DE3020580A1 - Verfahren zum herstellen eines turbinenlaeufers - Google Patents

Verfahren zum herstellen eines turbinenlaeufers

Info

Publication number
DE3020580A1
DE3020580A1 DE19803020580 DE3020580A DE3020580A1 DE 3020580 A1 DE3020580 A1 DE 3020580A1 DE 19803020580 DE19803020580 DE 19803020580 DE 3020580 A DE3020580 A DE 3020580A DE 3020580 A1 DE3020580 A1 DE 3020580A1
Authority
DE
Germany
Prior art keywords
blades
retaining ring
hub
hub disk
jacket surface
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.)
Withdrawn
Application number
DE19803020580
Other languages
German (de)
English (en)
Inventor
Bruce Allan Ewing
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.)
Motors Liquidation Co
Original Assignee
General Motors Corp
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 Motors Corp filed Critical General Motors Corp
Publication of DE3020580A1 publication Critical patent/DE3020580A1/de
Withdrawn legal-status Critical Current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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3061—Fixing blades to rotors; Blade roots ; Blade spacers by welding, brazing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/4981—Utilizing transitory attached element or associated separate material
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49863—Assembling or joining with prestressing of part
    • Y10T29/49865—Assembling or joining with prestressing of part by temperature differential [e.g., shrink fit]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Powder Metallurgy (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Articles (AREA)
DE19803020580 1979-06-06 1980-05-29 Verfahren zum herstellen eines turbinenlaeufers Withdrawn DE3020580A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/046,104 US4270256A (en) 1979-06-06 1979-06-06 Manufacture of composite turbine rotors

Publications (1)

Publication Number Publication Date
DE3020580A1 true DE3020580A1 (de) 1980-12-18

Family

ID=21941642

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19803020580 Withdrawn DE3020580A1 (de) 1979-06-06 1980-05-29 Verfahren zum herstellen eines turbinenlaeufers

Country Status (5)

Country Link
US (1) US4270256A (enExample)
JP (1) JPS55164703A (enExample)
CA (1) CA1132339A (enExample)
DE (1) DE3020580A1 (enExample)
GB (1) GB2052645B (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3725132A1 (de) * 1986-08-01 1988-02-11 Rolls Royce Plc Verfahren zur herstellung einer rotorbaugruppe fuer gasturbinentriebwerke
DE102006061448B4 (de) * 2006-12-23 2011-12-08 Mtu Aero Engines Gmbh Verfahren zur Herstellung einer Blisk oder eines Blings einer Gasturbine und danach hergestelltes Bauteil
DE102006016205B4 (de) * 2006-04-06 2015-01-29 MTU Aero Engines AG Verfahren zum Verbinden von metallischen Bauelementen und damit hergestelltes Bauteil

Families Citing this family (63)

