Aircraft undercarriage

Aeronautics and astronautics – Landing gear – Retractable

Patent

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Details

B64C 2510

Patent

active

044338201

ABSTRACT:
The undercarriage comprises: a leg (1) pivotally mounted about a first pivot axis (14) which is fixed relative to a rigid structure of the aircraft; a main side-brace (30) comprising at least two articulated levers (31 and 32) having first ends pivotally connected to each other about a fourth pivot axis (33), having respective other ends pivotally mounted about a second pivot axis (37) which is fixed relative to the rigid structure, and pivotally mounted about a third pivot axis (36) which is fixed relative to the leg; and a drive (40 to 48) for causing the levers to pivot relative to each other. The first, second, third, and fourth pivot axes are parallel to each other.

REFERENCES:
patent: 2362016 (1944-11-01), McKinnie
patent: 2750134 (1956-06-01), Hawkins, Jr. et al.
patent: 2960287 (1960-11-01), Barlow
patent: 2974909 (1961-03-01), Perdue
patent: 3488020 (1970-01-01), Scherer
patent: 4312485 (1982-01-01), Masclef et al.

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