| 发明名称 | Aircraft flap actuator assembly | ||
| 摘要 | An aircraft flap actuator assembly includes at least one fixed support, at least one track having a curvilinear track surface connected to the fixed support, at least one flap support adapted to traverse the curvilinear track surface, a trailing edge flap connected to the at least one flap support and a flap actuator engaging the at least one flap support. | ||
| 申请公布号 | US8763953(B2) | 申请公布日期 | 2014.07.01 |
| 申请号 | US201012835925 | 申请日期 | 2010.07.14 |
| 申请人 | The Boeing Company | 发明人 | Sakurai Seiya;Wheaton James M.;Fox Stephen J. |
| 分类号 | B64C9/00 | 主分类号 | B64C9/00 |
| 代理机构 | Parsons Behle & Latimer | 代理人 | Parsons Behle & Latimer |
| 主权项 | 1. An aircraft flap actuator assembly, comprising: at least one fixed support: at least one track having a curvilinear track surface fixedly connected to the fixed support; a floating beam, directly pivotally connected to the fixed support; a fore flap support adapted to traverse the curvilinear track surface; an aft flap support, pivotally connected to the floating beam and spaced-apart from the fore flap support; a trailing edge flap fixedly connected to the fore and aft flap supports; and a flap actuator connected to the fore flap support. | ||
| 地址 | Chicago IL US | ||