CH702551B8 - Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen. - Google Patents

Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen. Download PDF

Info

Publication number
CH702551B8
CH702551B8 CH00004/11A CH42011A CH702551B8 CH 702551 B8 CH702551 B8 CH 702551B8 CH 00004/11 A CH00004/11 A CH 00004/11A CH 42011 A CH42011 A CH 42011A CH 702551 B8 CH702551 B8 CH 702551B8
Authority
CH
Switzerland
Prior art keywords
airfoil
vortex generators
trailing edge
internal cooling
cooling cavities
Prior art date
Application number
CH00004/11A
Other languages
English (en)
Other versions
CH702551A2 (de
CH702551B1 (de
Inventor
Jaime Maldonado
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH702551A2 publication Critical patent/CH702551A2/de
Priority to EP12405004.8A priority Critical patent/EP2500458B1/de
Publication of CH702551B1 publication Critical patent/CH702551B1/de
Publication of CH702551B8 publication Critical patent/CH702551B8/de

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
    • 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
    • F01D5/186Film 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
    • F05D2240/122Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
    • 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
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/304Characteristics 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
    • 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
    • F05D2260/22141Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Ein Schaufelblatt (10) enthält eine Vorderkante (12), eine Hinterkante (14), eine Saugseite (16) und eine Druckseite (18), wobei sich mehrere innere Hohlräume (20, 22, 24) innerhalb des Schaufelblattes (10) in Radialrichtung erstrecken, wobei sich ein erster innerer Hohlraum (24) entlang der Hinterkante (14) erstreckt. Die Hinterkante (14) ist mit mehreren entlang dieser angeordneten Kühlmittelaustrittsöffnungen versehen. Mehrere Wirbelgeneratoren sind auf einer Innenfläche der Druckseite (18) und/oder der Saugseite (16) des Schaufelblattes (10) ausgebildet. Die Wirbelgeneratoren sind erfindungsgemäss in einer radial voneinander beabstandeten Anordnung im hinteren inneren Hohlraum (24) angeordnet und erstrecken sich im Wesentlichen parallel zu der Hinterkante (14).
CH00004/11A 2010-01-06 2011-01-03 Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen. CH702551B8 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP12405004.8A EP2500458B1 (de) 2011-01-03 2012-01-09 Aktivierungsvorrichtung zur weg-und zeitabhängigen Bewegung einer Fadenschneid- und Anstickeinheit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/683,133 US8439628B2 (en) 2010-01-06 2010-01-06 Heat transfer enhancement in internal cavities of turbine engine airfoils

Publications (3)

Publication Number Publication Date
CH702551A2 CH702551A2 (de) 2011-07-15
CH702551B1 CH702551B1 (de) 2015-09-15
CH702551B8 true CH702551B8 (de) 2015-11-30

Family

ID=44215088

Family Applications (1)

Application Number Title Priority Date Filing Date
CH00004/11A CH702551B8 (de) 2010-01-06 2011-01-03 Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen.

Country Status (5)

