| 摘要 |
<p>A steering device for a landing gear of an aircraft, including at least one actuator and at least one rack, located alongside the landing gear strut, outside and parallel to an upper tube of the landing gear. The steering device includes bevel pinions having a first conical pinion with an axis perpendicular to an axis of the landing gear strut and which meshes with a second conical pinion coaxial with a rotary annulus so that movement of the rack parallel to the strut is transferred to the annulus perpendicular to an axis of the landing gear through the bevel pinions having an axis perpendicular to the landing gear.</p> |
