FR2652524B1 - Procede de fabrication de disques de turbine constitues de deux alliages, et disques ainsi obtenus. - Google Patents

Procede de fabrication de disques de turbine constitues de deux alliages, et disques ainsi obtenus.

Info

Publication number
FR2652524B1
FR2652524B1 FR9011872A FR9011872A FR2652524B1 FR 2652524 B1 FR2652524 B1 FR 2652524B1 FR 9011872 A FR9011872 A FR 9011872A FR 9011872 A FR9011872 A FR 9011872A FR 2652524 B1 FR2652524 B1 FR 2652524B1
Authority
FR
France
Prior art keywords
discs
alloys
producing turbine
producing
discs made
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 - Fee Related
Application number
FR9011872A
Other languages
English (en)
Other versions
FR2652524A1 (fr
Inventor
Donald Krueger Daniel
Eugene Sauby Michael
Chand Jain Sulekh
Paul Bardes Bruce
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 FR2652524A1 publication Critical patent/FR2652524A1/fr
Application granted granted Critical
Publication of FR2652524B1 publication Critical patent/FR2652524B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/02—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00—Making machine elements
    • B21K1/28—Making machine elements wheels; discs
    • B21K1/32—Making machine elements wheels; discs discs, e.g. disc wheels
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S72/00—Metal deforming
    • Y10S72/70—Deforming specified alloys or uncommon metal or bimetallic work
FR9011872A 1989-10-04 1990-09-26 Procede de fabrication de disques de turbine constitues de deux alliages, et disques ainsi obtenus. Expired - Fee Related FR2652524B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/417,095 US5100050A (en) 1989-10-04 1989-10-04 Method of manufacturing dual alloy turbine disks

Publications (2)

Publication Number Publication Date
FR2652524A1 FR2652524A1 (fr) 1991-04-05
FR2652524B1 true FR2652524B1 (fr) 1995-05-19

Family

ID=23652561

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9011872A Expired - Fee Related FR2652524B1 (fr) 1989-10-04 1990-09-26 Procede de fabrication de disques de turbine constitues de deux alliages, et disques ainsi obtenus.

Country Status (7)

Country Link
US (1) US5100050A (fr)
JP (1) JP2980661B2 (fr)
CA (1) CA2021628C (fr)
DE (1) DE4031173A1 (fr)
FR (1) FR2652524B1 (fr)
GB (1) GB2240063B (fr)
IT (1) IT1243090B (fr)

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US8668790B2 (en) * 2007-01-08 2014-03-11 General Electric Company Heat treatment method and components treated according to the method
EP2217869A4 (fr) * 2007-12-07 2015-06-24 Dresser Rand Co Système et procédé de compression pour un système de liquéfaction de gaz
US7947240B2 (en) 2008-10-08 2011-05-24 Expansion Energy, Llc System and method of carbon capture and sequestration
US8501125B2 (en) * 2008-10-08 2013-08-06 Expansion Energy, Llc System and method of carbon capture and sequestration, environmental remediation, and metals recovery
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DE102009039824B4 (de) * 2009-09-02 2014-10-16 Siemens Aktiengesellschaft Rotorwelle für eine Dampfturbine
GB201005270D0 (en) * 2010-03-30 2010-05-12 Rolls Royce Plc A method and apparatus for manufacturing a rotor disc
US8727203B2 (en) 2010-09-16 2014-05-20 Howmedica Osteonics Corp. Methods for manufacturing porous orthopaedic implants
US8918996B2 (en) 2011-05-04 2014-12-30 General Electric Company Components and processes of producing components with regions having different grain structures
US9156113B2 (en) 2011-06-03 2015-10-13 General Electric Company Components and processes of producing components with regions having different grain structures
CN102303083B (zh) * 2011-06-30 2013-05-29 钢铁研究总院 制备难变形合金饼坯的快速等温锻造方法和装置
US9243514B2 (en) * 2012-11-16 2016-01-26 United Technologies Corporation Hybrid gas turbine bearing support
US9540949B2 (en) 2012-12-13 2017-01-10 Hamilton Sundstrand Corporation Turbine hub retainer
DE102014115370A1 (de) * 2013-10-25 2015-04-30 Richard Bergner Verbindungstechnik Gmbh & Co. Kg Montageeinheit mit einem Montageteil und einem Schweißelement sowie Verfahren zur Herstellung der Montageeinheit
DE102014116988A1 (de) * 2013-11-28 2015-05-28 Richard Bergner Verbindungstechnik Gmbh & Co. Kg Verfahren zur Herstellung einer Montageeinheit
WO2015122882A1 (fr) * 2014-02-12 2015-08-20 Hewlett-Packard Development Company, L.P. Formation d'un boîtier d'un dispositif électronique
EP3061556B1 (fr) 2015-02-26 2018-08-15 Rolls-Royce Corporation Procédé de réparation de composants métalliques à paroi double au moyen d'un matériau de brasage et composant ainsi obtenu
KR200480791Y1 (ko) * 2015-03-05 2016-07-07 권태영 고강도 종이 팔레트
US10328489B1 (en) 2015-12-29 2019-06-25 United Technologies Corporation Dynamic bonding of powder metallurgy materials
US20180104765A1 (en) * 2016-10-13 2018-04-19 United Technologies Corporation Hybrid component and method of making
US10508316B2 (en) 2017-03-31 2019-12-17 General Electric Company Method and fixture for counteracting tensile stress
US11338396B2 (en) * 2018-03-08 2022-05-24 Rolls-Royce Corporation Techniques and assemblies for joining components
US11549374B2 (en) 2020-02-18 2023-01-10 Raytheon Technologies Corporation Gas turbine rotor component and method of manufacture

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Also Published As

Publication number Publication date
CA2021628A1 (fr) 1991-04-05
GB9021420D0 (en) 1990-11-14
GB2240063B (en) 1994-06-15
IT1243090B (it) 1994-05-23
JP2980661B2 (ja) 1999-11-22
IT9021627A0 (it) 1990-10-02
FR2652524A1 (fr) 1991-04-05
DE4031173A1 (de) 1991-04-11
US5100050A (en) 1992-03-31
JPH03174986A (ja) 1991-07-30
CA2021628C (fr) 2000-07-04
IT9021627A1 (it) 1992-04-02
GB2240063A (en) 1991-07-24

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Legal Events

Date Code Title Description
ST Notification of lapse