Country Link
US (1) US8439628B2 (de)
JP (1) JP5898841B2 (de)
CN (1) CN102116177B (de)
CH (1) CH702551B8 (de)
DE (1) DE102010061376A1 (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8757701B2 (en) * 2010-01-15 2014-06-24 Aeroserve Technologies, Ltd. Drag reduction device for transport vehicles having randomized irregular shaped edge vortex generating channels
US9249675B2 (en) 2011-08-30 2016-02-02 General Electric Company Pin-fin array
US9506351B2 (en) 2012-04-27 2016-11-29 General Electric Company Durable turbine vane
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
US20150003962A1 (en) * 2013-06-27 2015-01-01 Bruce L. Smith Apparatus for reducing a temperature gradient of mainstream fluid downstream of an airfoil in a gas turbine engine
JP6245740B2 (ja) * 2013-11-20 2017-12-13 三菱日立パワーシステムズ株式会社 ガスタービン翼
EP2886797B1 (de) * 2013-12-20 2018-11-28 Ansaldo Energia Switzerland AG Ein hohle gekühlte Rotor- oder Leitschaufel einer Gasturbine, wobei die kühlkanäle Stifte mit Verbindungsstreben beinhalten
WO2015094531A1 (en) 2013-12-20 2015-06-25 United Technologies Corporation Gas turbine engine component cooling cavity with vortex promoting features
WO2015154729A1 (en) * 2014-04-07 2015-10-15 Prihoda S.R.O. Air-conditioning element for air distribution
US9476406B2 (en) * 2014-04-14 2016-10-25 Siemens Aktiengesellschaft Vortex generators aligned with trailing edge features on wind turbine blade
US9957816B2 (en) 2014-05-29 2018-05-01 General Electric Company Angled impingement insert
EP3149279A1 (de) 2014-05-29 2017-04-05 General Electric Company Fastback-turbulator
US10364684B2 (en) 2014-05-29 2019-07-30 General Electric Company Fastback vorticor pin
US10422235B2 (en) 2014-05-29 2019-09-24 General Electric Company Angled impingement inserts with cooling features
EP3149284A2 (de) 2014-05-29 2017-04-05 General Electric Company Motorkomponenten mit prallkühlungsfunktionen
US10233775B2 (en) 2014-10-31 2019-03-19 General Electric Company Engine component for a gas turbine engine
US10280785B2 (en) 2014-10-31 2019-05-07 General Electric Company Shroud assembly for a turbine engine
US9777635B2 (en) * 2014-12-31 2017-10-03 General Electric Company Engine component
EP3436669B1 (de) * 2016-03-31 2023-06-07 Siemens Energy Global GmbH & Co. KG Turbinenschaufel mit internen kühlkanälen mit strömungsteilung
US10655477B2 (en) * 2016-07-26 2020-05-19 General Electric Company Turbine components and method for forming turbine components
WO2018186891A1 (en) * 2017-04-07 2018-10-11 General Electric Company Cooling assembly for a turbine assembly
US10494948B2 (en) * 2017-05-09 2019-12-03 General Electric Company Impingement insert
CN106988790A (zh) * 2017-06-08 2017-07-28 哈尔滨工业大学 一种高温涡轮动叶顶部对转涡的冷却结构
US10458253B2 (en) 2018-01-08 2019-10-29 United Technologies Corporation Gas turbine engine components having internal hybrid cooling cavities
CN108910019B (zh) * 2018-07-05 2020-03-31 中国空气动力研究与发展中心高速空气动力研究所 一种采用热双金属微锯齿结构的空气流动控制系统
CN114763748A (zh) * 2021-01-12 2022-07-19 上海交通大学 带有表面微型涡发生器的气膜冷却结构

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4655419A (en) 1984-12-31 1987-04-07 The Boeing Company Vortex generator
US4787442A (en) 1987-12-04 1988-11-29 Carrier Corporation Delta wing and ramp wing enhanced plate fin
US5695321A (en) 1991-12-17 1997-12-09 General Electric Company Turbine blade having variable configuration turbulators
US5695320A (en) 1991-12-17 1997-12-09 General Electric Company Turbine blade having auxiliary turbulators
US5681144A (en) 1991-12-17 1997-10-28 General Electric Company Turbine blade having offset turbulators
JP3040590B2 (ja) * 1992-05-11 2000-05-15 三菱重工業株式会社 ガスタービン翼
US5361828A (en) * 1993-02-17 1994-11-08 General Electric Company Scaled heat transfer surface with protruding ramp surface turbulators
JP3192854B2 (ja) * 1993-12-28 2001-07-30 株式会社東芝 タービン冷却翼
WO1996015357A1 (en) 1994-11-10 1996-05-23 Westinghouse Electric Corporation Gas turbine vane with a cooled inner shroud
US5598990A (en) 1994-12-15 1997-02-04 University Of Kansas Center For Research Inc. Supersonic vortex generator
US5797726A (en) 1997-01-03 1998-08-25 General Electric Company Turbulator configuration for cooling passages or rotor blade in a gas turbine engine
EP1022435B1 (de) 1999-01-25 2009-06-03 General Electric Company Interner Kühlkreislauf für eine Gasturbinenschaufel
US6174134B1 (en) * 1999-03-05 2001-01-16 General Electric Company Multiple impingement airfoil cooling
US6406254B1 (en) 1999-05-10 2002-06-18 General Electric Company Cooling circuit for steam and air-cooled turbine nozzle stage
US6200087B1 (en) * 1999-05-10 2001-03-13 General Electric Company Pressure compensated turbine nozzle
US6273682B1 (en) 1999-08-23 2001-08-14 General Electric Company Turbine blade with preferentially-cooled trailing edge pressure wall
ATE355918T1 (de) 1999-12-08 2007-03-15 Gen Electric Kern zur einstellung der wanddicke einer turbinenschaufel und verfahren
NL1014151C2 (nl) * 2000-01-21 2001-07-24 Inalfa Ind Bv Open-dakconstructie voor een voertuig.
US6777836B2 (en) 2000-12-20 2004-08-17 General Electric Company Heat transfer enhancement at generator stator core space blocks
GB0114503D0 (en) * 2001-06-14 2001-08-08 Rolls Royce Plc Air cooled aerofoil
US6837465B2 (en) 2003-01-03 2005-01-04 Orbital Research Inc Flow control device and method of controlling flow
TW200503608A (en) * 2003-07-15 2005-01-16 Ind Tech Res Inst Cooling plate having vortices generator
US7097425B2 (en) * 2003-08-08 2006-08-29 United Technologies Corporation Microcircuit cooling for a turbine airfoil
US6916150B2 (en) * 2003-11-26 2005-07-12 Siemens Westinghouse Power Corporation Cooling system for a tip of a turbine blade
US7094031B2 (en) 2004-09-09 2006-08-22 General Electric Company Offset Coriolis turbulator blade
US7699583B2 (en) * 2006-07-21 2010-04-20 United Technologies Corporation Serpentine microcircuit vortex turbulatons for blade cooling
US7637720B1 (en) * 2006-11-16 2009-12-29 Florida Turbine Technologies, Inc. Turbulator for a turbine airfoil cooling passage
US8186942B2 (en) * 2007-12-14 2012-05-29 United Technologies Corporation Nacelle assembly with turbulators
CH700321A1 (de) * 2009-01-30 2010-07-30 Alstom Technology Ltd Gekühlte schaufel für eine gasturbine.