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SE446606B (sv) * 1981-08-27 1986-09-29 Stal Laval Turbin Ab Sett att framstella skovelringar och skivor med skovlar for roterande maskiner sasom kompressorer eller turbiner
US4592120A (en) * 1983-02-14 1986-06-03 Williams International Corporation Method for manufacturing a multiple property integral turbine wheel
US4494287A (en) * 1983-02-14 1985-01-22 Williams International Corporation Method of manufacturing a turbine rotor
US4587700A (en) * 1984-06-08 1986-05-13 The Garrett Corporation Method for manufacturing a dual alloy cooled turbine wheel
US4529452A (en) * 1984-07-30 1985-07-16 United Technologies Corporation Process for fabricating multi-alloy components
US4659288A (en) * 1984-12-10 1987-04-21 The Garrett Corporation Dual alloy radial turbine rotor with hub material exposed in saddle regions of blade ring
US4702673A (en) * 1985-10-18 1987-10-27 General Electric Company Method for assembly of tangential entry dovetailed bucket assemblies on a turbomachine bucket wheel
US4692644A (en) * 1985-12-23 1987-09-08 General Electric Company Fluid cooled acyclic generator rotor having a copper conductor diffusion bonded to a magnetic steel core
US4864706A (en) * 1987-08-12 1989-09-12 United Technologies Corporation Fabrication of dual alloy integrally bladed rotors
US4883216A (en) * 1988-03-28 1989-11-28 General Electric Company Method for bonding an article projection
DE3915702A1 (de) * 1989-05-13 1990-11-15 Forschungszentrum Juelich Gmbh Verfahren zum verbinden von werkstuecken mittels grenzflaechendiffusion
US4962586A (en) * 1989-11-29 1990-10-16 Westinghouse Electric Corp. Method of making a high temperature - low temperature rotor for turbines
CA2030427A1 (en) * 1989-12-19 1991-06-20 Jonathan S. Stinson Method of enhancing bond joint structural integrity of spray cast articles
DE9207017U1 (de) * 1992-05-23 1992-09-03 ABB Patent GmbH, 6800 Mannheim Laufrad einer Turbine
US5273708A (en) * 1992-06-23 1993-12-28 Howmet Corporation Method of making a dual alloy article
US5332022A (en) * 1992-09-08 1994-07-26 Howmet Corporation Composite casting method
FR2697284B1 (fr) * 1992-10-27 1995-01-27 Europ Propulsion Procédé de fabrication d'une roue de turbine à aubes insérées et roue obtenue par le procédé.
US6218026B1 (en) 1995-06-07 2001-04-17 Allison Engine Company Lightweight high stiffness member and manufacturing method thereof
US5724643A (en) * 1995-06-07 1998-03-03 Allison Engine Company, Inc. Lightweight high stiffness shaft and manufacturing method thereof
US5609471A (en) * 1995-12-07 1997-03-11 Allison Advanced Development Company, Inc. Multiproperty rotor disk and method of manufacture
US20030032057A1 (en) * 1997-08-26 2003-02-13 Genentech, Inc. Secreted and transmembrane polypeptides and nucleic acids encoding the same
US6003754A (en) * 1997-10-21 1999-12-21 Allison Advanced Development Co. Airfoil for a gas turbine engine and method of manufacture
US6223524B1 (en) 1998-01-23 2001-05-01 Diversitech, Inc. Shrouds for gas turbine engines and methods for making the same
US6224339B1 (en) 1998-07-08 2001-05-01 Allison Advanced Development Company High temperature airfoil
US6232688B1 (en) 1999-04-28 2001-05-15 Allison Advanced Development Company High speed magnetic thrust disk
US6261699B1 (en) 1999-04-28 2001-07-17 Allison Advanced Development Company Fiber reinforced iron-cobalt composite material system
US6247638B1 (en) * 1999-04-28 2001-06-19 Allison Advanced Development Company Selectively reinforced member and method of manufacture
US6499953B1 (en) 2000-09-29 2002-12-31 Pratt & Whitney Canada Corp. Dual flow impeller
RU2196672C1 (ru) * 2001-12-17 2003-01-20 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" Способ изготовления ротора газотурбинного двигателя
US6726086B2 (en) * 2002-01-24 2004-04-27 Siemens Westinghouse Power Corporation Liquid phase diffusion bonding to a superalloy component
US7416108B2 (en) 2002-01-24 2008-08-26 Siemens Power Generation, Inc. High strength diffusion brazing utilizing nano-powders
US6709771B2 (en) 2002-05-24 2004-03-23 Siemens Westinghouse Power Corporation Hybrid single crystal-powder metallurgy turbine component
US8266800B2 (en) 2003-09-10 2012-09-18 Siemens Energy, Inc. Repair of nickel-based alloy turbine disk
US6969238B2 (en) * 2003-10-21 2005-11-29 General Electric Company Tri-property rotor assembly of a turbine engine, and method for its preparation
GB0408497D0 (en) * 2004-04-16 2004-05-19 Rolls Royce Plc Turbine blisk
US7641985B2 (en) * 2004-06-21 2010-01-05 Siemens Energy, Inc. Boron free joint for superalloy component
US7247000B2 (en) * 2004-08-30 2007-07-24 Honeywell International, Inc. Weld shielding device for automated welding of impellers and blisks
US7316057B2 (en) * 2004-10-08 2008-01-08 Siemens Power Generation, Inc. Method of manufacturing a rotating apparatus disk
US7278821B1 (en) * 2004-11-04 2007-10-09 General Electric Company Methods and apparatus for assembling gas turbine engines
FR2903921B1 (fr) * 2006-07-19 2009-06-05 Snecma Sa Procede de fabrication d'un disque aubage monobloc et moule pour la mise en oeuvre du procede
US7832986B2 (en) * 2007-03-07 2010-11-16 Honeywell International Inc. Multi-alloy turbine rotors and methods of manufacturing the rotors
US7950146B2 (en) * 2007-04-10 2011-05-31 Siemens Energy, Inc. Co-forged steel rotor component for steam and gas turbine engines
US7942635B1 (en) * 2007-08-02 2011-05-17 Florida Turbine Technologies, Inc. Twin spool rotor assembly for a small gas turbine engine
US20090304514A1 (en) * 2007-10-09 2009-12-10 Hamilton Sundstrand Corporation Method of manufacturing a turbine rotor
US8356980B2 (en) 2007-10-09 2013-01-22 Hamilton Sundstrand Corporation Method of manufacturing a turbine rotor
DE102007050142A1 (de) * 2007-10-19 2009-04-23 Mtu Aero Engines Gmbh Verfahren zur Herstellung einer Blisk oder eines Blings, damit hergestelltes Bauteil und Turbinenschaufel
US8206117B2 (en) * 2007-12-19 2012-06-26 Honeywell International Inc. Turbine components and methods of manufacturing turbine components
US8187724B2 (en) * 2009-02-24 2012-05-29 Honeywell International Inc. Method of manufacture of a dual alloy impeller
GB201005270D0 (en) * 2010-03-30 2010-05-12 Rolls Royce Plc A method and apparatus for manufacturing a rotor disc
RU2478796C1 (ru) * 2011-08-10 2013-04-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Способ изготовления интегрального блиска с охлаждаемыми рабочими лопатками, интегральный блиск и охлаждаемая лопатка для газотурбинного двигателя
JP2015227627A (ja) * 2014-05-30 2015-12-17 株式会社東芝 回転機械
US10280768B2 (en) 2014-11-12 2019-05-07 Rolls-Royce North American Technologies Inc. Turbine blisk including ceramic matrix composite blades and methods of manufacture
EP3069802B1 (de) * 2015-03-17 2018-11-07 MTU Aero Engines GmbH Verfahren zur herstellung eines bauteils aus einem verbund-werkstoff mit einer metall-matrix und eingelagerten intermetallischen phasen
RU2595331C1 (ru) * 2015-03-19 2016-08-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Способ позиционирования лопаток при изготовлении интегрального моноколеса турбины газотурбинного двигателя
US9938834B2 (en) 2015-04-30 2018-04-10 Honeywell International Inc. Bladed gas turbine engine rotors having deposited transition rings and methods for the manufacture thereof
US10294804B2 (en) * 2015-08-11 2019-05-21 Honeywell International Inc. Dual alloy gas turbine engine rotors and methods for the manufacture thereof
US10036254B2 (en) 2015-11-12 2018-07-31 Honeywell International Inc. Dual alloy bladed rotors suitable for usage in gas turbine engines and methods for the manufacture thereof
US10294954B2 (en) 2016-11-09 2019-05-21 Rolls-Royce North American Technologies Inc. Composite blisk
US10563665B2 (en) 2017-01-30 2020-02-18 Rolls-Royce North American Technologies, Inc. Turbomachine stage and method of making same
US10787917B2 (en) * 2018-05-04 2020-09-29 Rolls-Royce North American Technologies Inc. Multi-piece turbine disk for ceramic matrix composite components
US11549374B2 (en) * 2020-02-18 2023-01-10 Raytheon Technologies Corporation Gas turbine rotor component and method of manufacture
CN115070041B (zh) * 2021-03-10 2024-04-19 中国航发商用航空发动机有限责任公司 一种gh4169和tc17同种、异种材料多级转子组件及其制备方法
US20220388090A1 (en) * 2021-06-04 2022-12-08 The Boeing Company Fabrication of thick stock via diffusion bonding of titanium alloys

