Variable attitude aircraft crew station

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

B64C 114, B64C 128

Patent

active

041834798

ABSTRACT:
A crew station module that retracts or lowers itself during supersonic cruise flight to provide a small protuberance with adequate pilot vision over the nose and side which module extends or raises itself at takeoff and landing to provide increased downward vision over the nose and sides which module is adaptable for high acceleration cockpit seating i.e. seating that will be adjustable for accommodating variable G-loading upon the occupant such as during combat maneuvers and so forth.

REFERENCES:
patent: 2142997 (1939-01-01), Case
patent: 2701899 (1955-02-01), Krupp
patent: 2868477 (1959-01-01), Chaplin
patent: 3433439 (1969-03-01), Brame et al.

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