| 发明名称 |
DEVICE FOR COUPLING AN ACTUATOR FOR CONTROLLING THE LANDING GEAR OF AN AIRCRAFT |
| 摘要 |
A device for coupling an actuator for operating an aircraft undercarriage to an aircraft structure. The device comprises a lever having a first end for hinging to the structure of the aircraft, and a second end to which the actuator is hinged, a pre-loading structure acting on the lever to urge it towards a stable rest position that is occupied by the lever in the absence of any force transiting through the actuator; and an abutment structure defining at least one working position for the lever when the actuator is activated. |
| 申请公布号 |
US2014209738(A1) |
申请公布日期 |
2014.07.31 |
| 申请号 |
US201214238534 |
申请日期 |
2012.09.07 |
| 申请人 |
Blanpain Thierry;Ducos Dominique;Campbell Edouard |
发明人 |
Blanpain Thierry;Ducos Dominique;Campbell Edouard |
| 分类号 |
B64C25/20 |
主分类号 |
B64C25/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A device for coupling an actuator for operating an aircraft undercarriage to an aircraft structure, the device comprising:
a lever having a first end for hinging to the structure of the aircraft, and a second end to which the actuator is hinged; pre-loading means acting on the lever to urge it towards a stable rest position that is occupied by the lever in the absence of any force transiting through the actuator; and abutment means pour defining at least one working position for the lever when the actuator is activated. |
| 地址 |
Velizy Villacoublay FR |
