Landing gear for aircraft

Aeronautics and astronautics – Landing gear – Retractable

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B64C 2514

Patent

active

044226039

ABSTRACT:
The present invention relates to landing gears retractable between two positions.
The landing gear includes essentially a lever (14 ) mounted rotatably around an axis (5), a rocker beam (7) mounted rotatably on the same axis (5), a strut (21) including two links (22,23) pivoting in relation to each other, the strut being connected to the lever, a shock absorber (18) fixed respectively on the lever (14) and the rocker beam (7), and an actuating cylinder (32) for applying a pivoting force to the lever (14). This landing gear finds a particularly advantageous application in aircraft of the commuter type.

REFERENCES:
patent: 2471603 (1949-05-01), Bishop
patent: 2497489 (1950-02-01), Coursen et al.
patent: 2659555 (1953-11-01), Schlender
patent: 3899147 (1975-08-01), Masclet et al.
patent: 3904153 (1975-09-01), Watts

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