发明名称 Turbine component and a process of fabricating a turbine component
摘要 <p>A turbine component (101) and a process of fabricating a component are disclosed. The process includes excavating a base metal (103) of the component to form a fill region (105) and filling the fill region (105) with a filler metal (107). The filler metal (107) has a filler metal elongation that is at least 25% greater than a base metal elongation of the base metal (103). The filler includes, by weight, between about 4% and about 7% iron, between about 14% and about 17% chromium, between about 15% and about 17% molybdenum, between about 3% and about 5% tungsten, up to about 0.02% carbon, up to about 1% manganese, up to about 2.5% cobalt, and a balance of nickel and/or the filler metal elongation is greater than about 35% in/in per two inches.</p>
申请公布号 GB2520194(A) 申请公布日期 2015.05.13
申请号 GB20150000510 申请日期 2013.06.19
申请人 GENERAL ELECTRIC COMPANY 发明人 ERIC EICHER MCCONNELL;STEPHEN GERARD POPE;BILL DAMON JOHNSTON;JOHN GREGORY OBEIRNE
分类号 B23K35/30;B23K1/00;B23K9/23;B23K9/235;B23K20/12;B23K28/02;B23P6/00;C22C19/05 主分类号 B23K35/30
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