发明名称 BRAZE ALLOY COMPOSITIONS AND BRAZING METHODS FOR SUPERALLOYS
摘要 A multi-component braze filler alloy comprising 60-70% by weight CM247 superalloy and BRB braze alloy is diffusion brazed to a CM247 alloy base substrate, such as a gas turbine blade or vane. The substrate/braze interface may be subsequently weld-repaired without de-melting and migrating the braze alloy from the interface. The weld zone and surrounding area are solidification crack resistant. After the alloy composition is brazed to the base substrate the component may be returned to service. Thereafter the component remains repairable by welding or re-brazing, if needed to correct future in-service defects.
申请公布号 US2015125282(A1) 申请公布日期 2015.05.07
申请号 US201314070664 申请日期 2013.11.04
申请人 Georgieva Petya M.;Yarbrough James A. 发明人 Georgieva Petya M.;Yarbrough James A.
分类号 F01D5/00;F01D9/02;F01D5/12;B23K35/30;B23K1/00 主分类号 F01D5/00
代理机构 代理人
主权项 1. A material for the braze repair of a nickel-base superalloy turbine component comprising a CM247/BRB mixture of CM247 base alloy in the range from approximately 60% to 70% by weight and the balance comprises BRB braze alloy.
地址 Oviedo FL US