A vibration control actuator includes a housing having a length between ends and a rotatable shaft located in the housing and extending along a housing length and which rotates about a shaft axis substantially parallel to the length. An inertia wheel assembly is operably connected to the rotatable shaft and configured to rotate therewith about the shaft axis. The inertia wheel assembly is in frictional contact with an inner wall of the housing and translatable to travel within the housing between the ends along at least a portion of the shaft axis.
ACTIVE VIBRATION CONTROL ACTUATOR
AKTUATOR FÜR AKTIVE SCHWINGUNGSSTEUERUNG
ACTIONNEUR ACTIF DE RÉGULATION DE VIBRATIONS
05.12.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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