| 摘要 |
<p>The invention relates to an actuator for hingedly connecting a first element to a second element about a first pivoting axis (A1), comprising a motorisation device, a first plate (4) for linking to a frame (2) of the motorisation device, a second plate (5) for linking to the second element, the second plate being mounted in the first plate so as to pivot about the first axis, and a bearing (6) mounted in the second plate such as to pivot about a second axis (A2) perpendicular to the first axis. The motorisation device has an output shaft (3) pivoting about a third axis (A3) perpendicular to the first axis and secant with the first axis, and is extended by a crank pin (7) which is pivotably received in the bearing and which has a central axis (A4) secant with the first axis and the third axis, forming an acute angle with the third axis. The invention also relates to an aircraft guidance assembly including such an actuator.</p> |
