发明名称 Composite blade with partial length spar
摘要 A composite axial flow rotary machine blade (50) and method of blade construction is disclosed. A partial-length, spanwisely-disposed hollow spar (20) partially captures a shaped foam core (30) which extends from within the spar's cavity (26) along a substantial length of the blade (50) in a spanwise fashion. A resin-impregnated high strength, high modulus cloth (34) and graphite (32) composition overlays the spar-core assembly (36) and forms the casing (50) with airfoil regions (52, 54) of the propeller blade (10). This construction results in a rotor blade (50) with enhanced natural frequencies thereby providing for an enhanced operational speed range.
申请公布号 US5269658(A) 申请公布日期 1993.12.14
申请号 US19900633566 申请日期 1990.12.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CARLSON, CHARLES E. K.;VIOLETTE, JOHN A.
分类号 B64C11/26;F01D5/28;F04D29/38;F04D29/66;(IPC1-7):B63H1/26 主分类号 B64C11/26
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