| 摘要 |
<p>Actuator (29) for an aircraft turbine engine nacelle with a notably one-piece annular rear part, comprising: - an engine assembly comprising a nut which is capable of rotating but not of translational movement, and means for turning this nut, and - a screw assembly (37) comprising a screw (39) capable of translational movement without rotating, in mesh with said nut and a ball joint (43) at one end of this screw (39) intended to be fixed to said element.</p> |
