Yaw stabilization for aircraft ejection seats

Details Yaw stabilization for aircraft ejection seats Yaw stabilization for aircraft ejection seats

1983-05-31

1984-09-11

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244141, B64D 2510

Patent

active

044705654

ABSTRACT:
An aircraft ejection seat is provided with deployable fins for stabilizing aw rotation. The fins are normally stowed along the sides of the ejection seat. During ejection, the fins are deployed aft of the seat by means of rotational actuators. Anti-entanglement sheets are collapsibly disposed between the fins and the sides of the seat in order to prevent fouling of the parachute.

REFERENCES:
patent: 2931598 (1960-04-01), Sanctuary
patent: 3027124 (1962-03-01), Statt
patent: 3662978 (1972-05-01), Hollrock
patent: 3679157 (1972-07-01), Roberts
patent: 3826448 (1974-07-01), Burk
patent: 4017041 (1977-04-01), Nelson
patent: 4017043 (1977-04-01), Barzda
patent: 4261535 (1981-04-01), Swanson
patent: 4303212 (1981-12-01), Stone et al.

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