Method and device for monitoring a servo-valve actuation system

A method for monitoring a variable-geometry actuation system (1) of a turbojet engine is disclosed. Said actuation system comprises a control device (2), a servo-valve (3), an a cylinder (4) that is controlled by the servo-valve (2), the control device being able to determine a control current (Icmd...

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Bibliographische Detailangaben
Hauptverfasser: GODEL FRANCK, GUEIT NICOLAS MARIE PIERRE, PONTALLIER BENOIT
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:A method for monitoring a variable-geometry actuation system (1) of a turbojet engine is disclosed. Said actuation system comprises a control device (2), a servo-valve (3), an a cylinder (4) that is controlled by the servo-valve (2), the control device being able to determine a control current (Icmd) according to a set position (Pos_c) and a measured position (Pos_m) of the cylinder (4) and feed said control current (Icmd) to the servo-valve (3). The monitoring method is characterized in that it includes: a step of detecting a stabilized state; a step of determining an average value of the control current during the detection of the stabilized state; and a step of comparing said average value with a predetermined threshold value.