| 摘要 |
The invention relates to landing gear of an aircraft, the landing gear having skids and cross-members. The landing gear has at least one damper device arranged on at least one of the cross-members referred to as a “damped” cross-member. The damper device includes two stroke-transfer means hinged to the damped cross-member and to a fuselage of the aircraft. Each stroke-transfer means comprises a crank hinged to the damped cross-member and a link rod hinged to the crank and to the fuselage. A damper is hinged to each crank. |
