发明名称 |
Method of configuring composite core in a core stiffened structure and a structure incorporating the same |
摘要 |
A method of manufacturing a core stiffened structure includes orienting the plurality of core wafers (2401) in a non-uniform pattern onto a first face sheet (2805), the non-uniform pattern producing non-uniform spacing (2809) between adjacent core wafers; assembling a second face sheet (2803) onto the plurality of wafers (2401); and curing an adhesive to create a bond between the plurality of wafers (2401), the first face sheet (2805), and the second face sheet (2803). |
申请公布号 |
EP2832533(B1) |
申请公布日期 |
2016.03.23 |
申请号 |
EP20130195029 |
申请日期 |
2013.11.29 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
KENDRICK, PHILLIP A.;CARLSON, DAVID G.;OLDROYD, PAUL K. |
分类号 |
B29D99/00;B32B3/12;B32B3/18;B32B3/20;B32B3/22;B32B5/14 |
主分类号 |
B29D99/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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