| 摘要 |
<p>The invention relates to a landing gear of an aircraft, comprising two walking beams (1, 2) carrying wheels and mounted in such a way as to pivot on a common pivot (Y1), the landing gear comprising a damping device having two rods (5, 6) respectively coupled to one of the walking beams, at least one of the rods being telescopic and forming a damper, the two rods also being coupled to a rocker (7) mounted pivotably on a central pivot (8). According to the invention, the common pivot of the walking beams is secured to the structure of the aircraft and mounted thereon in a fixed manner, whereas the central pivot of the rocker is mobile between a first position wherein the walking beams are in the landing position, and a second position wherein the rocker has pulled on the rods in order to pivot the walking beams towards a retracted position.</p> |
