DE59308916D1 - Verfahren zur Herstellung eines hochtemperatur-festen Bauteils aus zwei unterschiedlichen Werkstoffen - Google Patents

Verfahren zur Herstellung eines hochtemperatur-festen Bauteils aus zwei unterschiedlichen Werkstoffen

Info

Publication number
DE59308916D1
DE59308916D1 DE59308916T DE59308916T DE59308916D1 DE 59308916 D1 DE59308916 D1 DE 59308916D1 DE 59308916 T DE59308916 T DE 59308916T DE 59308916 T DE59308916 T DE 59308916T DE 59308916 D1 DE59308916 D1 DE 59308916D1
Authority
DE
Germany
Prior art keywords
producing
temperature
different materials
resistant component
resistant
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
DE59308916T
Other languages
English (en)
Inventor
Peter Dr Ernst
Manfred Dr Thumann
Christoph Toennes
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.)
Alstom SA
Original Assignee
Asea Brown Boveri AG Switzerland
Asea Brown Boveri AB
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 Asea Brown Boveri AG Switzerland, Asea Brown Boveri AB filed Critical Asea Brown Boveri AG Switzerland
Application granted granted Critical
Publication of DE59308916D1 publication Critical patent/DE59308916D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12014—All metal or with adjacent metals having metal particles
    • Y10T428/12021—All metal or with adjacent metals having metal particles having composition or density gradient or differential porosity
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12014—All metal or with adjacent metals having metal particles
    • Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12014—All metal or with adjacent metals having metal particles
    • Y10T428/1216—Continuous interengaged phases of plural metals, or oriented fiber containing
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12014—All metal or with adjacent metals having metal particles
    • Y10T428/1216—Continuous interengaged phases of plural metals, or oriented fiber containing
    • Y10T428/12174—Mo or W containing

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Powder Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE59308916T 1992-06-13 1993-05-21 Verfahren zur Herstellung eines hochtemperatur-festen Bauteils aus zwei unterschiedlichen Werkstoffen Expired - Fee Related DE59308916D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4219469A DE4219469A1 (de) 1992-06-13 1992-06-13 Hohen Temperaturen aussetzbares Bauteil, insbesondere Turbinenschaufel, und Verfahren zur Herstellung dieses Bauteils

Publications (1)

Publication Number Publication Date
DE59308916D1 true DE59308916D1 (de) 1998-10-01

Family

ID=6461000

Family Applications (2)

Application Number Title Priority Date Filing Date
DE4219469A Withdrawn DE4219469A1 (de) 1992-06-13 1992-06-13 Hohen Temperaturen aussetzbares Bauteil, insbesondere Turbinenschaufel, und Verfahren zur Herstellung dieses Bauteils
DE59308916T Expired - Fee Related DE59308916D1 (de) 1992-06-13 1993-05-21 Verfahren zur Herstellung eines hochtemperatur-festen Bauteils aus zwei unterschiedlichen Werkstoffen

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE4219469A Withdrawn DE4219469A1 (de) 1992-06-13 1992-06-13 Hohen Temperaturen aussetzbares Bauteil, insbesondere Turbinenschaufel, und Verfahren zur Herstellung dieses Bauteils

Country Status (4)

Country Link
US (1) US5395699A (de)
EP (1) EP0574727B1 (de)
JP (1) JPH06172816A (de)
DE (2) DE4219469A1 (de)

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US6551064B1 (en) 1996-07-24 2003-04-22 General Electric Company Laser shock peened gas turbine engine intermetallic parts
DE19710592A1 (de) * 1997-03-14 1998-09-17 Forschungszentrum Juelich Gmbh Oxidationsbeständige, TiAl-haltige Legierungen
DE19756354B4 (de) 1997-12-18 2007-03-01 Alstom Schaufel und Verfahren zur Herstellung der Schaufel
DE19933633A1 (de) * 1999-07-17 2001-01-18 Abb Alstom Power Ch Ag Hochtemperaturlegierung
DE10054229B4 (de) * 2000-11-02 2018-06-28 Ansaldo Energia Ip Uk Limited Hochtemperaturlegierung
US7566415B2 (en) * 2002-11-18 2009-07-28 Adma Products, Inc. Method for manufacturing fully dense metal sheets and layered composites from reactive alloy powders
US6852273B2 (en) * 2003-01-29 2005-02-08 Adma Products, Inc. High-strength metal aluminide-containing matrix composites and methods of manufacture the same
US7241416B2 (en) * 2003-08-12 2007-07-10 Borg Warner Inc. Metal injection molded turbine rotor and metal injection molded shaft connection attachment thereto
US20060083653A1 (en) * 2004-10-20 2006-04-20 Gopal Das Low porosity powder metallurgy produced components
US20070003416A1 (en) * 2005-06-30 2007-01-04 General Electric Company Niobium silicide-based turbine components, and related methods for laser deposition
JP2008202544A (ja) * 2007-02-21 2008-09-04 Mitsubishi Heavy Ind Ltd ロータの製造方法及びこのロータをそなえた排気ターボ過給機
EE05653B1 (et) 2010-04-29 2013-04-15 O� Skeleton Technologies Ssinikkomposiitelektrood elektrilise kaksikkihi kondensaatorile
DE102010042889A1 (de) * 2010-10-25 2012-04-26 Manfred Renkel Turboladerbauteil
US8944762B2 (en) 2011-10-28 2015-02-03 United Technologies Corporation Spoked spacer for a gas turbine engine
US9938831B2 (en) 2011-10-28 2018-04-10 United Technologies Corporation Spoked rotor for a gas turbine engine
US10315279B2 (en) 2014-08-08 2019-06-11 Siemens Aktiengesellschaft Hot isostatic pressing system for the assembly of modular components usable in a turbine engine
CN105014068A (zh) * 2015-08-06 2015-11-04 潘桂枝 一种双金属复合材料的制备方法
US10422228B2 (en) 2016-04-12 2019-09-24 United Technologies Corporation Manufacturing a monolithic component with discrete portions formed of different metals
US20190040749A1 (en) * 2017-08-01 2019-02-07 United Technologies Corporation Method of fabricating a turbine blade
RU178967U1 (ru) * 2017-10-31 2018-04-24 федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский государственный авиационный технический университет" Лопатка турбомашины из алюминиевого сплава с упрочняющим слоем, содержащим углерод

