发明名称 Composite material placement method and system
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 US7867352(B2) 申请公布日期 2011.01.11
申请号 US20060352274 申请日期 2006.02.13
申请人 THE BOEING COMPANY 发明人 JOHNSON BRICE A.;CARBERY DAVID J.
分类号 B32B38/04 主分类号 B32B38/04
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