JPS5612001A - Method of manufacturing liquiddcooled air wheel for gas turbine - Google Patents

Method of manufacturing liquiddcooled air wheel for gas turbine

Info

Publication number
JPS5612001A
JPS5612001A JP7158580A JP7158580A JPS5612001A JP S5612001 A JPS5612001 A JP S5612001A JP 7158580 A JP7158580 A JP 7158580A JP 7158580 A JP7158580 A JP 7158580A JP S5612001 A JPS5612001 A JP S5612001A
Authority
JP
Japan
Prior art keywords
liquiddcooled
manufacturing
gas turbine
air wheel
wheel
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.)
Pending
Application number
JP7158580A
Other languages
English (en)
Inventor
Meriru Gurandaaru Kureiton
Chiyaaruzu Uirumotsuto Reo
Kuraido Musu Mairon
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
Publication of JPS5612001A publication Critical patent/JPS5612001A/ja
Pending legal-status Critical Current

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
    • F01D5/185Liquid cooling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • 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
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • Y10T29/49339Hollow blade
    • Y10T29/49341Hollow blade with cooling passage
    • Y10T29/49343Passage contains tubular insert
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49995Shaping one-piece blank by removing material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Separation By Low-Temperature Treatments (AREA)
JP7158580A 1979-06-01 1980-05-30 Method of manufacturing liquiddcooled air wheel for gas turbine Pending JPS5612001A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/044,538 US4249291A (en) 1979-06-01 1979-06-01 Method for forming a liquid cooled airfoil for a gas turbine

Publications (1)

Publication Number Publication Date
JPS5612001A true JPS5612001A (en) 1981-02-05

Family

ID=21932942

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7158580A Pending JPS5612001A (en) 1979-06-01 1980-05-30 Method of manufacturing liquiddcooled air wheel for gas turbine

Country Status (9)

Country Link
US (1) US4249291A (ja)
JP (1) JPS5612001A (ja)
CA (1) CA1132456A (ja)
DE (1) DE3020363A1 (ja)
FR (1) FR2464123A1 (ja)
GB (1) GB2051255B (ja)
IT (1) IT1130680B (ja)
NL (1) NL8003183A (ja)
NO (1) NO148512C (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4573872A (en) * 1982-12-27 1986-03-04 Tokyo Shibaura Denki Kabushiki Kaisha High temperature heat resistant structure
JP2015513632A (ja) * 2012-02-17 2015-05-14 アルストム テクノロジー リミテッドALSTOM Technology Ltd 熱によって高い応力を受ける構成部材において表面付近冷却通路を形成する方法およびこのような通路を有する構成部材

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5030060A (en) * 1988-10-20 1991-07-09 The United States Of America As Represented By The Secretary Of The Air Force Method and apparatus for cooling high temperature ceramic turbine blade portions
US5810552A (en) * 1992-02-18 1998-09-22 Allison Engine Company, Inc. Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same
US5601254A (en) * 1994-10-28 1997-02-11 Rosemount Aerospace Inc. Single sided backbone strut for air data sensor
US7410342B2 (en) * 2005-05-05 2008-08-12 Florida Turbine Technologies, Inc. Airfoil support
KR20090004926A (ko) * 2006-03-09 2009-01-12 올테크 어소시에이츠, 인크. 복합 관형 부재, 관형 부재, 드리프트 튜브, 카트리지/임팩터 조립체, 카트리지, 전자 회로, 증기화 광 산란 검출기, 테스트 샘플 분석 방법 및 입력된 전압 신호 처리 방법
EP1923536A1 (en) * 2006-11-17 2008-05-21 Siemens Aktiengesellschaft Liner in a cooling channel of a turbine blade
US20100239409A1 (en) * 2009-03-18 2010-09-23 General Electric Company Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil
FR2961552B1 (fr) * 2010-06-21 2014-01-31 Snecma Aube de turbine a cavite de bord d'attaque refroidie par impact
US9624779B2 (en) * 2013-10-15 2017-04-18 General Electric Company Thermal management article and method of forming the same, and method of thermal management of a substrate
US10907609B2 (en) * 2014-07-15 2021-02-02 Ge Renewable Technologies Apparatus and method for modifying a geometry of a turbine part
CA2857297C (en) * 2014-07-21 2021-08-17 Alstom Renewable Technologies Apparatus and method for modifying a geometry of a turbine part
US20170044903A1 (en) * 2015-08-13 2017-02-16 General Electric Company Rotating component for a turbomachine and method for providing cooling of a rotating component
WO2020046359A1 (en) * 2018-08-31 2020-03-05 Siemens Aktiengesellschaft Radiatively cooled hybrid components
US10724387B2 (en) * 2018-11-08 2020-07-28 Raytheon Technologies Corporation Continuation of a shear tube through a vane platform for structural support
FR3114762B1 (fr) * 2020-10-06 2022-08-19 Safran Aircraft Engines Procédé de fabrication d'une aube de compresseur de turbomachine par compactage
US11859512B2 (en) * 2022-03-31 2024-01-02 General Electric Company Cooling passage exit opening cross-sectional area reduction for turbine system component
US11739646B1 (en) * 2022-03-31 2023-08-29 General Electric Company Pre-sintered preform ball for ball-chute with hollow member therein for internal cooling of turbine component

