发明名称 Method of making bead-stiffened composite parts and parts made thereby
摘要 A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
申请公布号 US8052826(B2) 申请公布日期 2011.11.08
申请号 US20090409742 申请日期 2009.03.24
申请人 THE BOEING COMPANY 发明人 BURPO STEVEN J.;RENIERI MICHAEL P.;SEGOBIANO NICHOLAS B.;FROESCHNER NEAL A.
分类号 B29C65/00;B32B37/02;B32B38/04 主分类号 B29C65/00
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