发明名称 Composite composition for turbine blade tips, related articles, and methods
摘要 A composite composition that includes an MCrAlX alloy and a nano-oxide ceramic is disclosed. In the formula, M includes nickel, cobalt, iron, or a combination thereof, and X includes yttrium, hafnium, or a combination thereof, from about 0.001 percent to about 2 percent by weight of the alloy. The amount of the nano-oxide ceramic is greater than about 40 percent, by volume of the composition. A protective covering that includes the composite composition is also disclosed. The protective covering can be attached to a tip portion of a blade with a braze material. A method for joining a protective covering to a tip portion of a blade, and a method for repair of a blade, are also provided.
申请公布号 US9511436(B2) 申请公布日期 2016.12.06
申请号 US201314075156 申请日期 2013.11.08
申请人 General Electric Company 发明人 Kumar Sundeep;Krishnamurthy Anand;Onal Kivilcim;Subramanian Pazhayannur Ramanathan;Gray Dennis Michael;Parakala Padmaja
分类号 B23K1/00;C04B35/117;C04B35/46;C04B35/488;C04B35/495;C04B35/50;C04B35/505;B23K1/012;B32B9/00;B32B9/04 主分类号 B23K1/00
代理机构 代理人 Coppa Francis T.
主权项 1. A protective covering comprising a composite composition bonded to a substrate with a braze material, wherein the composite composition comprises: a MCrAlX alloy, wherein M comprises nickel, cobalt, iron, or combinations thereof, and X comprises, by weight of the alloy, from about 0.001 percent to about 2 percent yttrium, hafnium, or a combination thereof; a nano-oxide ceramic in a range from about 70 percent to about 90 percent by volume of the composite composition; and wherein the braze material comprises a nickel-based alloy having from about 1 percent to about 10 percent titanium by weight of the braze material.
地址 Niskayuna NY US