发明名称 METHOD AND APPARATUS FOR FORMING FUSELAGE STRINGERS
摘要 A composite part, such as a stiffener is formed in place. A composite charge (30) is placed on a tool spanning a mold cavity (54), with the centerline of the charge (32) offset from the centerline of the mold cavity (28). Opposite sides of the charge (70, 74) are held against the tool as the charge (30) is formed into the mold cavity (54). One side of the charge (70) is held against movement on the tool while the other side of the charge (74) is allowed to slip over the tool toward the mold cavity (54).
申请公布号 CA2882362(A1) 申请公布日期 2014.04.17
申请号 CA20132882362 申请日期 2013.09.03
申请人 THE BOEING COMPANY 发明人 COXON, BRAD A.;KLEWIADA, MARK;WRIGHT, DONALD E.;MODIN, ANDREW E.
分类号 B29C70/54;B29C70/44;B29C70/56;B29D99/00 主分类号 B29C70/54
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