| 发明名称 |
SANDWICH PANEL FOR AN AIRCRAFT |
| 摘要 |
A sandwich panel for an aircraft includes a lower top layer, an upper top layer and a core layer, wherein the core layer in turn includes pins. The pins extend from a lower top layer in the direction of the upper top layer, and the pins are interconnected by rods. In addition, the rods run inside the core layer, and the pins and rods form a one-piece network. |
| 申请公布号 |
US2016297509(A1) |
申请公布日期 |
2016.10.13 |
| 申请号 |
US201615041474 |
申请日期 |
2016.02.11 |
| 申请人 |
Airbus Operations GmbH |
发明人 |
Estadieu Jean-Bernard;Tchankova Lubka;Dering Fedor |
| 分类号 |
B64C1/18;B29C67/00 |
主分类号 |
B64C1/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A sandwich panel for an aircraft, the sandwich panel comprising:
a lower top layer; an upper top layer; and a core layer, wherein the core layer includes a plurality of pins, wherein the plurality of pins extends from the lower top layer in the direction of the upper top layer, wherein the pins are interconnected by a plurality of rods, wherein the plurality of rods run inside the core layer, and wherein the pins and rods form a one-piece network. |
| 地址 |
Hamburg DE |
