An actuator monitoring circuit (1) which is mounted in an airplane and monitors an actuator (30) having a piston (output portion) calculates the moving distance of the piston, and outputs, when the moving distance exceeds a predetermined threshold, an approaching notification signal (78s) and a progression notification signal (79s) to notify the excess over the threshold.
SET OF ACTUATOR UNITS THAT DRIVE A CONTROL SURFACE OF AN AIRPLANE
GRUPPE VON ANTRIEBSEINHEITEN, DIE EINE STEUERFLÄCHE EINES FLUGZEUGS STEUERN
ENSEMBLE D'UNITÉS D'ACTIONNEMENT QUI ENTRAÎNENT UNE SURFACE DE CONTRÔLE D'UN AVION
2022-08-17
Patent
Elektronische Ressource
Englisch
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