PL1834066T3 - Łopatka turbinowa do turbiny gazowej, zastosowanie łopatki turbinowej oraz sposób chłodzenia łopatki turbinowej - Google Patents

Łopatka turbinowa do turbiny gazowej, zastosowanie łopatki turbinowej oraz sposób chłodzenia łopatki turbinowej

Info

Publication number
PL1834066T3
PL1834066T3 PL05807981T PL05807981T PL1834066T3 PL 1834066 T3 PL1834066 T3 PL 1834066T3 PL 05807981 T PL05807981 T PL 05807981T PL 05807981 T PL05807981 T PL 05807981T PL 1834066 T3 PL1834066 T3 PL 1834066T3
Authority
PL
Poland
Prior art keywords
turbine blade
turbine
blade
cooling
rear edge
Prior art date
Application number
PL05807981T
Other languages
English (en)
Inventor
Stefan Baldauf
Michael Händler
Christian Lerner
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
Publication of PL1834066T3 publication Critical patent/PL1834066T3/pl

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • F05D2240/127Vortex generators, turbulators, or the like, for mixing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/24Three-dimensional ellipsoidal
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/24Three-dimensional ellipsoidal
    • F05D2250/241Three-dimensional ellipsoidal spherical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/202Heat transfer, e.g. cooling by film cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2212Improvement of heat transfer by creating turbulence
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2214Improvement of heat transfer by increasing the heat transfer surface
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
PL05807981T 2004-11-23 2005-11-07 Łopatka turbinowa do turbiny gazowej, zastosowanie łopatki turbinowej oraz sposób chłodzenia łopatki turbinowej PL1834066T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP04027789A EP1659262A1 (de) 2004-11-23 2004-11-23 Turbinenschaufel für eine Gasturbine, Verwendung einer Turbinenschaufel sowie Verfahren zum Kühlen einer Turbinenschaufel
EP05807981A EP1834066B1 (de) 2004-11-23 2005-11-07 Turbinenschaufel für eine gasturbine, verwendung einer turbinenschaufel sowie verfahren zum kühlen einer turbinenschaufel
PCT/EP2005/055779 WO2006056525A1 (de) 2004-11-23 2005-11-07 Turbinenschaufel für eine gasturbine, verwendung einer turbinenschaufel sowie verfahren zum kühlen einer turbinenschaufel

Publications (1)

Publication Number Publication Date
PL1834066T3 true PL1834066T3 (pl) 2010-03-31

Family

ID=34927494

Family Applications (1)

Application Number Title Priority Date Filing Date
PL05807981T PL1834066T3 (pl) 2004-11-23 2005-11-07 Łopatka turbinowa do turbiny gazowej, zastosowanie łopatki turbinowej oraz sposób chłodzenia łopatki turbinowej

Country Status (10)

Country Link
US (1) US7766616B2 (pl)
EP (2) EP1659262A1 (pl)
JP (1) JP2008520890A (pl)
CN (1) CN100575672C (pl)
AT (1) ATE445085T1 (pl)
DE (1) DE502005008298D1 (pl)
ES (1) ES2333242T3 (pl)
PL (1) PL1834066T3 (pl)
RU (1) RU2393356C2 (pl)
WO (1) WO2006056525A1 (pl)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7766615B2 (en) * 2007-02-21 2010-08-03 United Technlogies Corporation Local indented trailing edge heat transfer devices
US7815414B2 (en) * 2007-07-27 2010-10-19 United Technologies Corporation Airfoil mini-core plugging devices
JP2010043568A (ja) * 2008-08-11 2010-02-25 Ihi Corp タービン翼及びタービン翼後縁部の放熱促進部品
US8061989B1 (en) * 2008-10-20 2011-11-22 Florida Turbine Technologies, Inc. Turbine blade with near wall cooling
US20110033311A1 (en) * 2009-08-06 2011-02-10 Martin Nicholas F Turbine Airfoil Cooling System with Pin Fin Cooling Chambers
US20110268583A1 (en) * 2010-04-30 2011-11-03 General Electric Company Airfoil trailing edge and method of manufacturing the same
EP2418357A1 (en) * 2010-08-05 2012-02-15 Siemens Aktiengesellschaft Turbine airfoil and method for thermal barrier coating
JP2012189026A (ja) * 2011-03-11 2012-10-04 Ihi Corp タービン翼
CN103542748A (zh) * 2011-07-28 2014-01-29 上海交通大学 热沉的针肋-凹陷复合阵列结构及针肋-凹陷复合阵列的布置方法
CN102410687A (zh) * 2011-07-28 2012-04-11 上海交通大学 具有针肋-凹陷复合阵列的热沉及针肋-凹陷复合阵列的布置方法
JP6025110B2 (ja) 2011-11-30 2016-11-16 株式会社Ihi タービン翼
US9488052B2 (en) * 2012-02-10 2016-11-08 General Electric Technology Gmbh Method for reconditioning a blade of a gas turbine and also a reconditioned blade
US20130280093A1 (en) * 2012-04-24 2013-10-24 Mark F. Zelesky Gas turbine engine core providing exterior airfoil portion
US9644903B1 (en) 2012-06-01 2017-05-09 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Shaped recess flow control
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
US9732617B2 (en) * 2013-11-26 2017-08-15 General Electric Company Cooled airfoil trailing edge and method of cooling the airfoil trailing edge
US9957816B2 (en) 2014-05-29 2018-05-01 General Electric Company Angled impingement insert
US10364684B2 (en) 2014-05-29 2019-07-30 General Electric Company Fastback vorticor pin
CA2950011C (en) 2014-05-29 2020-01-28 General Electric Company Fastback turbulator
US10422235B2 (en) 2014-05-29 2019-09-24 General Electric Company Angled impingement inserts with cooling features
CA2949539A1 (en) 2014-05-29 2016-02-18 General Electric Company Engine components with impingement cooling features
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
US10260354B2 (en) 2016-02-12 2019-04-16 General Electric Company Airfoil trailing edge cooling
US20170234225A1 (en) * 2016-02-13 2017-08-17 General Electric Company Component cooling for a gas turbine engine
CN107269319A (zh) * 2017-06-01 2017-10-20 西北工业大学 一种带有球面凹坑的涡轮叶片尾缘扰流半劈缝冷却结构
CN107035421A (zh) * 2017-06-01 2017-08-11 西北工业大学 一种带有阵列针肋的涡轮叶片尾缘扰流半劈缝冷却结构
CN107013254A (zh) * 2017-06-01 2017-08-04 西北工业大学 一种带有球面凸块的涡轮叶片尾缘扰流半劈缝冷却结构
JP7168926B2 (ja) * 2018-03-28 2022-11-10 三菱重工業株式会社 フィルム冷却構造
CN109058173A (zh) * 2018-08-17 2018-12-21 大连凌海华威科技服务有限责任公司 凹坑型压气机叶片及其对叶栅内流动分离的控制方法
FR3102794B1 (fr) * 2019-10-31 2022-09-09 Safran Aircraft Engines Composant de turbomachine comportant des orifices de refroidissement ameliores
FR3107562B1 (fr) * 2020-02-20 2022-06-10 Safran Aube de turbomachine comportant des fentes de refroidissement de son bord de fuite équipées de perturbateurs
CN112682107B (zh) * 2020-12-20 2023-07-21 中国航发四川燃气涡轮研究院 带有穿孔肋的涡轮叶片尾缘冷却结构及方法和燃气轮机

