Vertical seeking aircrew escape system

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244122A, B64D 2510

Patent

active

043032125

ABSTRACT:
An aircraft ejection seat which seeks the upward vertical direction to ene safe ejection from inverted aircraft at low altitude. An attitude control processor processes signals from three-axis attitude sensors and controls servo valves which regulate the flow of hydraulic fluid to hydraulic actuators connected to a spherical rocket motor mounted on a two axis gimbal system.

REFERENCES:
patent: 3216676 (1965-11-01), Brown et al.
patent: 3362662 (1968-01-01), McIntyre et al.
patent: 3592419 (1971-07-01), Hantzsch
patent: 3624367 (1971-11-01), Hamilton et al.
patent: 3870940 (1975-03-01), Espen
patent: 3979089 (1976-09-01), Miller et al.

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