Also Published As

Publication number Publication date
CH702551A2 (de) 2011-07-15
CN102116177B (zh) 2015-05-20
US8439628B2 (en) 2013-05-14
CH702551B1 (de) 2015-09-15
JP5898841B2 (ja) 2016-04-06
CN102116177A (zh) 2011-07-06
JP2011140951A (ja) 2011-07-21
US20110164960A1 (en) 2011-07-07
DE102010061376A1 (de) 2011-07-07

Similar Documents

Publication Publication Date Title
CH702551B8 (de) Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen.
WO2014070279A3 (en) Endwall contouring
EP2787171A3 (de) Schaufelgitter mit Seitenwandkonturierung und Strömungsmaschine
WO2015112225A3 (en) Gas turbine engine airfoil with leading edge trench and impingement cooling
WO2014021981A3 (en) Vortex generators for improved film effectiveness
JP2013139816A5 (de)
EP2390465A3 (de) Gasturbinenbauteil mit Chevron-förmigen Filmkühlungsbohrungen und verwandte Prozesse
JP2013130189A5 (de)
WO2014105270A3 (en) Airfoil assembly with paired endwall contouring
EP2615244A3 (de) Filmgekühlte Turbinenschaufel mit mehreren Furchensegmenten auf der Aussenfläche
JP2011140951A5 (de)
JP2014114810A5 (de)
WO2013180792A3 (en) Gas turbine engine airfoil trailing edge passage and core for making same
WO2012021194A3 (en) Component wall having diffusion sections for cooling in a turbine engine
EP2615245A3 (de) Filmgekühlte Turbinenschaufel mit Furchensegmenten auf der Aussenfläche
EP3032035A3 (de) Versetzte übergänge für tragflächen
EP2599962A3 (de) Abgestellte Schaufeltragflächenanordnung
EP2687680A3 (de) Axialturbine und Kraftwerk
EP3225781A3 (de) Schaufelkanal, schaufelgitter und strömungsmaschine
NZ609330A (en) Turbine rotor assembly
EP2738350A3 (de) Turbinenschaufel mit Duschkopf-Filmkühlungssystemen und Verfahren zur Herstellung einer verbesserten Schaufel mit Duschkopf-Filmkühlung einer Turbinenschaufel
WO2014163694A3 (en) Trenched cooling hole arrangement for a ceramic matrix composite vane
WO2014070280A3 (en) Endwall contouring
WO2014011253A3 (en) Turbine airfoil trailing edge cooling slots
WO2015163949A3 (en) Fan cooling hole array

Legal Events

Date Code Title Description
PK Correction

Free format text: BERICHTIGUNG ERFINDER

PK Correction

Free format text: ERFINDER BERICHTIGT.

NV New agent

Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH

PL Patent ceased