) 2023-02-14
GB2574532B (en) 2022-03-02
WO2018164148A1 (ja) 2018-09-13

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