In-line actuator monitoring and control apparatus

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

91363A, 318564, G05D 100

Patent

active

041204697

ABSTRACT:
An in-line actuator monitoring apparatus utilized in a redundant actuator system for determining which of the two redundant secondary actuators in a flight control system has failed and providing a disable signal to the failed actuator unit.

REFERENCES:
patent: 3438306 (1969-04-01), Kazmarek
patent: 3505929 (1970-04-01), Coppola
patent: 3509435 (1970-04-01), Howells
patent: 3741073 (1973-06-01), Garnjost

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