Landing gear for aircraft

Aeronautics and astronautics – Landing gear

Patent

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Details

244 50, 244104FP, 18832111, B64C 2558

Patent

active

043961703

ABSTRACT:
The invention concerns a landing gear. The landing gear is characterized essentially by the fact that it comprises at least one shock absorber (15), this shock absorber being mounted in the leg (1) and casing (2) assembly by means of two convex surfaces (22, 31) made on the cylinder (16) of the shock absorber (15) and cooperating with two concave surfaces (25, 32) integral respectively with the leg (1) and the casing (2). This landing gear finds an application as a nose gear of the rocker-beam type.

REFERENCES:
patent: 2279447 (1942-04-01), Cowey
patent: 2468939 (1949-05-01), Mercier
patent: 2747817 (1956-05-01), Saulivier

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