DE602006009210D1 - Maschinenbauteile und Herstellungs- und Reparaturverfahren - Google Patents

Maschinenbauteile und Herstellungs- und Reparaturverfahren

Info

Publication number
DE602006009210D1
DE602006009210D1 DE602006009210T DE602006009210T DE602006009210D1 DE 602006009210 D1 DE602006009210 D1 DE 602006009210D1 DE 602006009210 T DE602006009210 T DE 602006009210T DE 602006009210 T DE602006009210 T DE 602006009210T DE 602006009210 D1 DE602006009210 D1 DE 602006009210D1
Authority
DE
Germany
Prior art keywords
sintered preform
machine component
manufacturing
preform
machine components
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.)
Active
Application number
DE602006009210T
Other languages
English (en)
Inventor
Sujith Sathian
Anjiliveltl K Kuruvilla
Daniel Nowak
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=37852721&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE602006009210(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by General Electric Co filed Critical General Electric Co
Publication of DE602006009210D1 publication Critical patent/DE602006009210D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B23K1/00—Soldering, e.g. brazing, or unsoldering
    • 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
    • B23K1/00—Soldering, e.g. brazing, or unsoldering
    • B23K1/0008—Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
    • B23K1/0018—Brazing of turbine parts
    • 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
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/02—Compacting only
    • 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
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
    • 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
    • F01D5/005—Repairing methods or devices
    • 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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—Turbines
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/22—Manufacture essentially without removing material by sintering
    • 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
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Chemical & Material Sciences (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Manufacturing Of Magnetic Record Carriers (AREA)
  • Manufacturing Of Printed Circuit Boards (AREA)
  • Manufacturing Of Printed Wiring (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602006009210T 2006-01-03 2006-12-19 Maschinenbauteile und Herstellungs- und Reparaturverfahren Active DE602006009210D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/324,445 US8703044B2 (en) 2006-01-03 2006-01-03 Machine components and methods of fabricating and repairing

Publications (1)

Publication Number Publication Date
DE602006009210D1 true DE602006009210D1 (de) 2009-10-29

Family

ID=37852721

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006009210T Active DE602006009210D1 (de) 2006-01-03 2006-12-19 Maschinenbauteile und Herstellungs- und Reparaturverfahren

Country Status (8)

Country Link
US (1) US8703044B2 (de)
EP (1) EP1803521B2 (de)
JP (1) JP5698889B2 (de)
KR (1) KR101440152B1 (de)
CN (1) CN1994646A (de)
AT (1) ATE442932T1 (de)
DE (1) DE602006009210D1 (de)
PL (1) PL1803521T5 (de)

