| 摘要 |
The invention relates to a rotorcraft ( 21 ) comprising a fuselage ( 22 ) and an undercarriage ( 20 ) having skids ( 24, 25 ) interconnected by at least one cross-member ( 26, 27 ), together with connection means for connecting the cross-member to the fuselage and presenting angular stiffness that varies with varying sinking (E) of the undercarriage as a result of contact with the ground ( 23 ).
|