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US3000081A (en) * 1957-07-16 1961-09-19 Ford Motor Co Wheel manufacture
US3571906A (en) * 1968-09-26 1971-03-23 Caterpillar Tractor Co Friction bonding of hard-to-grip workpieces
US4096615A (en) * 1977-05-31 1978-06-27 General Motors Corporation Turbine rotor fabrication

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US2475772A (en) * 1943-03-31 1949-07-12 Allis Chalmers Mfg Co Method of blading rotors and other elements
NL64042C (enExample) * 1944-02-25
US3292245A (en) * 1962-02-20 1966-12-20 Demag Ag Process and apparatus for making rotors
US4051585A (en) * 1976-07-26 1977-10-04 United Technologies Corporation Method of forming a turbine rotor
US4186473A (en) * 1978-08-14 1980-02-05 General Motors Corporation Turbine rotor fabrication by thermal methods

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3000081A (en) * 1957-07-16 1961-09-19 Ford Motor Co Wheel manufacture
US3571906A (en) * 1968-09-26 1971-03-23 Caterpillar Tractor Co Friction bonding of hard-to-grip workpieces
US4096615A (en) * 1977-05-31 1978-06-27 General Motors Corporation Turbine rotor fabrication

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3725132A1 (de) * 1986-08-01 1988-02-11 Rolls Royce Plc Verfahren zur herstellung einer rotorbaugruppe fuer gasturbinentriebwerke
DE102006016205B4 (de) * 2006-04-06 2015-01-29 MTU Aero Engines AG Verfahren zum Verbinden von metallischen Bauelementen und damit hergestelltes Bauteil
DE102006061448B4 (de) * 2006-12-23 2011-12-08 Mtu Aero Engines Gmbh Verfahren zur Herstellung einer Blisk oder eines Blings einer Gasturbine und danach hergestelltes Bauteil

Also Published As

Publication number Publication date
JPS6130123B2 (enExample) 1986-07-11
US4270256A (en) 1981-06-02
JPS55164703A (en) 1980-12-22
GB2052645A (en) 1981-01-28
CA1132339A (en) 1982-09-28
GB2052645B (en) 1983-02-09

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Legal Events

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8110 Request for examination paragraph 44
8128 New person/name/address of the agent

Representative=s name: MANITZ, G., DIPL.-PHYS. DR.RER.NAT. FINSTERWALD, M

8139 Disposal/non-payment of the annual fee