PL1803521T5 - Sposób formowania warstwy utwardzającej powierzchnię na części składowej maszyny - Google Patents
Sposób formowania warstwy utwardzającej powierzchnię na części składowej maszynyInfo
- Publication number
- PL1803521T5 PL1803521T5 PL06126536T PL06126536T PL1803521T5 PL 1803521 T5 PL1803521 T5 PL 1803521T5 PL 06126536 T PL06126536 T PL 06126536T PL 06126536 T PL06126536 T PL 06126536T PL 1803521 T5 PL1803521 T5 PL 1803521T5
- Authority
- PL
- Poland
- Prior art keywords
- machine component
- sintered preform
- forming
- preform
- hardfacing layer
- Prior art date
Links
- 238000000034 method Methods 0.000 title abstract 7
- 238000005552 hardfacing Methods 0.000 title abstract 2
- 238000005219 brazing Methods 0.000 abstract 2
- 239000000463 material Substances 0.000 abstract 2
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
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 Printed Wiring (AREA)
- Manufacturing Of Magnetic Record Carriers (AREA)
- Manufacturing Of Printed Circuit Boards (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Applications Claiming Priority (2)
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 |
EP06126536.9A EP1803521B2 (en) | 2006-01-03 | 2006-12-19 | Method of forming a hardfacing layer on a machine component |
Publications (2)
Publication Number | Publication Date |
---|---|
PL1803521T3 PL1803521T3 (pl) | 2010-02-26 |
PL1803521T5 true PL1803521T5 (pl) | 2014-05-30 |
Family
ID=37852721
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL06126536T PL1803521T5 (pl) | 2006-01-03 | 2006-12-19 | Sposób formowania warstwy utwardzającej powierzchnię na części składowej maszyny |
Country Status (8)
Country | Link |
---|---|
US (1) | US8703044B2 (pl) |
EP (1) | EP1803521B2 (pl) |
JP (1) | JP5698889B2 (pl) |
KR (1) | KR101440152B1 (pl) |
CN (1) | CN1994646A (pl) |
AT (1) | ATE442932T1 (pl) |
DE (1) | DE602006009210D1 (pl) |
PL (1) | PL1803521T5 (pl) |
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US8182228B2 (en) * | 2007-08-16 | 2012-05-22 | General Electric Company | Turbine blade having midspan shroud with recessed wear pad and methods for manufacture |
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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 |
FR2948889B1 (fr) * | 2009-08-07 | 2011-08-26 | Snecma | Procede optimise de fabrication d'un disque aubage monobloc par jet d'eau abrasif |
FR2948888B1 (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 (en) * | 2010-02-10 | 2011-08-10 | Siemens Aktiengesellschaft | A method of manufacturing a hot-gas component with a cooling channel by brazing a sintered sheet on a carrier ;corresponding hot-gas component |
US8641381B2 (en) * | 2010-04-14 | 2014-02-04 | General Electric Company | System and method for reducing grain boundaries in shrouded airfoils |
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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 |
US10315264B2 (en) | 2013-01-29 | 2019-06-11 | General Electric Company | Joining process and joined article |
US20140212681A1 (en) * | 2013-01-29 | 2014-07-31 | General Electric Company | Joining process and joined article |
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US9346101B2 (en) | 2013-03-15 | 2016-05-24 | Kennametal Inc. | Cladded articles and methods of making the same |
US10279438B2 (en) | 2013-03-15 | 2019-05-07 | Siemens Energy, Inc. | Presintered preform for repair of superalloy component |
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 |
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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 |
US10450871B2 (en) | 2015-02-26 | 2019-10-22 | Rolls-Royce Corporation | Repair of dual walled metallic components using directed energy deposition material addition |
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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 |
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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 |
-
2006
- 2006-01-03 US US11/324,445 patent/US8703044B2/en active Active
- 2006-12-19 AT AT06126536T patent/ATE442932T1/de not_active IP Right Cessation
- 2006-12-19 EP EP06126536.9A patent/EP1803521B2/en active Active
- 2006-12-19 DE DE602006009210T patent/DE602006009210D1/de active Active
- 2006-12-19 PL PL06126536T patent/PL1803521T5/pl unknown
- 2006-12-26 JP JP2006350604A patent/JP5698889B2/ja active Active
- 2006-12-31 CN CNA200610172756XA patent/CN1994646A/zh active Pending
-
2007
- 2007-01-02 KR KR1020070000299A patent/KR101440152B1/ko active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP1803521B2 (en) | 2013-12-11 |
KR101440152B1 (ko) | 2014-09-12 |
JP2007224414A (ja) | 2007-09-06 |
DE602006009210D1 (de) | 2009-10-29 |
US20070154338A1 (en) | 2007-07-05 |
EP1803521A1 (en) | 2007-07-04 |
US8703044B2 (en) | 2014-04-22 |
EP1803521B1 (en) | 2009-09-16 |
JP5698889B2 (ja) | 2015-04-08 |
KR20070073612A (ko) | 2007-07-10 |
ATE442932T1 (de) | 2009-10-15 |
CN1994646A (zh) | 2007-07-11 |
PL1803521T3 (pl) | 2010-02-26 |
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