| 摘要 |
<p>PROBLEM TO BE SOLVED: To provide a parallel hybrid multi-rotor aircraft with an electric motor and an engine, which can increase continuous flight time while maintaining advantages of structural simplicity and high attitude controllability.SOLUTION: The parallel hybrid multi-rotor aircraft is constituted of: an engine 2; fuel supplied to the engine; propellers 3 that are connected to an output shaft of the engine and generates thrust; a power generator 4 that is connected to the output shaft of the engine and generates power; at least three electric motors to be operated by the power generated by the power generator; at least three propellers that are connected to the output shafts of the electric motors and generate thrust; and a battery that absorbs a difference between power required by the electric motors and power generated by the power generator.</p> |