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB679931A (en) * 1949-12-02 1952-09-24 Bristol Aeroplane Co Ltd Improvements in or relating to blades for turbines or the like
DE1601613A1 (de) * 1967-08-03 1970-12-17 Motoren Turbinen Union Turbinenschaufel,insbesondere Turbinenleitschaufel fuer Gasturbinentriebwerke
US4720239A (en) * 1982-10-22 1988-01-19 Owczarek Jerzy A Stator blades of turbomachines
US5243759A (en) * 1991-10-07 1993-09-14 United Technologies Corporation Method of casting to control the cooling air flow rate of the airfoil trailing edge
US5337568A (en) * 1993-04-05 1994-08-16 General Electric Company Micro-grooved heat transfer wall
FR2782118B1 (fr) * 1998-08-05 2000-09-15 Snecma Aube de turbine refroidie a bord de fuite amenage
US6183197B1 (en) * 1999-02-22 2001-02-06 General Electric Company Airfoil with reduced heat load
US6607355B2 (en) * 2001-10-09 2003-08-19 United Technologies Corporation Turbine airfoil with enhanced heat transfer
US6695582B2 (en) * 2002-06-06 2004-02-24 General Electric Company Turbine blade wall cooling apparatus and method of fabrication

Also Published As

Publication number Publication date
WO2006056525A1 (de) 2006-06-01
EP1659262A1 (de) 2006-05-24
DE502005008298D1 (de) 2009-11-19
RU2007123582A (ru) 2008-12-27
RU2393356C2 (ru) 2010-06-27
US20080124225A1 (en) 2008-05-29
ATE445085T1 (de) 2009-10-15
JP2008520890A (ja) 2008-06-19
CN100575672C (zh) 2009-12-30
US7766616B2 (en) 2010-08-03
EP1834066B1 (de) 2009-10-07
ES2333242T3 (es) 2010-02-18
EP1834066A1 (de) 2007-09-19
CN101057061A (zh) 2007-10-17

Similar Documents

Publication Publication Date Title
PL1834066T3 (pl) Łopatka turbinowa do turbiny gazowej, zastosowanie łopatki turbinowej oraz sposób chłodzenia łopatki turbinowej
TW200718859A (en) Peripheral microcircuit serpentine cooling for turbine airfoils
PL1706592T3 (pl) Łopatka turbiny i turbina gazowa z taką łopatką turbiny
EP1674659A3 (en) Turbine nozzle with bullnose step-down platform
EP1614860A3 (en) Turbine blade
EP1898052A3 (en) Flared tip turbine blade
EP1533477A3 (en) Dual coolant turbine blade
EP1788192A3 (en) Gas turbine bucket with cooled platform edge and method of cooling platform leading edge
EP1271481A3 (en) Negative pressure type head slider and disk drive employing same
EP1065343A3 (en) Airfoil leading edge cooling
GB2431888A (en) Golf club head with variable face thickness
SG134214A1 (en) Microcircuits for small engines
EP1298285A3 (en) Ramped tip shelf blade
PL1706593T3 (pl) Łopatka turbiny i turbina gazowa z taką łopatką
EP1882817A3 (en) Dust hole dome blade
EP1936118A3 (en) Turbine blade main core modifications for peripheral serpentine microcircuits
EP1647672A3 (en) Airfoil with impingement cooling of a large fillet
SE0201335L (sv) Vakuumpump och sätt att tillhandahålla undertryck
PL1774179T3 (pl) Łopatka sprężarki
EP1813774A3 (en) Turbine element cooling
TWI256435B (en) Cooled rotor blade with vibration damping device
EP2236767A3 (en) Gas turbine inner flowpath coverpiece
EP1749967A3 (en) Cooling arrangement for a gas turbine
PL1776539T3 (pl) Pierścień nacinający
CA2451402A1 (en) Knife and apparatus for clamping a knife