发明名称 High performance wrought powder metal articles and method of manufacture
摘要 A nickel base powder metallurgy superalloy gas turbine engine disk for a compressor or turbine. The wrought powder metallurgy gas turbine engine disk has desirable fatigue crack growth resistance and a superior balance of tensile, creep rupture and low cycle fatigue strength characteristics. In one embodiment the disk defines a segregation free homogenous structure.
申请公布号 US6551372(B1) 申请公布日期 2003.04.22
申请号 US20000663025 申请日期 2000.09.15
申请人 ROLLS-ROYCE CORPORATION 发明人 EWING BRUCE A.;JAIN SUSHIL K.;GREEN KENNETH A.;HELMINK RANDOLPH C.;JAMES ALLISTER
分类号 C22C1/04;C22C19/05;C22F1/10;F01D5/28;(IPC1-7):C22C33/02 主分类号 C22C1/04
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