Families Citing this family (64)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090041611A1 (en) * 2007-08-07 2009-02-12 General Electric Company Braze alloy composition with enhanced oxidation resistance and methods of using the same
US8182228B2 (en) * 2007-08-16 2012-05-22 General Electric Company Turbine blade having midspan shroud with recessed wear pad and methods for manufacture
JP5078537B2 (ja) 2007-10-15 2012-11-21 三菱重工業株式会社 補修方法
US8500594B2 (en) * 2007-10-17 2013-08-06 Metaldyne Company Llc Differential assembly and method for manufacturing same
US8087565B2 (en) * 2008-09-08 2012-01-03 General Electric Company Process of filling openings in a component
US7789288B1 (en) 2009-07-31 2010-09-07 General Electric Company Brazing process and material for repairing a component
FR2948888B1 (fr) * 2009-08-07 2011-08-26 Snecma Procede optimise de fabrication d'un disque aubage monobloc par jet d'eau abrasif
FR2948889B1 (fr) * 2009-08-07 2011-08-26 Snecma Procede optimise de fabrication d'un disque aubage monobloc par jet d'eau abrasif
US8573949B2 (en) * 2009-09-30 2013-11-05 General Electric Company Method and system for focused energy brazing
EP2353763A1 (de) * 2010-02-10 2011-08-10 Siemens Aktiengesellschaft Verfahren zur Herstellung einer Heißgaskomponente mit einem Kühlkanal beim Löten eines sinteren Teils an einen Träger ; entsprechender Heißgaskomponent
US8641381B2 (en) * 2010-04-14 2014-02-04 General Electric Company System and method for reducing grain boundaries in shrouded airfoils
IT1399883B1 (it) * 2010-05-18 2013-05-09 Nuova Pignone S R L Girante incamiciata con materiale funzionale graduato e metodo
US9976664B2 (en) 2010-11-05 2018-05-22 Hamilton Sundtrand Corporation Furnace braze deposition of hardface coating on wear surface
US20120231295A1 (en) * 2011-03-08 2012-09-13 General Electric Company Method of fabricating a component and a component
DE102011087158A1 (de) * 2011-11-25 2013-05-29 Mtu Aero Engines Gmbh Verfahren zur Panzerung der Z-Notch von TiAl-Schaufeln
US20130156555A1 (en) * 2011-12-15 2013-06-20 General Electric Company Braze materials, brazing processes, and components with wear-resistant coatings formed thereby
FR2985759B1 (fr) * 2012-01-17 2014-03-07 Snecma Aube mobile de turbomachine
US10105795B2 (en) 2012-05-25 2018-10-23 General Electric Company Braze compositions, and related devices
US9700941B2 (en) * 2012-10-03 2017-07-11 Siemens Energy, Inc. Method for repairing a component for use in a turbine engine
US20140140807A1 (en) * 2012-11-19 2014-05-22 General Electric Company Turbine shroud arrangement for a turbine system and method of controlling a turbine shroud arrangement
US9863249B2 (en) * 2012-12-04 2018-01-09 Siemens Energy, Inc. Pre-sintered preform repair of turbine blades
US20140212681A1 (en) * 2013-01-29 2014-07-31 General Electric Company Joining process and joined article
US10315264B2 (en) 2013-01-29 2019-06-11 General Electric Company Joining process and joined article
US9862029B2 (en) 2013-03-15 2018-01-09 Kennametal Inc Methods of making metal matrix composite and alloy articles
US9346101B2 (en) 2013-03-15 2016-05-24 Kennametal Inc. Cladded articles and methods of making the same
CN105102181A (zh) * 2013-03-15 2015-11-25 西门子能源公司 用于修复超合金部件的预烧结的预成形坯
US9458725B2 (en) * 2013-10-04 2016-10-04 General Electric Company Method and system for providing cooling for turbine components
US9664049B2 (en) 2013-11-04 2017-05-30 Siemens Energy, Inc. Braze alloy compositions and brazing methods for superalloys
US9610643B2 (en) * 2014-06-02 2017-04-04 Solar Turbines Incorporated Combustor assembly for a gas turbine engine having a braze layer having a centerline eutectic free region
US20150354374A1 (en) * 2014-06-09 2015-12-10 General Electric Company Turbine blisk and method of manufacturing thereof
