The invention relates to a protective cover of a multi-rotor aircraft. The protective cover is installed on a central disc of an aircraft. The protective cover comprises a cover body with an arc-shaped cross section. The bottom surface of the cover body is equipped with flanges. A main control system in the central disc is prevented from contact with water, a protection function is achieved, and the service life of the aircraft is prolonged.
Protective cover of multi-rotor aircraft
16.09.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |