发明名称 Nickel base alloy and turbine engine blade cast therefrom.
摘要 <p>Improved nickel base alloys for use in vacuum directional solidification casting which alloys include a plurality of elements but which, in particular, include the following elements in the percentages by weight specified: carbon .07-.09, zirconium .007-.015, tungsten 9.3-9,7, and molybdenum 0.4-0.6. The new ultra high strength casting alloys are free of the problem of grain boundary cracking which has been encountered in the production of directional solidification castings of this type of alloy and minimize M6C acicular phase formation in turbine blades under high temperature conditions over extended operating periods. The invention also includes a turbine engine blade cast from the alloy.</p>
申请公布号 EP0032812(A1) 申请公布日期 1981.07.29
申请号 EP19810300158 申请日期 1981.01.14
申请人 CANNON-MUSKEGON CORPORATION 发明人 HARRIS, KENNETH
分类号 C22C19/05;C30B21/02;F01D5/28;(IPC1-7):22C19/05;30B21/02 主分类号 C22C19/05
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