US9434017B2 (en) * 2014-06-30 2016-09-06 General Electric Company Braze methods and components with heat resistant materials
US10786875B2 (en) * 2014-07-02 2020-09-29 Raytheon Technologies Corporation Abrasive preforms and manufacture and use methods
CN104117783B (zh) * 2014-07-23 2017-01-18 深圳市威勒科技股份有限公司 一种焊接材料及其制备方法
MX2017006493A (es) * 2014-11-21 2017-09-12 Metaldyne Llc Soldadura fuerte presinterizada.
US20160175991A1 (en) * 2014-12-19 2016-06-23 General Electric Company Weld filler for superalloys
US20160237822A1 (en) * 2015-02-16 2016-08-18 United Technologies Corporation Blade restoration using shroud plating
US10766105B2 (en) 2015-02-26 2020-09-08 Rolls-Royce Corporation Repair of dual walled metallic components using braze material
EP3061557B1 (de) 2015-02-26 2018-04-18 Rolls-Royce Corporation Reparatur von zwei dünnwandigen metallischen bauteilen mit gerichteter energieablagerungs-materialzugabe
EP3095550A1 (de) * 2015-05-20 2016-11-23 Rolls-Royce Corporation Vorgesintertes vorformhartlot zum verbinden von legierungsgussstücken
JP2017020421A (ja) * 2015-07-10 2017-01-26 株式会社東芝 タービン部品の補修方法およびタービン部品
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
US10610982B2 (en) 2015-11-12 2020-04-07 General Electric Company Weld filler metal for superalloys and methods of making
EP3216554B1 (de) * 2016-03-09 2020-05-06 MTU Aero Engines GmbH Bauteil mit verschleissgeschützten öffnungen und vertiefungen sowie verfahren zur herstellung derselben
US10544683B2 (en) 2016-08-30 2020-01-28 Rolls-Royce Corporation Air-film cooled component for a gas turbine engine
US20180073390A1 (en) 2016-09-13 2018-03-15 Rolls-Royce Corporation Additively deposited gas turbine engine cooling component
US10689984B2 (en) 2016-09-13 2020-06-23 Rolls-Royce Corporation Cast gas turbine engine cooling components
CN106583964B (zh) * 2016-10-27 2019-07-23 中国人民解放军第五七一九工厂 一种发动机热端部件三维尺寸钎焊修复材料及制备方法
US11039507B2 (en) 2017-02-23 2021-06-15 General Electric Company Method of brazing a treatment area of a load-bearing component
US11117208B2 (en) 2017-03-21 2021-09-14 Kennametal Inc. Imparting wear resistance to superalloy articles
US20180345396A1 (en) * 2017-06-02 2018-12-06 General Electric Company Machine components and methods of fabricating and repairing
US11224915B2 (en) * 2017-06-05 2022-01-18 General Electric Company Method of repairing a component using an additive manufacture replacement coupon, and alloy for additive manufacturing
US10603734B2 (en) * 2017-07-18 2020-03-31 General Electric Company Method for hardfacing a metal article
US10294801B2 (en) * 2017-07-25 2019-05-21 United Technologies Corporation Rotor blade having anti-wear surface
DE102017116973A1 (de) * 2017-07-27 2019-01-31 Strama-Mps Maschinenbau Gmbh & Co. Kg Verfahren und Vorrichtung zum Bearbeiten von Leitersegmenten eines Wicklungsträgers einer elektrischen Maschine
US11338396B2 (en) 2018-03-08 2022-05-24 Rolls-Royce Corporation Techniques and assemblies for joining components
US20190337102A1 (en) * 2018-05-07 2019-11-07 General Electric Company Interlocking Stage of Airfoils
CN108620702A (zh) * 2018-05-09 2018-10-09 苏州铭觉贸易有限公司 一种表面贴装焊接方法及设备
US11090771B2 (en) 2018-11-05 2021-08-17 Rolls-Royce Corporation Dual-walled components for a gas turbine engine
US11305363B2 (en) 2019-02-11 2022-04-19 Rolls-Royce Corporation Repair of through-hole damage using braze sintered preform
US11999000B2 (en) * 2020-01-03 2024-06-04 Rolls-Royce Corporation Pre-sintered preform braze reinforcement of pressure vessels
CN111321402A (zh) * 2020-04-30 2020-06-23 株洲辉锐增材制造技术有限公司 一种利用激光熔覆技术修复52米数控铣主轴锥孔磨损的工艺方法
JP7434199B2 (ja) * 2021-03-08 2024-02-20 株式会社東芝 タービン動翼
US11692446B2 (en) 2021-09-23 2023-07-04 Rolls-Royce North American Technologies, Inc. Airfoil with sintered powder components
US11524350B1 (en) 2021-10-04 2022-12-13 General Electric Company Backwall strike braze repair

