| 发明名称 |
DECOMPRESSION PANEL FOR USE IN AN AIRCRAFT |
| 摘要 |
A decompression panel includes a body portion having a first end and a second end opposing the first end. The decompression panel also includes a tab extending along the first end and a flange coupled to the body portion. The flange defines a slot adjacent the second end. The decompression panel is secured in an airplane cabin by the tab and slot features, such that unwanted access to areas behind such panels is prevented. |
| 申请公布号 |
US2015115102(A1) |
申请公布日期 |
2015.04.30 |
| 申请号 |
US201414228524 |
申请日期 |
2014.03.28 |
| 申请人 |
The Boeing Company |
发明人 |
Perkins Thomas;Olliges Michael J.;Loken Allan A.;Arm Hannah Rebecca;Glaze Tatum Jeremy Ryan |
| 分类号 |
B64C1/06;B32B3/06 |
主分类号 |
B64C1/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A decompression panel for use in an aircraft, said decompression panel comprising:
a body portion comprising a first end and an opposing second end; a tab extending along said first end; and a flange extending from said body portion, said flange defining a slot adjacent said second end. |
| 地址 |
Seal Beach CA US |
