An aircraft is provided and includes an airframe, an engine, a drive portion driven by the engine, a rotor apparatus, which includes a rotor rotatable relative to the airframe and a fairing, a gearbox disposed to transmit rotational energy from the drive portion to the rotor to drive the rotor to rotate relative to the airframe and which generates a rotor rotation vibration, support members by which the gearbox is disposed on the airframe and an actuation system including actuation elements disposed at the fairing, the actuation system being configured to generate an anti-vibration moment using the actuation elements disposed at the fairing to counter the rotor rotation vibration.
ANTI-VIBRATION MOMENT GENERATING AIRCRAFT ACTUATION SYSTEM
SCHWINGUNGSDÄMPFENDES, MOMENTERZEUGENDES FLUGZEUGBETÄTIGUNGSSYSTEM
SYSTÈME D'ACTIONNEMENT D'AÉRONEF PRODUISANT UN MOMENT ANTI-VIBRATIONS
2019-06-26
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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