CPC B64C 27/82 (2013.01) [B60L 53/00 (2019.02); B60L 58/12 (2019.02); B64C 27/32 (2013.01); B64C 29/0025 (2013.01); B64D 27/02 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B64D 31/10 (2013.01); B64D 31/12 (2013.01); B64D 33/02 (2013.01); B64D 35/02 (2013.01); B60L 2200/10 (2013.01); B64C 2027/8227 (2013.01); B64D 27/026 (2024.01); B64D 2033/0213 (2013.01)] | 20 Claims |
1. An air mobility vehicle comprising:
a vehicle body that includes a cabin;
an engine mounted in the vehicle body and configured to provide mechanical driving force or electric energy;
a battery configured to be charged with the electric energy from the engine;
main rotors configured to operate using the electric energy of the battery and electric power generated by the engine to perform takeoff, landing, and cruising;
auxiliary rotors disposed at or adjacent to a center of gravity of the vehicle body, each of the auxiliary rotors being rotatably coupled to the vehicle body and mechanically connected to the engine via a clutch, the auxiliary rotors configured to perform the takeoff, the landing, or the cruising by receiving the mechanical driving force from the engine when the clutch is in an engaged position;
a motor coupled to the auxiliary rotors and configured to rotate the auxiliary rotors between a first position and a second position; and
a controller configured to monitor states of the battery and the main rotors and to control operations of the engine and the clutch;
wherein each of the auxiliary rotors comprise an inlet; and
wherein the vehicle body comprises an air intake in a front portion thereof and the air intake is configured to supply air to the inlets of the auxiliary rotors located on both sides through an internal duct.
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