发明名称 Landing gear foa rotorcraft and method for the dissipation of ground resonance oscillations
摘要 A linking system for attaching a cross tube to a skid of a landing gear of a rotorcraft, the linking system comprising a hinge element, means for connecting the hinge element to the cross tube and means for connecting the hinge element to the skid, the hinge element in turn comprising a cross tube-sided part and a skid-sided part able to rotate with respect to one another, a torsion bar spring and a rotary damper element suitable for dissipating a ground resonance excitation energy when the rotation of the cross tube-sided part with respect to the skid-sided part occurs.
申请公布号 EP2944567(A1) 申请公布日期 2015.11.18
申请号 EP20140400036 申请日期 2014.05.13
申请人 AIRBUS HELICOPTERS DEUTSCHLAND GMBH 发明人 OBERINGER, OLIVER
分类号 B64C25/52;B64C25/32;B64C25/62 主分类号 B64C25/52
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