Stabilizer for an ejection seat

Details Stabilizer for an ejection seat Stabilizer for an ejection seat

1980-01-10

1982-03-16

Frankfort, Charles E.

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244141, B64D 2510

Patent

active

043197230

ABSTRACT:
A yaw stabilization system for an aircraft ejection seat having a vane for sensing the angular offset of the yaw air flow velocity vector and for extending paddles into the air stream in response to the velocity vector offset. The extended paddle is acted upon by the air stream to provide a restoring moment around the center of gravity of the seat and occupant to return the seat to the desired attitude with respect to the air flow velocity vector.

REFERENCES:
patent: 1087993 (1914-02-01), Sprater
patent: 2829850 (1958-04-01), Culver
patent: 2931598 (1960-04-01), Sanctuary
patent: 3042347 (1962-07-01), Halsey

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