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ATE410586T1 - Gekühltes bauteil einer strömungsmaschine und verfahren zum giessen dieses gekühlten bauteils - Google Patents

Gekühltes bauteil einer strömungsmaschine und verfahren zum giessen dieses gekühlten bauteils

Info

Publication number
ATE410586T1
ATE410586T1 AT04017673T AT04017673T ATE410586T1 AT E410586 T1 ATE410586 T1 AT E410586T1 AT 04017673 T AT04017673 T AT 04017673T AT 04017673 T AT04017673 T AT 04017673T AT E410586 T1 ATE410586 T1 AT E410586T1
Authority
AT
Austria
Prior art keywords
cooled component
casting
cooling channel
flow machine
cooled
Prior art date
Application number
AT04017673T
Other languages
English (en)
Inventor
Juergen Dellmann
Gernot Lang
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Application granted granted Critical
Publication of ATE410586T1 publication Critical patent/ATE410586T1/de

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/08—Cooling thereof; Tube walls
    • F23M5/085—Cooling thereof; Tube walls using air or other gas as the cooling medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/25—Three-dimensional helical
    • 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

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)
AT04017673T 2004-07-26 2004-07-26 Gekühltes bauteil einer strömungsmaschine und verfahren zum giessen dieses gekühlten bauteils ATE410586T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP04017673A EP1621730B1 (de) 2004-07-26 2004-07-26 Gekühltes Bauteil einer Strömungsmaschine und Verfahren zum Giessen dieses gekühlten Bauteils

Publications (1)

Publication Number Publication Date
ATE410586T1 true ATE410586T1 (de) 2008-10-15

Family

ID=34925939

Family Applications (1)

Application Number Title Priority Date Filing Date
AT04017673T ATE410586T1 (de) 2004-07-26 2004-07-26 Gekühltes bauteil einer strömungsmaschine und verfahren zum giessen dieses gekühlten bauteils

Country Status (6)

Country Link
US (1) US7824156B2 (de)
EP (1) EP1621730B1 (de)
CN (1) CN1727643B (de)
AT (1) ATE410586T1 (de)
DE (1) DE502004008210D1 (de)
ES (1) ES2312890T3 (de)

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US7665965B1 (en) * 2007-01-17 2010-02-23 Florida Turbine Technologies, Inc. Turbine rotor disk with dirt particle separator
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US10689986B1 (en) * 2012-06-01 2020-06-23 United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration High blowing ratio high effectiveness film cooling configurations
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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
US9850762B2 (en) 2013-03-13 2017-12-26 General Electric Company Dust mitigation for turbine blade tip turns
EP3039340B1 (de) * 2013-08-30 2018-11-28 United Technologies Corporation Vena-contracta-verwirbelungs-verdünnungspassagen für eine gasturbinenmotor-brennkammer
US20160199954A1 (en) * 2013-09-09 2016-07-14 Siemens Aktiengesellschaft Combustion chamber for a gas turbine, and tool and method for producing cooling ducts in a gas turbine component
WO2015094531A1 (en) * 2013-12-20 2015-06-25 United Technologies Corporation Gas turbine engine component cooling cavity with vortex promoting features
KR101509385B1 (ko) * 2014-01-16 2015-04-07 두산중공업 주식회사 스월링 냉각 채널을 구비한 터빈 블레이드 및 그 냉각 방법
US20150204197A1 (en) * 2014-01-23 2015-07-23 Siemens Aktiengesellschaft Airfoil leading edge chamber cooling with angled impingement
US20150260048A1 (en) * 2014-03-11 2015-09-17 United Technologies Corporation Component with cooling hole having helical groove
US9932835B2 (en) * 2014-05-23 2018-04-03 United Technologies Corporation Airfoil cooling device and method of manufacture
US10690055B2 (en) 2014-05-29 2020-06-23 General Electric Company Engine components with impingement cooling features
US9957816B2 (en) 2014-05-29 2018-05-01 General Electric Company Angled impingement insert
US10422235B2 (en) 2014-05-29 2019-09-24 General Electric Company Angled impingement inserts with cooling features
US10364684B2 (en) 2014-05-29 2019-07-30 General Electric Company Fastback vorticor pin
US10563514B2 (en) 2014-05-29 2020-02-18 General Electric Company Fastback turbulator
WO2016014056A1 (en) * 2014-07-24 2016-01-28 Siemens Aktiengesellschaft Turbine airfoil cooling system with spanwise extending flow blockers
US10012090B2 (en) * 2014-07-25 2018-07-03 United Technologies Corporation Airfoil cooling apparatus
JP5679246B1 (ja) * 2014-08-04 2015-03-04 三菱日立パワーシステムズ株式会社 ガスタービンの高温部品、これを備えるガスタービン、及びガスタービンの高温部品の製造方法
JP6437099B2 (ja) * 2014-08-26 2018-12-12 シーメンス エナジー インコーポレイテッド タービンエンジンの燃焼器内における燃料ノズル用の冷却システム
US10697306B2 (en) 2014-09-18 2020-06-30 Siemens Aktiengesellschaft Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoil
US10280785B2 (en) 2014-10-31 2019-05-07 General Electric Company Shroud assembly for a turbine engine
US10233775B2 (en) 2014-10-31 2019-03-19 General Electric Company Engine component for a gas turbine engine
KR101609562B1 (ko) 2014-11-27 2016-04-06 한국항공우주연구원 유동 안내부를 갖는 터빈 블레이드
WO2016160029A1 (en) 2015-04-03 2016-10-06 Siemens Aktiengesellschaft Turbine blade trailing edge with low flow framing channel
US10577947B2 (en) * 2015-12-07 2020-03-03 United Technologies Corporation Baffle insert for a gas turbine engine component
DE102016221566A1 (de) * 2016-11-03 2018-05-03 Bayerische Motoren Werke Aktiengesellschaft Wasserabscheider zum Abscheiden von Wasser in einem Fahrzeug
GB2574368A (en) * 2018-04-09 2019-12-11 Rolls Royce Plc Coolant channel with interlaced ribs
GB201902997D0 (en) 2019-03-06 2019-04-17 Rolls Royce Plc Coolant channel
CN110700896B (zh) * 2019-11-29 2020-09-01 四川大学 具有旋流冲击冷却结构的燃气轮机涡轮转子叶片
US11441778B2 (en) * 2019-12-20 2022-09-13 Raytheon Technologies Corporation Article with cooling holes and method of forming the same
CN115247575B (zh) * 2022-05-12 2024-05-03 中国航发四川燃气涡轮研究院 一种螺旋状涡轮叶片冷却单元及冷却结构
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Also Published As

Publication number Publication date
DE502004008210D1 (de) 2008-11-20
US20070014664A1 (en) 2007-01-18
CN1727643B (zh) 2010-12-15
EP1621730A1 (de) 2006-02-01
EP1621730B1 (de) 2008-10-08
CN1727643A (zh) 2006-02-01
US7824156B2 (en) 2010-11-02
ES2312890T3 (es) 2009-03-01

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