发明名称 SYSTEM AND METHOD FOR SECURELY CONNECTING PORTIONS OF A COMPOSITE STRUCTURE TOGETHER
摘要 A composite component assembly may include a composite core including a plurality of core cells between first and second ends. A connection joint is formed between the first and second ends. An adhesive layer is disposed within the connection joint between the first and second ends. The adhesive layer is configured to bond the first and second ends through a curing process. A peg splice securing joint securely connects the first and second ends together before and during the curing process.
申请公布号 CA2925896(A1) 申请公布日期 2016.10.03
申请号 CA20162925896 申请日期 2016.04.01
申请人 THE BOEING COMPANY 发明人 TAYLOR, BRUCE;GIBBINGS, GEOFFREY;BRAUN, RUDY;ADVENT, KYLE CHRISTOPHER
分类号 B32B3/06;B32B3/12;B32B7/12;B32B37/12;F02C7/24 主分类号 B32B3/06
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