The invention relates to a multi-rotor-wing oil-
electricity hybrid power aircraft. The multi-rotor-wing oil-
electricity hybrid power aircraft is characterized in that the aircraft comprises a rotor wing
assembly, an aircraft body support, an engine, a driving motor, a control box, a battery box, an
oil tank and an undercarriage; and the rotor wing
assembly is vertically distributed and mounted at the two ends of the aircraft body support in the directions of rotor wing rotary shafts, the control box, the battery box and the
oil tank are mounted on the aircraft body support, and the undercarriage is connected and mounted below the aircraft body support. Compared with a traditional oil drive multi-rotor-wing helicopter, in an oil drive multi-rotor-wing helicopter, a rotor wing orientation adjustment structure is omitted, so that the multi-rotor-wing oil-
electricity hybrid power aircraft is greatly simplified in structure, convenient to maintain, low in
failure rate and low in manufacturing cost; the multi-rotor-wing oil-electricity
hybrid power aircraft is easy to achieve, the adjusting mode is simple in advancing, the structure is simple and reasonable, and components are easy to obtain; and a
hybrid power aircraft driving
system of the multi-rotor-wing oil-electricity
hybrid power aircraft can achieve the remote navigation effect and the large
load capacity and is applicable to serving as a driving
system of the multi-rotor-wing helicopter.