| 发明名称 |
WINDOW PANEL FOR AN AIRFRAME AND METHOD OF PRODUCING SAME |
| 摘要 |
The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core. |
| 申请公布号 |
US2015064389(A1) |
申请公布日期 |
2015.03.05 |
| 申请号 |
US201414469146 |
申请日期 |
2014.08.26 |
| 申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
Zahlen Pierre C.;Born Johannes;Meyer Lars;Baumbach Gregor;Hanske Claus;Prowe Jens;Oentoro Johan;Zuardy M. Ichwan;Brok Wouter;Metten Martin |
| 分类号 |
B64C1/14;B32B37/16;B32B5/18;B32B3/26;B32B7/04;E06B3/263;B32B37/30 |
主分类号 |
B64C1/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A window panel for a body structure of a vehicle, comprising:
a first skin extending over a first side of the panel to form an outer skin of the vehicle body structure; a second skin extending over a second side of the panel to form an inner skin of the vehicle body structure; a core located between and covered by the first and second skins in a sandwich structure; and at least one window aperture formed through the first layer, the core, and the second layer. |
| 地址 |
Hamburg DE |
