发明名称 Molding process for producing unified composite structures
摘要 A method of forming a unitary, composite structural member, and a member formed in accordance with the process. The process involves stitching a plurality of warp knit panel sections together to generally form a plurality of independent panel sections. The sections are placed within the dies of a molding tool such that a rib portion of each section aligns. Inflatable bladders are then slipped into voids formed in between the various panel sections of the assembly. The bladders are inflated to hold the panel sections in the shape of the final product and to hold the rib portions in contact with one another. Resin is then infused into the panels that make up the assembly. The assembly is then cured. When the panels are removed from the molding tool a unitary, complexly shaped, composite structural member is formed. The invention provides the advantage of not requiring any subsequent manufacturing step such as bonding or mechanical fastening of two or more sub-panels in order to form the finished structural part.
申请公布号 EP1459873(A2) 申请公布日期 2004.09.22
申请号 EP20040006496 申请日期 2004.03.18
申请人 THE BOEING COMPANY 发明人 VELICKI ALEXANDER;THRASH PATRICK JOSEPH;BURGESS ROGER ALAN;STANDISH COLE
分类号 B29C70/44;B29C65/00;B29D24/00;B64C1/00;B64C3/18 主分类号 B29C70/44
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