| 发明名称 |
ACTUATORS FOR FLIGHT CONTROL SURFACES |
| 摘要 |
An actuator assembly includes an actuator body, a ram, and a cross pin. The actuator body has an internal axial cavity bounded by an actuator body wall and defines a pivot axis. A longitudinal slot extends along a portion of the length of the actuator body wall and is in communication with the internal axial cavity. The ram is slidably received within the axial cavity of the actuator body. The cross pin is mounted to the ram and extends laterally from the ram and into the longitudinal slot for converting linear motion of the ram into rotational motion about the pivot axis for displacing a control surface of an air vehicle. |
| 申请公布号 |
US2015353186(A1) |
申请公布日期 |
2015.12.10 |
| 申请号 |
US201414228004 |
申请日期 |
2014.03.27 |
| 申请人 |
Simmonds Precision Products, Inc. |
发明人 |
Buttolph Martin E. |
| 分类号 |
B64C9/00;B64C13/28 |
主分类号 |
B64C9/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An actuator assembly, comprising:
an actuator body with an internal axial cavity bounded by an actuator body wall and a longitudinal slot communicating through the actuator body wall and into the cavity; a ram slidably received within the axial cavity; and a cross pin mounted to the ram and extending laterally from the ram and into the longitudinal slot, wherein the actuator body defines a pivot axis and the cross pin and longitudinal slot are configured to convert linear motion of the ram into rotational motion about the pivot axis for displacing a control surface of an air vehicle. |
| 地址 |
Vergennes VT US |
