发明名称 |
Method of making bead-stiffened composite parts and parts made thereby |
摘要 |
A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
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申请公布号 |
US8052826(B2) |
申请公布日期 |
2011.11.08 |
申请号 |
US20090409742 |
申请日期 |
2009.03.24 |
申请人 |
THE BOEING COMPANY |
发明人 |
BURPO STEVEN J.;RENIERI MICHAEL P.;SEGOBIANO NICHOLAS B.;FROESCHNER NEAL A. |
分类号 |
B29C65/00;B32B37/02;B32B38/04 |
主分类号 |
B29C65/00 |
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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