Command bar mechanism for flight director indicator

Details Command bar mechanism for flight director indicator Command bar mechanism for flight director indicator

1975-09-02

1976-11-02

Wood, Donald O.

Measuring and testing

Navigation

Take-off and landing monitors

116DIG43, G01C 2100

Patent

active

039889270

ABSTRACT:
A command driving mechanism for command bars which are rotatable about the longitudinal axis of and transversely displaceable with respect to the horizontal reference line of a flight director indicator includes a command plate, the plane of which is parallel to the front face of the indicator. The perpendicular axis of the command plate is coaxial with the longitudinal axis of the indicator and rotatable thereon in accordance with roll commands. Command bar struts are pivotally supported at diametrically opposed peripheral portions of the command plate and connected through a wire bail which is driven by a helical cam in accordance with pitch commands.

REFERENCES:
patent: 2613050 (1952-10-01), Esval
patent: 2696597 (1954-12-01), Chombard
patent: 3162834 (1964-12-01), Schweighoffer et al.
patent: 3691987 (1972-09-01), Strock

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