发明名称 |
Method of making composite fan blade |
摘要 |
<p>A method for designing a composite airfoil (10), comprises designing a mold (32) having an inner surface (32i) that defines a surface profile of the airfoil, defining a preliminary core surface of a woven core (30), wherein the preliminary core surface is offset from the inner surface of the mold (32i) by a specified percentage, filling the space between the mold (32) and the preliminary core surface with a plurality of plies (26) and assembling the woven core (30) and the plurality of plies (26) in the mold (32) and curing to form the composite airfoil (10).</p> |
申请公布号 |
EP2540486(A2) |
申请公布日期 |
2013.01.02 |
申请号 |
EP20120182979 |
申请日期 |
2010.11.29 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
PARKIN, MICHAEL;ALEXANDER, PHILLIP;HUTH, BRIAN P.;KLINETOB, CARL BRIAN |
分类号 |
B29D99/00;F01D5/28 |
主分类号 |
B29D99/00 |
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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