Ejection seats for military aircraft

Details Ejection seats for military aircraft Ejection seats for military aircraft

1991-04-01

1992-07-21

Basinger, Sherman

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244122AG, B64D 25115

Patent

active

051316080

ABSTRACT:
An ejection seat (1), supported on ejection gun guide rails (2) and moveable between an upright position to a reclining position thus affords the pilot greater protection from the effects of high "g" forces. Movement of the seat (1) is effected by hydraulic acutators (3), (4), guided by an arcuate track (15). The invention has the further advantage of allowing ejection from an upright or a reclining position or any intermediate transitional position.

REFERENCES:
patent: 2702677 (1955-02-01), Replogle
patent: 3098631 (1963-07-01), Hall et al.
patent: 3647168 (1972-03-01), Eggert, Jr. et al.
patent: 3981465 (1976-09-01), Sinnett et al.
patent: 4004763 (1977-01-01), Bunnell, III et al.
patent: 4218035 (1980-08-01), Jordan
patent: 4301983 (1981-11-01), Horan
patent: 4667901 (1987-05-01), Herndon
patent: 4749153 (1988-06-01), Herndon
patent: 4787576 (1988-11-01), McGrady et al.
European Search Report, Jul. 16, 1991, EP 91 10 4448.

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