The invention provides a multi-rotor type aircraft. The multi-rotor type aircraft comprises a main rotor and a plurality of secondary rotors, wherein the main rotor is driven by a fuel engine, and is arranged at the lower end or the upper end of the center position of the engine body of the fuel engine; the plurality of secondary rotors are distributed on the periphery of the engine body; the secondary rotors are driven by motors respectively. The multi-rotor aircraft has the advantages of high carrying capacity and long voyage time.
Multi-rotor type aircraft
2015-07-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |