发明名称 Forming of staged thermoset composite materials
摘要 A method of forming a composite article may include initially curing a composite laminate at an initial temperature to an initial cure stage of 30-50 percent of full cure and beyond a gel point to form an initially-cured composite laminate. The method may initially include heating the initially-cured composite laminate to an intermediate temperature higher than the initial temperature and above a resin glass transition temperature. In addition, the method may include intermediately curing the composite laminate to an intermediate cure stage of 50-70 percent of full cure while on a final forming tool to form an intermediately-cured composite laminate. Furthermore, the method may include removing the intermediately-cured composite laminate from the final forming tool, and finally curing the intermediately-cured composite laminate at a final temperature higher than the intermediate temperature to a final cure stage.
申请公布号 US9539767(B2) 申请公布日期 2017.01.10
申请号 US201414561900 申请日期 2014.12.05
申请人 The Boeing Company 发明人 Butler Geoffrey A.
分类号 B29C35/02;B29C70/30;B29C70/44;B29C73/10;B29C73/12;B29C65/00;B29K105/24 主分类号 B29C35/02
代理机构 代理人
主权项 1. A method of forming a composite article, comprising: initially curing a composite laminate at an initial temperature to an initial cure stage of 30-50 percent of full cure and beyond a gel point to form an initially-cured composite laminate; heating the initially-cured composite laminate to an intermediate temperature higher than the initial temperature and above a resin glass transition temperature; intermediately curing the composite laminate to an intermediate cure stage of 50-70 percent of full cure while on a final forming tool to form an intermediately-cured composite laminate; removing the intermediately-cured composite laminate from the final forming tool; and finally curing the intermediately-cured composite laminate at a final temperature higher than the intermediate temperature to a final cure stage.
地址 Chicago IL US
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