Aircraft undercarriage of tilting-beam type and of reduced bulk

Details Aircraft undercarriage of tilting-beam type and of reduced bulk Aircraft undercarriage of tilting-beam type and of reduced bulk

1987-04-29

1988-06-07

Barefoot, Galen

Aeronautics and astronautics

Landing gear

Wheel

18832111, 267 6426, B64C 2522

Patent

active

047491523

ABSTRACT:
The present invention is concerned with tilting-beam undercarriages.
The undercarriage is characterized in that the shock absorber means (7) comprise a hollow cylinder (11) entered by a plunger stem (14) at its first end (12) and by a piston (18) at its second end, while the hollow cylinder (11) has a hinge member (22) onto which the beam (8) is hinged at a point C differing from the center of it and the piston (18) is connected to the beam at a point D differing from the point of hinge C.

REFERENCES:
patent: 2670160 (1954-02-01), Neilson
patent: 2967682 (1961-01-01), Fullam et al.
patent: 3056598 (1962-10-01), Conway et al.
patent: 3653682 (1972-04-01), Palmer et al.
patent: 4396170 (1983-08-01), Turiot et al.

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