Undercarriage apparatus for vertical-lift aircraft

Aeronautics and astronautics – Landing gear

Patent

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Details

244103R, 244 1717, 244104R, B64C 2536

Patent

active

048528293

ABSTRACT:
Axial motion of the wheel assembly of a flat-spring undercarriage for vertical-lift aircraft is provided to permit proper deflection of the flat spring so as to effectively cushion the touchdown of such an aircraft from a hover.

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