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Landing gear foa rotorcraft and method for the dissipation of ground resonance oscillations
Landing gear foa rotorcraft and method for the dissipation of ground resonance oscillations
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机译:起落架foa旋翼飞机及用于消除地面共振的方法
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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.
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