SG103899A1 - Method of restoration of mehchanical properties of cast inconel 718 for serviced aircraft components - Google Patents

Method of restoration of mehchanical properties of cast inconel 718 for serviced aircraft components

Info

Publication number
SG103899A1
SG103899A1 SG200207629A SG200207629A SG103899A1 SG 103899 A1 SG103899 A1 SG 103899A1 SG 200207629 A SG200207629 A SG 200207629A SG 200207629 A SG200207629 A SG 200207629A SG 103899 A1 SG103899 A1 SG 103899A1
Authority
SG
Singapore
Prior art keywords
mehchanical
restoration
properties
aircraft components
cast inconel
Prior art date
Application number
SG200207629A
Other languages
English (en)
Inventor
Henry Harrison William
Joseph Kelly Thomas
James Weimer Michael
Original Assignee
Gen Electric
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=21848648&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=SG103899(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Gen Electric filed Critical Gen Electric
Publication of SG103899A1 publication Critical patent/SG103899A1/en

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
    • 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
    • Y10T29/49318—Repairing or disassembling

Landscapes

  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Articles (AREA)
  • Forging (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
SG200207629A 2001-12-20 2002-12-17 Method of restoration of mehchanical properties of cast inconel 718 for serviced aircraft components SG103899A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/029,365 US6755924B2 (en) 2001-12-20 2001-12-20 Method of restoration of mechanical properties of a cast nickel-based super alloy for serviced aircraft components

Publications (1)

Publication Number Publication Date
SG103899A1 true SG103899A1 (en) 2004-05-26

Family

ID=21848648

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200207629A SG103899A1 (en) 2001-12-20 2002-12-17 Method of restoration of mehchanical properties of cast inconel 718 for serviced aircraft components

Country Status (7)

Country Link
US (1) US6755924B2 (fr)
EP (1) EP1323842B1 (fr)
JP (1) JP4554882B2 (fr)
BR (1) BRPI0205198B1 (fr)
CA (1) CA2413641C (fr)
DE (1) DE60220012T2 (fr)
SG (1) SG103899A1 (fr)

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US7744709B2 (en) * 2005-08-22 2010-06-29 United Technologies Corporation Welding repair method for full hoop structures
US7531054B2 (en) * 2005-08-24 2009-05-12 Ati Properties, Inc. Nickel alloy and method including direct aging
US7503113B2 (en) * 2005-10-13 2009-03-17 Siemens Energy, Inc. Turbine vane airfoil reconfiguration system
US7708846B2 (en) * 2005-11-28 2010-05-04 United Technologies Corporation Superalloy stabilization
US7793416B2 (en) * 2006-05-15 2010-09-14 Viking Pump, Inc. Methods for hardening pump casings
US20070267109A1 (en) * 2006-05-17 2007-11-22 General Electric Company High pressure turbine airfoil recovery device and method of heat treatment
US7854064B2 (en) * 2006-06-05 2010-12-21 United Technologies Corporation Enhanced weldability for high strength cast and wrought nickel superalloys
US7653995B2 (en) * 2006-08-01 2010-02-02 Siemens Energy, Inc. Weld repair of superalloy materials
US7985304B2 (en) * 2007-04-19 2011-07-26 Ati Properties, Inc. Nickel-base alloys and articles made therefrom
EP2205771B1 (fr) * 2007-10-25 2019-04-03 GKN Aerospace Sweden AB Procédé, alliage à base de nickel et composant
US8192152B2 (en) * 2008-05-02 2012-06-05 United Technologies Corporation Repaired internal holding structures for gas turbine engine cases and method of repairing the same
US8257039B2 (en) * 2008-05-02 2012-09-04 United Technologies Corporation Gas turbine engine case with replaced flange and method of repairing the same using cold metal transfer
US8510926B2 (en) * 2008-05-05 2013-08-20 United Technologies Corporation Method for repairing a gas turbine engine component
US9598774B2 (en) 2011-12-16 2017-03-21 General Electric Corporation Cold spray of nickel-base alloys
CN102554552B (zh) * 2012-01-30 2014-02-05 重庆生竹科技发展有限公司 薄型空心辊的修复方法
US20160023439A1 (en) * 2014-07-22 2016-01-28 General Electric Company Method for joining high temperature materials and articles made therewith
US10563293B2 (en) 2015-12-07 2020-02-18 Ati Properties Llc Methods for processing nickel-base alloys
CN106914673B (zh) * 2017-04-13 2018-07-17 中国石油大学(华东) 一种镍基材料钎焊接头成分与力学性能均匀化方法
CN110964992B (zh) * 2019-11-28 2021-06-01 西安航天发动机有限公司 一种低温环境工作的增材制造高温合金的热处理方法
CN110842466B (zh) * 2019-11-30 2020-11-27 中车大连机车车辆有限公司 一种机车转向架构架变形的修复工艺

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Also Published As

Publication number Publication date
EP1323842A1 (fr) 2003-07-02
CA2413641A1 (fr) 2003-06-20
BRPI0205198B1 (pt) 2016-05-31
JP4554882B2 (ja) 2010-09-29
US20030116242A1 (en) 2003-06-26
BR0205198A (pt) 2004-06-29
JP2003231957A (ja) 2003-08-19
DE60220012D1 (de) 2007-06-21
EP1323842B1 (fr) 2007-05-09
CA2413641C (fr) 2010-08-10
US6755924B2 (en) 2004-06-29
DE60220012T2 (de) 2008-01-10

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