Pilot seat with lateral vibration isolation

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

248358A, 297216, B64D 2504

Patent

active

040035344

ABSTRACT:
An adjustable crashworthy pilot seat adapted to be used in aircraft such as helicopters is supported from the floor thereof within a support frame such that the normal lateral vibrations of the aircraft are not imparted to the pilot and so that the seat retains its crashworthy and adjustment capabilities.

REFERENCES:
patent: 2301903 (1942-11-01), Flader

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