发明名称 TURBINE ENGINE HYBRID ROTOR
摘要 A turbine engine rotor component has a Ti-based first member (66) circumscribing an axis (500) and has either a circumferential array of integrally formed airfoils (62) or a circumferential array of blade retention features. A TiB particulate reinforced second member (90) also circumscribes the axis.
申请公布号 EP2971530(A4) 申请公布日期 2016.12.07
申请号 EP20140769241 申请日期 2014.03.11
申请人 United Technologies Corporation 发明人 HANSEN, James, O.
分类号 F01D5/14;B22F5/04;B22F7/08;C22C1/04;C22C14/00;C22C32/00;F01D5/34 主分类号 F01D5/14
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