| 摘要 |
The landing gear for a Piper Cub ® light aircraft, comprises at least two wheels, is attached to a part of the fuselage in front of the centre of gravity, and has a fixed tubular reinforcement (1) that is generally triangular in shape, of which the apex (1a) is turned downwards, the ends (1b) and (1e) of the base of the reinforcement (1) and the apex (1a) of same being coupled, with articulation capability, to a suspension system linked to the wheels. Each end (1b) and (1e) of the base of the reinforcement (1) is angularly coupled to a wheel (R), by means of a damping member (2), while the apex (1a) of said reinforcement (1) is coupled symmetrically to each of the wheels, by means of a connecting rod (3). |
