发明名称 |
Method for forming bends in composite panels and composite panels made thereby |
摘要 |
A composite panel with a bend therein is formed by first and second adjacent panel sections having a common facesheet forming an outer radius of the bend, and a substantially void-free joint between the adjacent panel sections. |
申请公布号 |
US9114587(B2) |
申请公布日期 |
2015.08.25 |
申请号 |
US201213660554 |
申请日期 |
2012.10.25 |
申请人 |
THE BOEING COMPANY |
发明人 |
Lewis Michael S.;Roets Guy W. |
分类号 |
B32B3/04;B32B3/10;B26D3/06;B29C53/06;B32B3/12;B32B3/26;B26D5/20;B29L9/00 |
主分类号 |
B32B3/04 |
代理机构 |
Yee & Associates, P.C. |
代理人 |
Yee & Associates, P.C. |
主权项 |
1. A composite panel having a curved bend therein, consisting essentially of:
a first panel section comprising a first core section having a first inclined surface and a first flange formed therein, the first core section sandwiched between a common facesheet and a first separate facesheet; a second panel section comprising a second core section having a second inclined surface and a second flange formed therein, the second core section completely divided from the first core section by a slot, the slot forming the first inclined surface and the second inclined surface, the second core section sandwiched between the common facesheet and a second separate facesheet, the common facesheet forming an outer arcuate surface of the curved bend; and a substantially void-free joint between the first panel section and the second panel section, in which the joint includes the first inclined surface and the second inclined surface engaged in substantially face-to-face contact along a plane passing through the radius of the curved bend. |
地址 |
Chicago IL US |