| 发明名称 |
AIRCRAFT DOOR AND AIRCRAFT COMPRISING SUCH AN AIRCRAFT DOOR |
| 摘要 |
An aircraft door includes an outer shell with an exterior and an interior, a stiffening structure arranged on the interior of the outer shell, and at least one door seal arranged on the interior of the outer shell. The door seal is circumferential in an edge region. In the edge region between the outer shell and the door seal at least one circumferential stiffening component is arranged that is connected to the stiffening structure. Thus, in a particularly simple manner and without modifications to a stiffening structure, an aircraft door may be provided with very substantial stiffness in an edge region. |
| 申请公布号 |
US2015344122(A1) |
申请公布日期 |
2015.12.03 |
| 申请号 |
US201514722267 |
申请日期 |
2015.05.27 |
| 申请人 |
Airbus Operations GmbH |
发明人 |
Paul Carsten;Homann Holger |
| 分类号 |
B64C1/14;E06B7/23;E06B7/22 |
主分类号 |
B64C1/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft door, comprising:
an outer shell with an exterior and an interior; a stiffening structure arranged on the interior of the outer shell; and at least one door seal arranged on the interior of the outer shell, which door seal is circumferential in an edge region, wherein in the edge region between the outer shell and the door seal at least one circumferential stiffening component is arranged that is connected to the stiffening structure. |
| 地址 |
Hamburg DE |
