Differential linkage apparatus for an aircraft series servoactua

Electricity: motive power systems – Positional servo systems – 'feelback' systems

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Details

318580, 318584, 318586, 318626, 244223, G05B 1101

Patent

active

044266073

ABSTRACT:
In a servoactuator system for an aircraft, a strapdown series servoactuator having an external linkage assembly is coupled between the pilot's control stick and a control surface member. The external linkage assembly includes a differential link and servo link having specially tapered stop surfaces adapted to be varied in dimensions to accommodate a wide variety of installations, which stop surfaces cooperate with fixed stops on the servoactuator housing whereby to provide a variety of pilot authority limits and series servo authority limits depending upon particular installation requirements.

REFERENCES:
patent: 3369161 (1968-02-01), Kaufman
patent: 3733039 (1973-05-01), O'Conner et al.
patent: 4228386 (1980-10-01), Griffith
patent: 4313165 (1982-01-01), Clelford et al.

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