| 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 | US9511852(B2) | 申请公布日期 | 2016.12.06 |
| 申请号 | US201214238534 | 申请日期 | 2012.09.07 |
| 申请人 | MESSIER-BUGATTI-DOWTY | 发明人 | Blanpain Thierry;Ducos Dominique;Campbell Edouard |
| 分类号 | B64C25/20;B64C25/26;B64C25/62;B64C25/58 | 主分类号 | B64C25/20 |
| 代理机构 | Sughrue Mion, PLLC | 代理人 | Sughrue Mion, PLLC |
| 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 for defining at least one working position wherein the lever contacts said abutment means when the actuator is actuated. | ||
| 地址 | Velizy Villacoublay FR | ||