| 摘要 |
<p>A device for damping the control stick of an aircraft, whose movements in pitch and roll, respectively, are transferred to a rotational shaft, with a damping means for damping its rotational movement is characterized primarily by a differential gear (1) with said shaft (2) as an inwardly extending shaft and with a 1:st and a 2:nd outwardly extending shaft (7, 10), respectively, standing in mechanical rotational connection with the 1:st and 2:nd damping elements respectively of the damping means in the form of short-circuited electric motors (9, 12).</p> |
