Aircraft ejected seat stabilizing and delayed parachute system

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244141, B64D 2510

Patent

active

047655704

ABSTRACT:
A system and method for stabilizing an aircraft ejection seat and crew member after seat ejection and prior to main parachute inflation. The system also providing for delayed opening of the main chute until air speed and altitude have decreased to an acceptable parachute inflation range.

REFERENCES:
patent: 2610815 (1952-09-01), Smith
patent: 3436037 (1969-04-01), Stanley
patent: 3603536 (1971-09-01), Dochow
patent: 4004764 (1977-01-01), Burklund et al.
patent: 4175722 (1979-11-01), Higgins

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