| 摘要 |
<p>The invention relates to a means for rotating the strut (1) of the landing gear of an aircraft about a retraction axis (2), such as an actuator (12a, 12b) comprising a first end that can be fixed to the structure of the aircraft and a second end forming an actuating point that can be fixed to the gear, characterised in that it comprises a first mobile set (121a, 121b) defining a first elongation of the actuating point and a second mobile set (122a, 122b) defining a second elongation of the actuating point, the two mobile sets (121a and122a, 121b and 122b) being positioned in each other's axis and acting in series in order to define the total elongation of the actuating point.</p> |
