发明名称 |
COMPOSITE BLADE MANUFACTURE |
摘要 |
<p>A method of manufacturing a lightweight composite propulsor blade of spar and shell construction comprises forming a composite spar (30) having an elongated foam body (20) bonded to a short metal retention tulip (10) and overlayed with a dry braided wrap of angular structural fibers and substantially unidirectional spanwisely aligned structural fiber plies disposed between the braided layers; adding a leading edge foam body (42) and a trailing edge foam body (44) to the spar assembly to form a blade subassembly (50); providing a dry braided fabric wrap over the blade assembly; disposing the fabric covered blade subassembly into a shell molding die and simultaneously impregnating the dry spar fabric wrap and the dry shell fabric wrap with a curable resin material; and curing the impregnated blade subassembly.</p> |
申请公布号 |
EP0610273(B1) |
申请公布日期 |
1995.12.27 |
申请号 |
EP19920921623 |
申请日期 |
1992.10.06 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
GRAFF, JOHN, M.;VIOLETTE, JOHN, A. |
分类号 |
B29C70/86;B29D99/00;B64C11/26;(IPC1-7):B29D31/00;B29C70/00 |
主分类号 |
B29C70/86 |
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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