发明名称 Single vacuum debulk composite panel repair
摘要 A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure.
申请公布号 US8790485(B2) 申请公布日期 2014.07.29
申请号 US200511064824 申请日期 2005.02.25
申请人 Bell Helicopter Textron Inc. 发明人 Whitworth Denver;Bergerson Anthony;Marvin Michael
分类号 B32B37/10;B29C65/18;B29C65/00;B29C73/10 主分类号 B32B37/10
代理机构 Pillsbury Winthrop Shaw Pittman LLP 代理人 Pillsbury Winthrop Shaw Pittman LLP
主权项 1. A method of attaching a composite member to a structure, comprising: forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying a partial vacuum at a first vacuum pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the structure by applying heat at a second temperature and by applying vacuum at a second vacuum pressure, the second vacuum pressure greater than the first vacuum pressure, wherein only a same single vacuum enclosure is used when applying heat at the first temperature, when applying the partial vacuum at the first vacuum pressure, and when curing the degassed, impregnated laminate.
地址 Hurst TX US