发明名称 STRUCTURAL BRAZE REPAIR OF SUPERALLOY COMPONENT
摘要 Boron and silicon free braze alloys useful for structural repairs of superalloy gas turbine engine components. The braze alloy composition may contain only elements that are contained in the superalloy material to be repaired, and may have melting temperature ranges as low as 10 °C. to facilitate producing a high strength homogenized braze joint during a solution heat treatment of the superalloy substrate material.
申请公布号 WO2014197060(A3) 申请公布日期 2015.02.26
申请号 WO2014US25354 申请日期 2014.03.13
申请人 SIEMENS ENERGY, INC. 发明人 OZBAYSAL, KAZIM
分类号 B23K35/30;B23K1/00;B23K1/19;B23K1/20;B23K35/02;B23P6/00;C22C19/05;F01D5/00 主分类号 B23K35/30
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