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GB608766A (en) * 1944-12-01 1948-09-21 Bbc Brown Boveri & Cie Improvements in turbine blades
FR1052893A (fr) * 1951-02-07 1954-01-28 Plansee Metallwerk Aube de turbine à grande résistance à la chaleur et à l'inflammation utilisable en particulier dans les turbines à gaz, et son procédé de fabrication
US2946680A (en) * 1955-08-10 1960-07-26 Thompson Ramo Wooldridge Inc Powder metallurgy
AT309154B (de) * 1970-11-24 1973-08-10 Plansee Metallwerk Werkstoff für Turbinenschaufeln
CH544217A (de) * 1971-04-08 1973-11-15 Bbc Sulzer Turbomaschinen Gasturbinenschaufel
FR2149990A5 (en) * 1971-08-09 1973-03-30 Imp Metal Ind Kynoch Ltd Metal parts prodn from several elements - eg for aircraft using process which reduces fatigue
US3940268A (en) * 1973-04-12 1976-02-24 Crucible Inc. Method for producing rotor discs
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US4063939A (en) * 1975-06-27 1977-12-20 Special Metals Corporation Composite turbine wheel and process for making same
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US4529452A (en) * 1984-07-30 1985-07-16 United Technologies Corporation Process for fabricating multi-alloy components
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US4680160A (en) * 1985-12-11 1987-07-14 Trw Inc. Method of forming a rotor
DE3543831A1 (de) * 1985-12-12 1987-07-02 Aluminium Walzwerke Singen Verbundprofil, insbesondere verbundstromschiene
US4787821A (en) * 1987-04-10 1988-11-29 Allied Signal Inc. Dual alloy rotor
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US4828793A (en) * 1988-05-06 1989-05-09 United States Of America As Represented By The Secretary Of The Air Force Method to produce titanium alloy articles with high fatigue and fracture resistance
US4851053A (en) * 1988-05-06 1989-07-25 The United States Of America As Represented By The Secretary Of The Air Force Method to produce dispersion strengthened titanium alloy articles with high creep resistance
US4897127A (en) * 1988-10-03 1990-01-30 General Electric Company Rapidly solidified and heat-treated manganese and niobium-modified titanium aluminum alloys
US4904546A (en) * 1989-04-03 1990-02-27 General Electric Company Material system for high temperature jet engine operation
US4916028A (en) * 1989-07-28 1990-04-10 General Electric Company Gamma titanium aluminum alloys modified by carbon, chromium and niobium
CA2025272A1 (en) * 1989-12-04 1991-06-05 Shyh-Chin Huang High-niobium titanium aluminide alloys
US5098653A (en) * 1990-07-02 1992-03-24 General Electric Company Tantalum and chromium containing titanium aluminide rendered castable by boron inoculation
US5080860A (en) * 1990-07-02 1992-01-14 General Electric Company Niobium and chromium containing titanium aluminide rendered castable by boron inoculations
DE59103639D1 (de) * 1990-07-04 1995-01-12 Asea Brown Boveri Verfahren zur Herstellung eines Werkstücks aus einer dotierstoffhaltigen Legierung auf der Basis Titanaluminid.
US5113583A (en) * 1990-09-14 1992-05-19 United Technologies Corporation Integrally bladed rotor fabrication
US5098484A (en) * 1991-01-30 1992-03-24 The United States Of America As Represented By The Secretary Of The Air Force Method for producing very fine microstructures in titanium aluminide alloy powder compacts
DE59106047D1 (de) * 1991-05-13 1995-08-24 Asea Brown Boveri Verfahren zur Herstellung einer Turbinenschaufel.
US5226985A (en) * 1992-01-22 1993-07-13 The United States Of America As Represented By The Secretary Of The Air Force Method to produce gamma titanium aluminide articles having improved properties

Also Published As

Publication number Publication date
EP0574727A1 (de) 1993-12-22
EP0574727B1 (de) 1998-08-26
JPH06172816A (ja) 1994-06-21
US5395699A (en) 1995-03-07
DE4219469A1 (de) 1993-12-16

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: ALSTOM, PARIS, FR

8328 Change in the person/name/address of the agent

Free format text: ROESLER, U., DIPL.-PHYS.UNIV., PAT.-ANW., 81241 MUENCHEN

8339 Ceased/non-payment of the annual fee