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1066524B (de) * 1959-10-08 Regensburg Dr.-Ing. Wilhelm Sdimid Gärbottich und Lagertank mit Außenkühlung
DE730114C (de) * 1940-12-14 1943-01-07 Adolf Bangert Apparat zur Durchfuehtung von unter Waermetausch verlaufenden Reaktionen
US2641439A (en) * 1947-10-01 1953-06-09 Chrysler Corp Cooled turbine or compressor blade
DE816686C (de) * 1950-09-09 1951-10-11 Seppelfricke Geb Gmbh Lagerschale fuer Warmwalzwerke
US2983994A (en) * 1955-08-01 1961-05-16 Olin Mathieson Metal articles having hollow sections and method of making same
US3091846A (en) * 1958-03-21 1963-06-04 Smith Corp A O Method of brazing
US3305918A (en) * 1963-03-19 1967-02-28 Universal American Corp Method of producing composite castforged aluminum piston with bonded ferrous ring carrier
US3446481A (en) * 1967-03-24 1969-05-27 Gen Electric Liquid cooled turbine rotor
US3446482A (en) * 1967-03-24 1969-05-27 Gen Electric Liquid cooled turbine rotor
GB1301524A (ja) * 1970-05-22 1972-12-29
SE350918B (ja) * 1971-03-26 1972-11-13 Asea Ab
US4119390A (en) * 1976-11-19 1978-10-10 General Electric Company Liquid-cooled, turbine bucket with enhanced heat transfer performance
US4156582A (en) * 1976-12-13 1979-05-29 General Electric Company Liquid cooled gas turbine buckets
US4137619A (en) * 1977-10-03 1979-02-06 General Electric Company Method of fabricating composite structures for water cooled gas turbine components
US4185369A (en) * 1978-03-22 1980-01-29 General Electric Company Method of manufacture of cooled turbine or compressor buckets

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4573872A (en) * 1982-12-27 1986-03-04 Tokyo Shibaura Denki Kabushiki Kaisha High temperature heat resistant structure
JP2015513632A (ja) * 2012-02-17 2015-05-14 アルストム テクノロジー リミテッドALSTOM Technology Ltd 熱によって高い応力を受ける構成部材において表面付近冷却通路を形成する方法およびこのような通路を有する構成部材
US9869479B2 (en) 2012-02-17 2018-01-16 Ansaldo Energia Ip Uk Limited Method for producing a near-surface cooling passage in a thermally highly stressed component, and component having such a passage

Also Published As

Publication number Publication date
IT1130680B (it) 1986-06-18
NO801619L (no) 1980-12-02
GB2051255A (en) 1981-01-14
FR2464123A1 (fr) 1981-03-06
NO148512C (no) 1983-10-26
DE3020363A1 (de) 1980-12-11
US4249291A (en) 1981-02-10
FR2464123B1 (ja) 1984-04-27
NO148512B (no) 1983-07-18
NL8003183A (nl) 1980-12-03
IT8022390A0 (it) 1980-05-29
GB2051255B (en) 1983-03-16
CA1132456A (en) 1982-09-28

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