Multi-rotor fuel-electric hybrid aircraft
A technology for multi-rotor aircraft and aircraft, applied in the field of aircraft, can solve the problems of battery bottleneck, short flight time, difficulty in manned flight, etc., and achieve the effect of high thrust and long battery life
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[0019] Reference figure 1 , The first embodiment of the present invention is proposed, a multi-rotor hybrid aircraft, including an electronic governor 1, a flight control system 2, a fuselage 3 composed of multiple shafts, and multiple propellers. The first propeller 4 driven by the fuel engine and the second propeller 5 driven by an electric motor, the distance between the adjacent first propeller 4 and the second propeller 5 on the same shaft is 60cm-80cm, the fuselage 3 The shafts of the four first propellers 4 are connected in a "meter" shape. The four first propellers 4 are arranged symmetrically on each shaft with the center of the fuselage as the center point, and the distance from the center point is equal. The center of the body is the center point and is arranged symmetrically at the outer end of each machine shaft and the distance from the center point is equal.
Example Embodiment
[0020] Reference figure 2 , The second embodiment of the present invention is proposed, a multi-rotor hybrid aircraft, including an electronic governor 1, a flight control system 2, a fuselage 3 composed of multiple shafts, and multiple propellers. The first propeller 4 driven by the fuel engine and the second propeller 5 driven by an electric motor, the distance between the adjacent first propeller 4 and the second propeller 5 on the same shaft is 60cm-80cm, the fuselage 3 The shafts of the four first propellers 4 are connected in the shape of a "cross". The four first propellers 4 are evenly arranged on each shaft symmetrically with the center of the fuselage as the center point, and the distance from the center point is equal. The center is the center point and is evenly arranged in pairs on each machine shaft and the distance from the center point is equal.
[0021] The fuselage 3 of the present invention is made of 7075 aviation aluminum.
[0022] The above embodiment adopt...
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