发明名称 METHOD OF MANUFACTURING CURVED COMPOSITE STRUCTURAL ELEMENTS
摘要 A method of manufacturing curved composite structural elements can include fabricating a web ply in a flat curve over a removable substrate and laying up the ply on a curved web surface of a manufacturing tool. The method also can include laying up a diagonal ply with fibers oriented at +/-45° from the centerline of the web surface. The method further can include cutting a unidirectional composite tape into segments and laying up the tape segments to form a cross ply with a fiber orientation normal to the centerline of the web surface. One or both edges of the diagonal and cross plies may be folded over one or two sides of the manufacturing tool to form one or two flange surfaces. Additionally, a cap ply can be laid up on one or both flange surfaces using composite tape. The structural element layup can then be inspected and any excess composite material can be trimmed away.
申请公布号 HK1115098(A1) 申请公布日期 2012.09.21
申请号 HK20080110115 申请日期 2008.09.11
申请人 THE BOEING COMPANY 发明人 BROWN, TODD A.;FRIDDELL, STEPHEN DOUGLAS;HARRIS, CHRISTOPHER G.;MODIN, ANDREW E.
分类号 B29C 主分类号 B29C
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