JP2013007118A5 - - Google Patents

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Publication number
JP2013007118A5
JP2013007118A5 JP2012104405A JP2012104405A JP2013007118A5 JP 2013007118 A5 JP2013007118 A5 JP 2013007118A5 JP 2012104405 A JP2012104405 A JP 2012104405A JP 2012104405 A JP2012104405 A JP 2012104405A JP 2013007118 A5 JP2013007118 A5 JP 2013007118A5
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JP
Japan
Prior art keywords
product
joint
strain
preforms
forging
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.)
Granted
Application number
JP2012104405A
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English (en)
Japanese (ja)
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JP2013007118A (ja
JP6165417B2 (ja
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Publication date
Priority claimed from US13/100,364 external-priority patent/US8918996B2/en
Application filed filed Critical
Publication of JP2013007118A publication Critical patent/JP2013007118A/ja
Publication of JP2013007118A5 publication Critical patent/JP2013007118A5/ja
Application granted granted Critical
Publication of JP6165417B2 publication Critical patent/JP6165417B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2012104405A 2011-05-04 2012-05-01 構成要素及び異なる粒子構造を有する領域を有する構成要素を製造する方法 Expired - Fee Related JP6165417B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/100,364 US8918996B2 (en) 2011-05-04 2011-05-04 Components and processes of producing components with regions having different grain structures
US13/100,364 2011-05-04

Publications (3)

Publication Number Publication Date
JP2013007118A JP2013007118A (ja) 2013-01-10
JP2013007118A5 true JP2013007118A5 (enExample) 2017-03-02
JP6165417B2 JP6165417B2 (ja) 2017-07-19

Family

ID=46052641

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012104405A Expired - Fee Related JP6165417B2 (ja) 2011-05-04 2012-05-01 構成要素及び異なる粒子構造を有する領域を有する構成要素を製造する方法

Country Status (4)

Country Link
US (1) US8918996B2 (enExample)
EP (1) EP2520395A3 (enExample)
JP (1) JP6165417B2 (enExample)
CA (1) CA2775920A1 (enExample)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008052030B4 (de) * 2008-10-16 2011-06-16 Mtu Aero Engines Gmbh Verfahren zum Verbinden wenigstens einer Turbinenschaufel mit einer Turbinenscheibe oder einem Turbinenring
EP2764947A1 (de) * 2013-02-12 2014-08-13 Siemens Aktiengesellschaft Fügeverbindungsvorformling, Verfahren zum Fügen sowie Verbundwerkstück mit härtender gamma-prime-Phase umfassenden Fügepartnern
FR3009800B1 (fr) * 2013-08-23 2016-02-12 Snecma Procede de fabrication d'une piece par soudage de parties
US9874099B2 (en) 2015-07-01 2018-01-23 Electro-Motive Diesel, Inc. Turbocharger having improved rupture containment
EP3239468A1 (de) * 2016-04-27 2017-11-01 MTU Aero Engines GmbH Verfahren zum herstellen einer schaufel für eine strömungsmaschine
GB201612912D0 (en) * 2016-07-26 2016-09-07 Rolls Royce Plc Rotary friction welding
US20180105914A1 (en) * 2016-10-13 2018-04-19 United Technologies Corporation Hybrid component and method of making
US20180104765A1 (en) * 2016-10-13 2018-04-19 United Technologies Corporation Hybrid component and method of making
GB2560001B (en) * 2017-02-24 2019-07-17 Rolls Royce Plc A weld stub arrangement and a method of using the arrangement to make an article
US10946476B2 (en) * 2017-05-11 2021-03-16 Raytheon Technologies Corporation Heat treatment and stress relief for solid-state welded nickel alloys
US10718041B2 (en) * 2017-06-26 2020-07-21 Raytheon Technologies Corporation Solid-state welding of coarse grain powder metallurgy nickel-based superalloys
US10751843B2 (en) 2017-06-30 2020-08-25 Honeywell International Inc. Turbine wheels, turbine engines including the same, and methods of fabricating turbine wheels with improved bond line geometry
EP3441166A1 (en) * 2017-08-08 2019-02-13 Siemens Aktiengesellschaft Improvements relating to components manufactured from metal alloys
US11897065B2 (en) 2019-11-12 2024-02-13 Honeywell International Inc. Composite turbine disc rotor for turbomachine
US11549374B2 (en) * 2020-02-18 2023-01-10 Raytheon Technologies Corporation Gas turbine rotor component and method of manufacture

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3576681A (en) 1969-03-26 1971-04-27 Gen Electric Wrought nickel base alloy article
US4063939A (en) * 1975-06-27 1977-12-20 Special Metals Corporation Composite turbine wheel and process for making same
US4479293A (en) * 1981-11-27 1984-10-30 United Technologies Corporation Process for fabricating integrally bladed bimetallic rotors
JPS58103972A (ja) * 1981-12-16 1983-06-21 Hitachi Ltd 超合金耐熱材料の溶接方法
US4820358A (en) 1987-04-01 1989-04-11 General Electric Company Method of making high strength superalloy components with graded properties
US5106012A (en) 1989-07-10 1992-04-21 Wyman-Gordon Company Dual-alloy disk system
US4957567A (en) 1988-12-13 1990-09-18 General Electric Company Fatigue crack growth resistant nickel-base article and alloy and method for making
US5161950A (en) * 1989-10-04 1992-11-10 General Electric Company Dual alloy turbine disk
US5100050A (en) 1989-10-04 1992-03-31 General Electric Company Method of manufacturing dual alloy turbine disks
US5527402A (en) 1992-03-13 1996-06-18 General Electric Company Differentially heat treated process for the manufacture thereof
US6521175B1 (en) 1998-02-09 2003-02-18 General Electric Co. Superalloy optimized for high-temperature performance in high-pressure turbine disks
US6969238B2 (en) * 2003-10-21 2005-11-29 General Electric Company Tri-property rotor assembly of a turbine engine, and method for its preparation
JP5109115B2 (ja) * 2005-04-07 2012-12-26 国立大学法人 長崎大学 ニッケル基超合金及びその製造方法
US7891952B2 (en) 2006-11-28 2011-02-22 General Electric Company Rotary machine components and methods of fabricating such components
US20080124210A1 (en) 2006-11-28 2008-05-29 Peter Wayte Rotary assembly components and methods of fabricating such components
US8262817B2 (en) * 2007-06-11 2012-09-11 Honeywell International Inc. First stage dual-alloy turbine wheel
US20090000706A1 (en) * 2007-06-28 2009-01-01 General Electric Company Method of controlling and refining final grain size in supersolvus heat treated nickel-base superalloys
US8083872B2 (en) * 2007-08-03 2011-12-27 Rolls-Royce Plc Method of heat treating a superalloy component and an alloy component
JP4719780B2 (ja) * 2008-09-09 2011-07-06 株式会社日立製作所 タービン用の溶接型ロータおよびその製造方法
US8187724B2 (en) * 2009-02-24 2012-05-29 Honeywell International Inc. Method of manufacture of a dual alloy impeller
US20100329883A1 (en) * 2009-06-30 2010-12-30 General Electric Company Method of controlling and refining final grain size in supersolvus heat treated nickel-base superalloys
JP2011064077A (ja) * 2009-09-15 2011-03-31 Toshiba Corp ガスタービン部品およびその補修方法

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