| 摘要 |
<p>The invention concerns a device and a method to cause the rotation of at least one wheel of the landing gear of air¬craft, according to which between the supporting structure (12) of the landing gear and the brake group (19, 20) of the wheel is placed at least an actuator element with variable geometry (35, 38, 40, 42) controlled and managed to develop such a force in or¬der impose an intermittent angular rotation of the wheel when the brake group is operated.</p> |
