| 发明名称 |
SELF-ADJUSTING DOOR JAMB FOR AN AIRCRAFT DOOR |
| 摘要 |
The disclosed embodiments relate to an aircraft having an interior door with a self-adjusting door jamb. The self-adjusting door jamb includes a door jamb configured to receive the interior door and a bias mechanism coupled to the door jamb and facilitating movement of the door jamb along an axis. Additionally, an angular translating mechanism coupled to the bias mechanism and facilitating angular displacement of the door jamb relative to the axis. |
| 申请公布号 |
US2017008608(A1) |
申请公布日期 |
2017.01.12 |
| 申请号 |
US201514792231 |
申请日期 |
2015.07.06 |
| 申请人 |
Gulfstream Aerospace Corporation |
发明人 |
Telmos Robert J. |
| 分类号 |
B64C1/14;B64C1/10 |
主分类号 |
B64C1/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A self-adjusting door jamb for an interior door of an aircraft, comprising:
a door jamb configured to receive the interior door; a bias mechanism coupled to the door jamb and facilitating movement of the door jamb along an axis; and an angular translating mechanism coupled to the door jamb and facilitating angular displacement of the door jamb relative to the axis. |
| 地址 |
Savannah GA US |
