DE60037927D1 - Turbinenschaufel mit besonderer Kühlung der Druckseite der Austrittskante - Google Patents

Turbinenschaufel mit besonderer Kühlung der Druckseite der Austrittskante

Info

Publication number
DE60037927D1
DE60037927D1 DE60037927T DE60037927T DE60037927D1 DE 60037927 D1 DE60037927 D1 DE 60037927D1 DE 60037927 T DE60037927 T DE 60037927T DE 60037927 T DE60037927 T DE 60037927T DE 60037927 D1 DE60037927 D1 DE 60037927D1
Authority
DE
Germany
Prior art keywords
trailing edge
pressure side
turbine blade
special cooling
special
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
DE60037927T
Other languages
English (en)
Other versions
DE60037927T2 (de
Inventor
Ching-Pang Lee
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=23495493&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE60037927(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60037927D1 publication Critical patent/DE60037927D1/de
Publication of DE60037927T2 publication Critical patent/DE60037927T2/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
    • 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
    • F01D5/186—Film cooling
    • 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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60037927T 1999-08-23 2000-08-04 Turbinenschaufel mit besonderer Kühlung der Druckseite der Austrittskante Expired - Lifetime DE60037927T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US379022 1989-07-12
US09/379,022 US6273682B1 (en) 1999-08-23 1999-08-23 Turbine blade with preferentially-cooled trailing edge pressure wall

Publications (2)

Publication Number Publication Date
DE60037927D1 true DE60037927D1 (de) 2008-03-20
DE60037927T2 DE60037927T2 (de) 2009-01-22

Family

ID=23495493

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60037927T Expired - Lifetime DE60037927T2 (de) 1999-08-23 2000-08-04 Turbinenschaufel mit besonderer Kühlung der Druckseite der Austrittskante

Country Status (4)

Country Link
US (1) US6273682B1 (de)
EP (1) EP1079071B1 (de)
JP (1) JP4659188B2 (de)
DE (1) DE60037927T2 (de)

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EP1000698B1 (de) * 1998-11-09 2003-05-21 ALSTOM (Switzerland) Ltd Gekühlte Komponenten mit konischen Kühlungskanälen
US6582584B2 (en) 1999-08-16 2003-06-24 General Electric Company Method for enhancing heat transfer inside a turbulated cooling passage
US6481972B2 (en) * 2000-12-22 2002-11-19 General Electric Company Turbine bucket natural frequency tuning rib
US6499949B2 (en) * 2001-03-27 2002-12-31 Robert Edward Schafrik Turbine airfoil trailing edge with micro cooling channels
US7074006B1 (en) 2002-10-08 2006-07-11 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Endwall treatment and method for gas turbine
US7094031B2 (en) * 2004-09-09 2006-08-22 General Electric Company Offset Coriolis turbulator blade
US7156620B2 (en) * 2004-12-21 2007-01-02 Pratt & Whitney Canada Corp. Internally cooled gas turbine airfoil and method
US7156619B2 (en) * 2004-12-21 2007-01-02 Pratt & Whitney Canada Corp. Internally cooled gas turbine airfoil and method
US7360434B1 (en) * 2005-12-31 2008-04-22 Florida Turbine Technologies, Inc. Apparatus and method to measure air pressure within a turbine airfoil
US7780413B2 (en) * 2006-08-01 2010-08-24 Siemens Energy, Inc. Turbine airfoil with near wall inflow chambers
US7481623B1 (en) 2006-08-11 2009-01-27 Florida Turbine Technologies, Inc. Compartment cooled turbine blade
US7540712B1 (en) 2006-09-15 2009-06-02 Florida Turbine Technologies, Inc. Turbine airfoil with showerhead cooling holes
US7597540B1 (en) 2006-10-06 2009-10-06 Florida Turbine Technologies, Inc. Turbine blade with showerhead film cooling holes
US7530789B1 (en) 2006-11-16 2009-05-12 Florida Turbine Technologies, Inc. Turbine blade with a serpentine flow and impingement cooling circuit
US7645122B1 (en) * 2006-12-01 2010-01-12 Florida Turbine Technologies, Inc. Turbine rotor blade with a nested parallel serpentine flow cooling circuit
US7806659B1 (en) 2007-07-10 2010-10-05 Florida Turbine Technologies, Inc. Turbine blade with trailing edge bleed slot arrangement
US8083485B2 (en) * 2007-08-15 2011-12-27 United Technologies Corporation Angled tripped airfoil peanut cavity
US8439628B2 (en) * 2010-01-06 2013-05-14 General Electric Company Heat transfer enhancement in internal cavities of turbine engine airfoils
US8535006B2 (en) 2010-07-14 2013-09-17 Siemens Energy, Inc. Near-wall serpentine cooled turbine airfoil
US8764394B2 (en) 2011-01-06 2014-07-01 Siemens Energy, Inc. Component cooling channel
US9017027B2 (en) 2011-01-06 2015-04-28 Siemens Energy, Inc. Component having cooling channel with hourglass cross section
US9022736B2 (en) 2011-02-15 2015-05-05 Siemens Energy, Inc. Integrated axial and tangential serpentine cooling circuit in a turbine airfoil
US9017025B2 (en) 2011-04-22 2015-04-28 Siemens Energy, Inc. Serpentine cooling circuit with T-shaped partitions in a turbine airfoil
EP2844839A1 (de) * 2012-04-23 2015-03-11 General Electric Company Turbinenschaufel mit lokaler wanddickensteuerung
US9506351B2 (en) 2012-04-27 2016-11-29 General Electric Company Durable turbine vane
EP2725235A1 (de) * 2012-10-24 2014-04-30 Siemens Aktiengesellschaft Unterschiedlich raue Schaufel und zugehörige Herstellungsverfahren
EP2946079B1 (de) * 2013-01-15 2021-05-19 Raytheon Technologies Corporation Bauteil eines gasturbinentriebwerks mit quer abgewinkelten pralllippen
US9458725B2 (en) * 2013-10-04 2016-10-04 General Electric Company Method and system for providing cooling for turbine components
US9039371B2 (en) * 2013-10-31 2015-05-26 Siemens Aktiengesellschaft Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements
US9551229B2 (en) 2013-12-26 2017-01-24 Siemens Aktiengesellschaft Turbine airfoil with an internal cooling system having trip strips with reduced pressure drop
US9970319B2 (en) 2014-05-05 2018-05-15 United Technologies Corporation Reducing variation in cooling hole meter length
US10041356B2 (en) 2014-08-15 2018-08-07 United Technologies Corporation Showerhead hole scheme apparatus and system
CN107429568B (zh) 2015-03-17 2019-11-29 西门子能源有限公司 用于涡轮发动机中的翼型件的在后缘冷却通道中具有收缩扩张出口槽的内部冷却系统
JP6806599B2 (ja) 2017-03-10 2021-01-06 三菱パワー株式会社 タービン翼、タービン及びタービン翼の冷却方法

