“A tilting apparatus for an aircraft, comprising: a tiltable aircraft component which tilts between a first and second position, at least one actuator for adjusting a tilt angle of the tiltable aircraft component, and at least one passive damper connected to the tiltable aircraft component and configured to limit a rate of change of the tilt angle of the tiltable aircraft component. The at least one passive damper is on a load path separate from a load path of the at least one actuator.”
REDUNDANT LOAD PATH FOR POWERED LIFT TILT ACTUATOR
REDUNDANTER LASTWEG FÜR EINEN ANGETRIEBENEN HUBKIPPAKTUATOR
TRAJET DE CHARGE REDONDANT POUR ACTIONNEUR D'INCLINAISON DE LEVAGE MOTORISÉ
28.05.2025
Patent
Elektronische Ressource
Englisch
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