发明名称 航空機のプロペラ羽根
摘要 An aircraft propeller blade including an airfoil-profile structure. The airfoil-profile structure includes at least one fiber reinforcement obtained by three-dimensional weaving of yarns and densified by a matrix, and a shaping part made of cellular rigid material of determined shape, the reinforcement including at least two halves linked together by continuous weaving in the leading edge of the propeller blade, the two halves fitting tightly around the shaping part.
申请公布号 JP5922032(B2) 申请公布日期 2016.05.24
申请号 JP20120545382 申请日期 2010.12.20
申请人 スネクマ 发明人 クーペ,ドミニク;ダンブリン,ブルーノ・ジヤツク・ジエラール;マイユ,ジヤン−ノエル
分类号 B64C11/26;B29C39/10;B29C39/24;B29C70/10;D03D1/00;D03D3/00 主分类号 B64C11/26
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