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4005988A (en) * 1975-12-19 1977-02-01 United Technologies Corporation Interlayer for transient liquid phase diffusion bonding
US4155152A (en) * 1977-12-12 1979-05-22 Matthew Bernardo Method of restoring the shrouds of turbine blades
US4291448A (en) * 1977-12-12 1981-09-29 Turbine Components Corporation Method of restoring the shrouds of turbine blades
FR2511908A1 (fr) * 1981-08-26 1983-03-04 Snecma Procede de brasage-diffusion destine aux pieces en superalliages
AT377938B (de) † 1983-06-24 1985-05-28 Philips Nv Schleifapparat
US4822248A (en) * 1987-04-15 1989-04-18 Metallurgical Industries, Inc. Rebuilt shrouded turbine blade and method of rebuilding the same
US5812926A (en) † 1991-09-03 1998-09-22 General Electric Company Process for hard facing a substrate
FR2691658B1 (fr) * 1992-05-27 1994-07-22 Snecma Piece en superalliage comportant un apport et procede de realisation de l'apport.
JPH06228609A (ja) * 1993-01-29 1994-08-16 Mitsubishi Materials Corp スローアウェイチップ
US5561827A (en) † 1994-12-28 1996-10-01 General Electric Company Coated nickel-base superalloy article and powder and method useful in its preparation
US6164916A (en) † 1998-11-02 2000-12-26 General Electric Company Method of applying wear-resistant materials to turbine blades, and turbine blades having wear-resistant materials
FR2785559B1 (fr) † 1998-11-10 2001-03-02 Metals Process Systems Procede de fabrication par metallurgie des poudres de pieces de forme autobrasantes
US6233822B1 (en) * 1998-12-22 2001-05-22 General Electric Company Repair of high pressure turbine shrouds
JP4231582B2 (ja) 1999-03-18 2009-03-04 金属技研株式会社 耐蝕耐摩耗性摺動部材およびその製造方法
US6451454B1 (en) * 1999-06-29 2002-09-17 General Electric Company Turbine engine component having wear coating and method for coating a turbine engine component
US20040124231A1 (en) † 1999-06-29 2004-07-01 Hasz Wayne Charles Method for coating a substrate
JP2001081502A (ja) 1999-09-14 2001-03-27 Kyushu Fukugo Zairyo Kenkyusho:Kk 抵抗加熱法を用いた耐摩耗材の製造方法
US6726086B2 (en) * 2002-01-24 2004-04-27 Siemens Westinghouse Power Corporation Liquid phase diffusion bonding to a superalloy component
US20050091848A1 (en) * 2003-11-03 2005-05-05 Nenov Krassimir P. Turbine blade and a method of manufacturing and repairing a turbine blade
US7343676B2 (en) * 2004-01-29 2008-03-18 United Technologies Corporation Method of restoring dimensions of an airfoil and preform for performing same
US7222422B2 (en) † 2004-02-16 2007-05-29 General Electric Company Method for refurbishing surfaces subjected to high compression contact
US7360991B2 (en) † 2004-06-09 2008-04-22 General Electric Company Methods and apparatus for fabricating gas turbine engines
US7335427B2 (en) 2004-12-17 2008-02-26 General Electric Company Preform and method of repairing nickel-base superalloys and components repaired thereby

Also Published As

Publication number Publication date
EP1803521A1 (de) 2007-07-04
KR20070073612A (ko) 2007-07-10
CN1994646A (zh) 2007-07-11
EP1803521B1 (de) 2009-09-16
KR101440152B1 (ko) 2014-09-12
ATE442932T1 (de) 2009-10-15
US20070154338A1 (en) 2007-07-05
PL1803521T3 (pl) 2010-02-26
JP2007224414A (ja) 2007-09-06
US8703044B2 (en) 2014-04-22
PL1803521T5 (pl) 2014-05-30
JP5698889B2 (ja) 2015-04-08
EP1803521B2 (de) 2013-12-11

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