发明名称 |
Distribution of point loads in honeycomb panels |
摘要 |
Composite panels used in aircraft are formed by a sandwich including a lightweight honeycomb core reinforced by a solid plank in medial regions of the panel. The plank is bonded to the honeycomb and forms an integral part of the core where a strut is attached to the panel. The plank distributes point loads imposed on the panel by the strut. |
申请公布号 |
US8418962(B2) |
申请公布日期 |
2013.04.16 |
申请号 |
US20080017009 |
申请日期 |
2008.01.19 |
申请人 |
PIEHL MARC. J.;FRISCH DOUGLAS A.;KAJITA KIRK B.;THE BOEING COMPANY |
发明人 |
PIEHL MARC. J.;FRISCH DOUGLAS A.;KAJITA KIRK B. |
分类号 |
B64C1/06 |
主分类号 |
B64C1/06 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|