The control device (10) has a rotational drive and a linear control movement, which has load transmitting components for transferring a force or a torque, where a part of the load transmitting components is redundant. A load path is formed by a set of load-bearing components, where the rotational drive is comprised of a rotational portion of a gear, which is part of the load path. Another load path is formed by another set of load-bearing components. A monitoring unit with an actively actuated brake unit is provided for error detection, particularly for detecting functional disorders. An independent claim is provided for a method for detecting faults in a control device for an aircraft.
DISPOSITIF DE REGLAGE, EN PARTICULIER DISPOSITIF DE REGLAGE POUR UN AERONEF
2017-10-13
Patent
Electronic Resource
French
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