发明名称 Nickel-based superalloy and gas turbine blade using the same
摘要 A Ni-based superalloy contains 13.1 to 16.0 percent by mass of Cr, 1.0 to 6.8 percent by mass of Co, 3.0 to 3.4 percent by mass of Al, 4.6 to 5.6 percent by mass of Ti, 2.0 to 4.4 percent by mass of Ta, 3.5 to 4.9 percent by mass of W, 0.1 to 0.9 percent by mass of Mo, 0.3 to 1.4 percent by mass of Nb, 0.05 to 0.20 percent by mass of C, and 0.01 to 0.03 percent by mass of B with the remainder being nickel and inevitable impurities. The superalloy excels in corrosion resistance, oxidation resistance, has high strength, and is used in parts of a gas turbine to be used at high temperature. The resulting gas turbine excels in durability.
申请公布号 US9103003(B2) 申请公布日期 2015.08.11
申请号 US200912543623 申请日期 2009.08.19
申请人 Mitsubishi Hitachi Power Systems, Ltd. 发明人 Yoshinari Akira
分类号 C22C19/05;F01D5/28 主分类号 C22C19/05
代理机构 Crowell & Moring LLP 代理人 Crowell & Moring LLP
主权项 1. A casting that is a conventional casting formed of a Ni-based conventional casting superalloy comprising: 13.1 to 16.0 percent by mass of Cr, 1.0 to 6.8 percent by mass of Co, 3.0 to 3.4 percent by mass of Al, more than 5.0 to 5.6 percent by mass of Ti, 2.0 to 4.4 percent by mass of Ta, 3.5 to 4.9 percent by mass of W, 0.1 to 0.9 percent by mass of Mo, 0.3 to 1.4 percent by mass of Nb, 0.05 to 0.20 percent by mass of C, and 0.014 to 0.02 percent by mass B, with the remainder being Ni and inevitable impurities, the conventional casting containing equiaxis grains.
地址 Kanagawa JP