A rotorcraft includes a main rotor system coupled to a mast and a rotor assembly. The rotor assembly includes a yoke comprising a rotor coupling, a first damper mount attached to the rotor coupling, a rotor extension configured to couple to the rotor coupling and comprising a second damper mount, a damper coupled to the first and second damper mounts, and a fairing enclosing the damper and the yoke.
LOW-DRAG FAIRING AND ROTOR ASSEMBLY
2020-12-24
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |