JPS5612002A - Turbine blade - Google Patents

Turbine blade

Info

Publication number
JPS5612002A
JPS5612002A JP8800080A JP8800080A JPS5612002A JP S5612002 A JPS5612002 A JP S5612002A JP 8800080 A JP8800080 A JP 8800080A JP 8800080 A JP8800080 A JP 8800080A JP S5612002 A JPS5612002 A JP S5612002A
Authority
JP
Japan
Prior art keywords
turbine blade
turbine
blade
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.)
Granted
Application number
JP8800080A
Other languages
English (en)
Other versions
JPS6123362B2 (ja
Inventor
Jiyon Horando Matsukusuueru
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of JPS5612002A publication Critical patent/JPS5612002A/ja
Publication of JPS6123362B2 publication Critical patent/JPS6123362B2/ja
Granted 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
    • F01D5/181—Blades having a closed internal cavity containing a cooling medium, e.g. sodium
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP8800080A 1979-06-30 1980-06-30 Turbine blade Granted JPS5612002A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7922806A GB2051964B (en) 1979-06-30 1979-06-30 Turbine blade

Publications (2)

Publication Number Publication Date
JPS5612002A true JPS5612002A (en) 1981-02-05
JPS6123362B2 JPS6123362B2 (ja) 1986-06-05

Family

ID=10506211

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8800080A Granted JPS5612002A (en) 1979-06-30 1980-06-30 Turbine blade

Country Status (5)

Country Link
US (1) US4529357A (ja)
JP (1) JPS5612002A (ja)
DE (1) DE3023022C2 (ja)
FR (1) FR2460387A1 (ja)
GB (1) GB2051964B (ja)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4418455A (en) * 1981-05-04 1983-12-06 Electric Power Research Institute, Inc. Method of manufacturing a fluid cooled blade or vane
DE3211139C1 (de) * 1982-03-26 1983-08-11 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Axialturbinenschaufel,insbesondere Axialturbinenlaufschaufel fuer Gasturbinentriebwerke
GB2283538B (en) * 1984-12-01 1995-09-13 Rolls Royce Air cooled gas turbine aerofoil
US4820123A (en) * 1988-04-25 1989-04-11 United Technologies Corporation Dirt removal means for air cooled blades
US4820122A (en) * 1988-04-25 1989-04-11 United Technologies Corporation Dirt removal means for air cooled blades
FR2678318B1 (fr) * 1991-06-25 1993-09-10 Snecma Aube refroidie de distributeur de turbine.
US5484258A (en) * 1994-03-01 1996-01-16 General Electric Company Turbine airfoil with convectively cooled double shell outer wall
US5702232A (en) * 1994-12-13 1997-12-30 United Technologies Corporation Cooled airfoils for a gas turbine engine
US6261054B1 (en) * 1999-01-25 2001-07-17 General Electric Company Coolable airfoil assembly
US6186741B1 (en) * 1999-07-22 2001-02-13 General Electric Company Airfoil component having internal cooling and method of cooling
EP1101900A1 (de) * 1999-11-16 2001-05-23 Siemens Aktiengesellschaft Turbinenschaufel und Verfahren zur Herstellung einer Turbinenschaufel
DE10064269A1 (de) * 2000-12-22 2002-07-04 Alstom Switzerland Ltd Komponente einer Strömungsmaschine mit Inspektionsöffnung
EP1247939A1 (de) * 2001-04-06 2002-10-09 Siemens Aktiengesellschaft Verfahren zur Herstellung einer Turbinenschaufel sowie Turbinenschaufel
ITTO20020699A1 (it) * 2002-08-06 2004-02-07 Fiatavio Spa Paletta per lo statore di una turbina a geometria variabile,
GB2443116B (en) * 2004-03-25 2008-08-13 Rolls Royce Plc A gas turbine engine component cooling arrangement
GB2412411A (en) * 2004-03-25 2005-09-28 Rolls Royce Plc A cooling arrangement
US7198458B2 (en) * 2004-12-02 2007-04-03 Siemens Power Generation, Inc. Fail safe cooling system for turbine vanes
RU2425982C2 (ru) * 2005-04-14 2011-08-10 Альстом Текнолоджи Лтд Лопатка газовой турбины
US7527475B1 (en) 2006-08-11 2009-05-05 Florida Turbine Technologies, Inc. Turbine blade with a near-wall cooling circuit
US7563072B1 (en) 2006-09-25 2009-07-21 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall spiral flow cooling circuit
US8206108B2 (en) * 2007-12-10 2012-06-26 Honeywell International Inc. Turbine blades and methods of manufacturing
US8727724B2 (en) * 2010-04-12 2014-05-20 General Electric Company Turbine bucket having a radial cooling hole
US8777567B2 (en) 2010-09-22 2014-07-15 Honeywell International Inc. Turbine blades, turbine assemblies, and methods of manufacturing turbine blades
US20120156054A1 (en) * 2010-12-15 2012-06-21 General Electric Company Turbine component with near-surface cooling passage and process therefor
EP2540970A1 (en) * 2011-07-01 2013-01-02 Siemens Aktiengesellschaft Liquid metal cooled blade
US10226735B2 (en) * 2011-07-14 2019-03-12 Xiaohua Wang Integrated enhanced heat exchange method by combining boundary layer control with mainstream disturbance
US9856739B2 (en) 2013-09-18 2018-01-02 Honeywell International Inc. Turbine blades with tip portions having converging cooling holes
US9879544B2 (en) 2013-10-16 2018-01-30 Honeywell International Inc. Turbine rotor blades with improved tip portion cooling holes
US9816389B2 (en) 2013-10-16 2017-11-14 Honeywell International Inc. Turbine rotor blades with tip portion parapet wall cavities
US10138735B2 (en) 2015-11-04 2018-11-27 General Electric Company Turbine airfoil internal core profile
US10472972B2 (en) 2015-12-01 2019-11-12 General Electric Company Thermal management of CMC articles having film holes
US10787932B2 (en) 2018-07-13 2020-09-29 Honeywell International Inc. Turbine blade with dust tolerant cooling system
US11162432B2 (en) 2019-09-19 2021-11-02 General Electric Company Integrated nozzle and diaphragm with optimized internal vane thickness
US11085374B2 (en) 2019-12-03 2021-08-10 General Electric Company Impingement insert with spring element for hot gas path component

