| 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 in a non-uniform pattern onto a first face sheet, the non-uniform pattern producing non-uniform spacing between adjacent core wafers; assembling a second face sheet onto the plurality of wafers; and curing an adhesive to create a bond between the plurality of wafers, the first face sheet, and the second face sheet. |
| 申请公布号 |
US2015037533(A1) |
申请公布日期 |
2015.02.05 |
| 申请号 |
US201313955105 |
申请日期 |
2013.07.31 |
| 申请人 |
Bell Helicopter Textron Inc. |
发明人 |
Kendrick Phillip A.;Oldroyd Paul K.;Carlson David G. |
| 分类号 |
B32B3/12;B64C1/18;B64C3/20;B32B37/14 |
主分类号 |
B32B3/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of manufacturing a core stiffened structure, the core stiffened structure having a first face sheet, a second face sheet, and a plurality of wafers of composite core, the method comprising:
orienting the plurality of wafers in a non-uniform pattern onto the first face sheet, the non-uniform pattern producing non-uniform spacing between adjacent wafers; assembling a second face sheet onto the plurality of wafers; and curing an adhesive to create a bond between the plurality of wafers, the first face sheet, and the second face sheet. |
| 地址 |
Fort Worth TX US |
