Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1979-04-26
1981-12-01
Miller, J. D.
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
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.
Stone W. James
Stoutmeyer Ronald G.
Eisenzopf Reinhard J.
Miller J. D.
Pritchard Kenneth G.
Sciascia R. S.
Skeer W. Thom
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