发明名称 HYBRID TURBINE BLADE FOR IMPROVED ENGINE PERFORMANCE OR ARCHITECTURE
摘要 A method is provided for casting an article such as a blade having an attachment root and an airfoil, the airfoil having a proximal end and a distal end. The method comprises introducing a molten alloy into a mold; and varying a composition of the introduced alloy during the introduction so as to produce a compositional variation.
申请公布号 EP2931459(A2) 申请公布日期 2015.10.21
申请号 EP20130876615 申请日期 2013.12.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SHAH, DILIP M.;CETEL, ALAN D.
分类号 B22D19/16;B22D25/00;C22C19/03 主分类号 B22D19/16
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