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
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