发明名称 |
COMPOSITE MATERIAL PLACEMENT METHOD |
摘要 |
To apply a course on a layup mold, a ply boundary that defines a ply area on the layup mold is determined and a tape of composite material is applied on the ply area at an oblique angle relative to the ply boundary. In addition, a leading edge of the tape is butt cut and the leading edge, and the ply boundary essentially converge. Furthermore, a trailing edge is generated. The trailing edge is a butt cut and the trailing edge and the ply boundary essentially converge. |
申请公布号 |
EP1986842(B1) |
申请公布日期 |
2016.09.28 |
申请号 |
EP20070750758 |
申请日期 |
2007.02.13 |
申请人 |
THE BOEING COMPANY |
发明人 |
JOHNSON, BRICE, A.;CARBERY, DAVID, J. |
分类号 |
B29C70/38;B29C70/32;B29C70/54 |
主分类号 |
B29C70/38 |
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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