| 发明名称 |
DECOMPRESSION PANEL FOR USE IN AN AIRCRAFT ASSEMBLY |
| 摘要 |
A decompression panel for use in an aircraft assembly is provided. The decompression panel includes a body portion including a top edge and a bottom edge, and a front surface and a rear surface opposing the front surface. A plurality of openings are formed in the body portion, and a first stiffening member is formed on the rear surface below the plurality of openings. The first stiffening member extends from the rear surface towards the top edge such that the plurality of openings are at least partially obstructed by the first stiffening member. |
| 申请公布号 |
US2015115104(A1) |
申请公布日期 |
2015.04.30 |
| 申请号 |
US201414471161 |
申请日期 |
2014.08.28 |
| 申请人 |
The Boeing Company |
发明人 |
Perkins Thomas;Tatum Jeremy Ryan Glaze;Loken Allan A.;Arm Hannah Rebecca |
| 分类号 |
B64C1/06;B32B3/26 |
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 assembly, said decompression panel comprising:
a body portion comprising a top edge and a bottom edge, and a front surface and a rear surface opposing said front surface; a plurality of openings formed in said body portion; and a first stiffening member formed on said rear surface below said plurality of openings, said first stiffening member extending from said rear surface towards said top edge such that said plurality of openings are at least partially obstructed by said first stiffening member. |
| 地址 |
Huntington Beach CA US |