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US4180373A (en) 1977-12-28 1979-12-25 United Technologies Corporation Turbine blade
US4515526A (en) 1981-12-28 1985-05-07 United Technologies Corporation Coolable airfoil for a rotary machine
US5232343A (en) 1984-05-24 1993-08-03 General Electric Company Turbine blade
GB2228540B (en) * 1988-12-07 1993-03-31 Rolls Royce Plc Cooling of turbine blades
JP3006174B2 (ja) * 1991-07-04 2000-02-07 株式会社日立製作所 内部に冷却通路を有する部材
US5700132A (en) 1991-12-17 1997-12-23 General Electric Company Turbine blade having opposing wall turbulators
US5695320A (en) 1991-12-17 1997-12-09 General Electric Company Turbine blade having auxiliary turbulators
US5695322A (en) 1991-12-17 1997-12-09 General Electric Company Turbine blade having restart turbulators
US5695321A (en) 1991-12-17 1997-12-09 General Electric Company Turbine blade having variable configuration turbulators
US5681144A (en) 1991-12-17 1997-10-28 General Electric Company Turbine blade having offset turbulators
US5306401A (en) 1993-03-15 1994-04-26 Fierkens Richard H J Method for drilling cooling holes in turbine blades
JP3192854B2 (ja) * 1993-12-28 2001-07-30 株式会社東芝 タービン冷却翼
US5472316A (en) * 1994-09-19 1995-12-05 General Electric Company Enhanced cooling apparatus for gas turbine engine airfoils
US5468125A (en) 1994-12-20 1995-11-21 Alliedsignal Inc. Turbine blade with improved heat transfer surface
US5738493A (en) 1997-01-03 1998-04-14 General Electric Company Turbulator configuration for cooling passages of an airfoil in a gas turbine engine
US5797726A (en) 1997-01-03 1998-08-25 General Electric Company Turbulator configuration for cooling passages or rotor blade in a gas turbine engine
JPH10205303A (ja) * 1997-01-21 1998-08-04 Hitachi Ltd タービン翼
US5931638A (en) * 1997-08-07 1999-08-03 United Technologies Corporation Turbomachinery airfoil with optimized heat transfer

Also Published As

Publication number Publication date
JP2001073705A (ja) 2001-03-21
US6273682B1 (en) 2001-08-14
EP1079071B1 (de) 2008-01-30
EP1079071A3 (de) 2003-09-10
EP1079071A2 (de) 2001-02-28
DE60037927T2 (de) 2009-01-22
JP4659188B2 (ja) 2011-03-30

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Legal Events

Date Code Title Description
8363 Opposition against the patent