Adjustable safety seat for a vehicle such as an aircraft

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

296 681, 296 651, 297326, B64D 2504

Patent

active

057226172

ABSTRACT:
An adjustable seat of a vehicle such as an aircraft, comprises a fixed baseplate, the top plate of which is mounted on two lower components by two hinged joints. These hinged joints define two pins oriented parallel to the plane of the top plate, in the vehicle's transverse and longitudinal directions respectively. Moreover, one of these hinged joints is placed at the apex of a triangle, the opposite side of which is coincident with the pin of the other hinged joint. The integrity of the bed of the seat is thereby preserved in the event of twisting of the floor.

REFERENCES:
patent: 1362041 (1920-12-01), Roe
patent: 2587679 (1952-03-01), Atkinson
patent: 3489250 (1970-01-01), Kuhlmann
patent: 3741511 (1973-06-01), Streeter
patent: 4095770 (1978-06-01), Long
patent: 4408744 (1983-10-01), Thompson
patent: 4846529 (1989-07-01), Tulley
patent: 5054739 (1991-10-01), Wallin

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