DE60122050D1 - Turbinenleitschaufel mit Einsatz mit Bereichen zur Prallkühlung und Konvektionskühlung - Google Patents

Turbinenleitschaufel mit Einsatz mit Bereichen zur Prallkühlung und Konvektionskühlung

Info

Publication number
DE60122050D1
DE60122050D1 DE60122050T DE60122050T DE60122050D1 DE 60122050 D1 DE60122050 D1 DE 60122050D1 DE 60122050 T DE60122050 T DE 60122050T DE 60122050 T DE60122050 T DE 60122050T DE 60122050 D1 DE60122050 D1 DE 60122050D1
Authority
DE
Germany
Prior art keywords
cooling
vane
insert
insert sleeve
impingement
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE60122050T
Other languages
English (en)
Other versions
DE60122050T2 (de
Inventor
Yufeng Phillip Yu
Sarah Osgood
Gary Michael Itzel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60122050D1 publication Critical patent/DE60122050D1/de
Publication of DE60122050T2 publication Critical patent/DE60122050T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • 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
    • 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
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
    • F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60122050T 2000-05-16 2001-01-10 Turbinenleitschaufel mit Einsatz mit Bereichen zur Prallkühlung und Konvektionskühlung Expired - Lifetime DE60122050T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US571835 2000-05-16
US09/571,835 US6468031B1 (en) 2000-05-16 2000-05-16 Nozzle cavity impingement/area reduction insert

Publications (2)

Publication Number Publication Date
DE60122050D1 true DE60122050D1 (de) 2006-09-21
DE60122050T2 DE60122050T2 (de) 2007-03-01

Family

ID=24285269

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60122050T Expired - Lifetime DE60122050T2 (de) 2000-05-16 2001-01-10 Turbinenleitschaufel mit Einsatz mit Bereichen zur Prallkühlung und Konvektionskühlung

Country Status (7)

Country Link
US (1) US6468031B1 (de)
EP (1) EP1156187B1 (de)
JP (1) JP4778621B2 (de)
KR (1) KR20010105148A (de)
AT (1) ATE335916T1 (de)
CZ (1) CZ20004335A3 (de)
DE (1) DE60122050T2 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6589010B2 (en) * 2001-08-27 2003-07-08 General Electric Company Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
GB2386926A (en) * 2002-03-27 2003-10-01 Alstom Two part impingement tube for a turbine blade or vane
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
US7008185B2 (en) * 2003-02-27 2006-03-07 General Electric Company Gas turbine engine turbine nozzle bifurcated impingement baffle
US6932568B2 (en) * 2003-02-27 2005-08-23 General Electric Company Turbine nozzle segment cantilevered mount
US6742984B1 (en) 2003-05-19 2004-06-01 General Electric Company Divided insert for steam cooled nozzles and method for supporting and separating divided insert
US7303372B2 (en) * 2005-11-18 2007-12-04 General Electric Company Methods and apparatus for cooling combustion turbine engine components
US7488156B2 (en) * 2006-06-06 2009-02-10 Siemens Energy, Inc. Turbine airfoil with floating wall mechanism and multi-metering diffusion technique
DE102007037208B4 (de) 2007-08-07 2013-06-20 Mtu Aero Engines Gmbh Turbinenschaufel mit zumindest einer Einsatzhülse zum Kühlen der Turbinenschaufel
GB0813839D0 (en) * 2008-07-30 2008-09-03 Rolls Royce Plc An aerofoil and method for making an aerofoil
US20100054915A1 (en) * 2008-08-28 2010-03-04 United Technologies Corporation Airfoil insert
US8714911B2 (en) * 2011-01-06 2014-05-06 General Electric Company Impingement plate for turbomachine components and components equipped therewith
US8840370B2 (en) 2011-11-04 2014-09-23 General Electric Company Bucket assembly for turbine system
US9151173B2 (en) * 2011-12-15 2015-10-06 General Electric Company Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components
US9328617B2 (en) * 2012-03-20 2016-05-03 United Technologies Corporation Trailing edge or tip flag antiflow separation
US9169733B2 (en) * 2013-03-20 2015-10-27 General Electric Company Turbine airfoil assembly
US20150064019A1 (en) * 2013-08-30 2015-03-05 General Electric Company Gas Turbine Components with Porous Cooling Features
ES2674241T3 (es) * 2014-03-13 2018-06-28 Bae Systems Plc Intercambiador de calor
EP2918957A1 (de) * 2014-03-13 2015-09-16 BAE Systems PLC Wärmetauscher
US10012092B2 (en) * 2015-08-12 2018-07-03 United Technologies Corporation Low turn loss baffle flow diverter
US10443407B2 (en) 2016-02-15 2019-10-15 General Electric Company Accelerator insert for a gas turbine engine airfoil
US10428660B2 (en) * 2017-01-31 2019-10-01 United Technologies Corporation Hybrid airfoil cooling
US10494948B2 (en) * 2017-05-09 2019-12-03 General Electric Company Impingement insert
US10577943B2 (en) 2017-05-11 2020-03-03 General Electric Company Turbine engine airfoil insert
US10815806B2 (en) * 2017-06-05 2020-10-27 General Electric Company Engine component with insert
US20240309810A1 (en) * 2023-03-14 2024-09-19 Raytheon Technologies Corporation Introducing steam into core air upstream of turbine engine diffuser plenum

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1467483A (en) * 1974-02-19 1977-03-16 Rolls Royce Cooled vane for a gas turbine engine
GB1565361A (en) * 1976-01-29 1980-04-16 Rolls Royce Blade or vane for a gas turbine engien
GB2119028B (en) * 1982-04-27 1985-02-27 Rolls Royce Aerofoil for a gas turbine engine
US4645415A (en) * 1983-12-23 1987-02-24 United Technologies Corporation Air cooler for providing buffer air to a bearing compartment
JP2862536B2 (ja) * 1987-09-25 1999-03-03 株式会社東芝 ガスタービンの翼
JP2818266B2 (ja) * 1990-06-30 1998-10-30 株式会社東芝 ガスタービン冷却翼
US5253976A (en) 1991-11-19 1993-10-19 General Electric Company Integrated steam and air cooling for combined cycle gas turbines
JP3260437B2 (ja) * 1992-09-03 2002-02-25 株式会社日立製作所 ガスタービン及びガスタービンの段落装置
US5634766A (en) 1994-08-23 1997-06-03 General Electric Co. Turbine stator vane segments having combined air and steam cooling circuits
US5593274A (en) 1995-03-31 1997-01-14 General Electric Co. Closed or open circuit cooling of turbine rotor components
US5685693A (en) 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control
US5536143A (en) 1995-03-31 1996-07-16 General Electric Co. Closed circuit steam cooled bucket
US5611662A (en) 1995-08-01 1997-03-18 General Electric Co. Impingement cooling for turbine stator vane trailing edge
US6183192B1 (en) * 1999-03-22 2001-02-06 General Electric Company Durable turbine nozzle

Also Published As

Publication number Publication date
CZ20004335A3 (cs) 2002-01-16
US6468031B1 (en) 2002-10-22
EP1156187A2 (de) 2001-11-21
EP1156187B1 (de) 2006-08-09
EP1156187A3 (de) 2003-07-23
JP4778621B2 (ja) 2011-09-21
DE60122050T2 (de) 2007-03-01
ATE335916T1 (de) 2006-09-15
KR20010105148A (ko) 2001-11-28
JP2001323801A (ja) 2001-11-22

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