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE715421C (de) * 1940-08-21 1941-12-20 Turbinenfabrik Brueckner Kanis Hohlschaufel fuer Kreiselmaschinen, insbesondere Brennkraftturbinen, und Verfahren zu ihrer Herstellung
US2696364A (en) * 1948-07-08 1954-12-07 Thompson Prod Inc Turbine bucket
GB754217A (en) * 1953-01-30 1956-08-08 Gen Motors Corp Improvements relating to turbine blades
US2991973A (en) * 1954-10-18 1961-07-11 Parsons & Marine Eng Turbine Cooling of bodies subject to a hot gas stream
FR1165132A (fr) * 1955-11-28 1958-10-20 Rolls Royce Perfectionnements aux turbines à gaz
US2894719A (en) * 1956-02-21 1959-07-14 Douglas V Foster Improved strut supported turbine blade
GB846277A (en) * 1956-11-20 1960-08-31 Rolls Royce Turbine and compressor blades
US2966331A (en) * 1958-03-11 1960-12-27 Orenda Engines Ltd Hollow, air cooled turbine blades
US3066910A (en) * 1958-07-09 1962-12-04 Thompson Ramo Wooldridge Inc Cooled turbine blade
DE1174329B (de) * 1959-08-24 1964-07-23 Zakl Mech Im Gen K S Leitradzwischenboden fuer Dampf- oder Gasturbinen
GB893706A (en) * 1960-01-05 1962-04-11 Rolls Royce Blades for fluid flow machines
US3420502A (en) * 1962-09-04 1969-01-07 Gen Electric Fluid-cooled airfoil
US3314650A (en) * 1965-07-20 1967-04-18 Gen Motors Corp Cooled blade
FR90542E (fr) * 1965-08-02 1967-12-29 Snecma Perfectionnement aux moyens de refroidissement d'aubes de turbine ou autres pièces
GB1257041A (ja) * 1968-03-27 1971-12-15
US3515499A (en) * 1968-04-22 1970-06-02 Aerojet General Co Blades and blade assemblies for turbine engines,compressors and the like
US3848307A (en) * 1972-04-03 1974-11-19 Gen Electric Manufacture of fluid-cooled gas turbine airfoils
JPS4992416A (ja) * 1972-09-06 1974-09-03
US4156582A (en) * 1976-12-13 1979-05-29 General Electric Company Liquid cooled gas turbine buckets
US4142831A (en) * 1977-06-15 1979-03-06 General Electric Company Liquid-cooled turbine bucket with enhanced heat transfer performance

Also Published As

Publication number Publication date
FR2460387A1 (fr) 1981-01-23
US4529357A (en) 1985-07-16
FR2460387B1 (ja) 1984-10-19
GB2051964B (en) 1983-01-12
JPS6123362B2 (ja) 1986-06-05
DE3023022C2 (de) 1982-06-16
DE3023022A1 (de) 1981-01-08
GB2051964A (en) 1981-01-21

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