Leg for an aircraft seat, a leg assembly including such a leg, a

Chairs and seats – Crash seat – Bottom and back movable as unit in response to force

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2972161, B60N 242

Patent

active

057435928

ABSTRACT:
A leg for the leg assembly of an aircraft seat presents over at least a portion of its length, at least one segment whose cross-section has at least a portion that is generally U-shaped defined by a web extending in a transverse direction and two flanges extending in a longitudinal direction, the opening of the U-shape facing in a longitudinal direction, said segment serving to contribute to absorbing energy.

REFERENCES:
patent: 4440441 (1984-04-01), Marrujo et al.
patent: 4861103 (1989-08-01), Vallee
patent: 4911381 (1990-03-01), Cannon et al.
patent: 5069505 (1991-12-01), Amthor et al.
patent: 5152578 (1992-10-01), Kiguchi
patent: 5499783 (1996-03-01), Marechal

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