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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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