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...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
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. |
---|