发明名称 COMPOSITE ROTOR BLADE
摘要 <p>COMPOSITE ROTOR BLADE A compressor rotor blade for a turbomachine is disclosed. Techniques for increasing the strength to weight ratio of the blade while maintaining adequate resistance to foreign object damage are developed. In one specific embodiment an all composite construction employs matrix materials of varied ductilities and yield strengths to improve the energy absorbing capabilities of the blade.</p>
申请公布号 IL53512(D0) 申请公布日期 1978.03.10
申请号 IL19770053512 申请日期 1977.12.02
申请人 UNITED TECHNOLOGIES CORP 发明人
分类号 B32B1/00;C22C47/00;C22C47/06;F01D5/28;F02K3/04;F04D29/02;F04D29/38 主分类号 B32B1/00
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