发明名称 STRUCTURAL INSERTS FOR HONEYCOMB STRUCTURES
摘要 <p>A method and apparatus for manufacturing a sandwich structure. A cavity is formed in a core of the sandwich structure. A structural insert is placed into the cavity. The structural insert comprises a first number of parts configured to receive a load and a second number of parts assembled with the first number of parts to form the structural insert.</p>
申请公布号 CA2859329(A1) 申请公布日期 2015.03.03
申请号 CA20142859329 申请日期 2014.08.14
申请人 THE BOEING COMPANY 发明人 HOLEMANS, PETER
分类号 B32B3/08;B32B3/12 主分类号 B32B3/08
代理机构 代理人
主权项
地址