Apparatus for adjustably mounting an ejection seat in an aircraf

Details Apparatus for adjustably mounting an ejection seat in an aircraf Apparatus for adjustably mounting an ejection seat in an aircraf

1984-09-27

1987-05-26

Blix, Trygve M.

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244122A, 297346, B64D 2510

Patent

active

046679014

ABSTRACT:
Apparatus for adjustably mounting an ejection seat (16) in an aircraft in which outer catapult cylinders (58, 60) support inner catapult cylinders (62, 64) and supply force to the inner cylinders to eject the inner cylinders and the seat from the aircraft, the inner cylinders being connected to an upper rear end of the seat (66, 68). The seat (16) is supported in the aircraft by the inner and outer catapult cylinders (62, 64, 58, 60), by adjusting actuators (40) to raise and lower and to tilt the seat forwardly and rearwardly, by lower anchor links (30) pivotally connected to the aircraft and to lower end (26, 28) of the outer catapult cylinders and to the actuators (40), and by upper links (50). The seat is connected to the catapult cylinders (58, 60) by slipper blocks 82. The slipper blocks (82) are pivotally connected to the seat by pins (84) and are slidably engaged with the outer catapult cylinders.

REFERENCES:
patent: 2148953 (1939-02-01), Meissner
patent: 2702677 (1955-02-01), Replogle
patent: 2726831 (1955-12-01), Bleck et al.
patent: 2836222 (1958-05-01), Martin
patent: 3098631 (1963-07-01), Hall et al.
patent: 3826434 (1974-07-01), Von Beckh
patent: 4128217 (1978-12-01), Mazelsky
patent: 4408738 (1983-10-01), Mazelsky
patent: 4423848 (1984-01-01), Mazelsky

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