发明名称 COMPOSITE AIRFOIL CONSTRUCTION
摘要 <p>An article such as a blade fabricated from a plurality of highstrength, reinforcing filaments embedded in a matrix material and characterized by a portion of the filaments oriented transverse to the blade longitudinal axis in a direction through the blade to enhance transverse shear strength. In one embodiment, a plurality of columnar filament cores are each wrapped with a filament sheet and bonded together laterally to form the blade primary structure. The orientation of the filaments within the sheet forms an angle with the core longitudinal axes such that at least a portion of the sheet filaments runs transverse to the blade from one aerodynamic surface to the other. In an alternative embodiment, a blade is formed of a plurality of bonded filament laminates accordian folded with the fold lines angled with respect to the longitudinal axes of the filaments, the distance between fold lines being equal to or greater than the blade thickness.</p>
申请公布号 CA1095664(A) 申请公布日期 1981.02.17
申请号 CA19770282178 申请日期 1977.07.06
申请人 GENERAL ELECTRIC COMPANY 发明人 ADAMSON, ARTHUR P.
分类号 B21K3/00;B23P15/02;B23P15/04;(IPC1-7):23P3/00;23P15/04;21K3/00;23P15/02 主分类号 B21K3/00
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