An aircraft includes a first rotor assembly, a second rotor assembly, and a rotor phase angle control system. The system includes a phase adjustor operably associated with the first rotor assembly and the second rotor assembly. The method includes sensing vibrations exerted on the aircraft and offsetting a phase angle of the first rotor assembly and the second rotor assembly to minimize the vibrations.
VARIABLE HUB-TO-HUB PHASING ROTOR SYSTEM
06.08.2015
Patent
Elektronische Ressource
Englisch