The present invention includes an apparatus and method for automatically adjusting the tracking of one or more blades comprising: a blade tracking adjustment mechanism (400) connected to one or more blades (404) of an aircraft; a blade tracking measurement system (406) that measures the tracking of the one or more blades; and a computer (410) that receives an output from the blade tracking measurement system with tracking information for each of the one or more blades; wherein the computer outputs instructions for the blade tracking adjustment mechanism to change a pitch of one or more of the blades to correct blade tracking.
AUTOMATIC, ACTIVE ROTOR BLADE TRACKING AND BALANCE SYSTEM
SYSTEM ZUR AUTOMATISCHE, AKTIVEN ROTORBLATTVERFOLGUNG UND -AUSWUCHTUNG
SYSTÈME D'ÉQUILIBRAGE ET DE SUIVI ACTIF AUTOMATIQUE D'UNE PALE DE ROTOR
2020-11-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Blade Integration of a Modular Active Trim Tab System for Onboard Rotor Tracking
British Library Conference Proceedings | 2011
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