发明名称 TRANSITION REINFORCEMENT OF COMPOSITE BLADE DOVETAILS
摘要 <p>The composite filament laminates of a composite blade are splayed at the root thereof to receive metallic inserts therebetween. A transition material having a modulus of elasticity greater than that of the inserts and less than that of the laminates is bonded therebetween to more uniformly distribute the blade loadings into the root region.</p>
申请公布号 CA1042350(A) 申请公布日期 1978.11.14
申请号 CA19760266622 申请日期 1976.11.26
申请人 GENERAL ELECTRIC COMPANY 发明人 CARLSON, ROBERT G.
分类号 F01D5/30;C22C47/00;F01D5/28;F04D29/38;(IPC1-7):04D29/38 主分类号 F01D5/30
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