Hybrid air mobility vehicle

A hybrid air mobility vehicle comprising:

• an engine and a generator;
• a battery and a drive motor electrically connected to the generator;
• a first propeller connected to the drive motor and a second propeller connected to the generator through a clutch;
• and
• a controller configured to:
• control driving of the engine, the clutch, and the drive motor, based on a flight factor including at least one of a flight mode, a required power, a battery charging amount, or a surrounding flight environment of the hybrid air mobility vehicle,
• wherein the flight mode includes hovering, cruising and taxing, and the required power required during the hovering or the cruising is determined based on a flight speed of the hybrid air mobility vehicle, and
• wherein when the flight mode is transitioning from the hovering to the cruising and the controller determines to save the battery based on the battery charging amount, the controller is configured to:
• operate the first propeller by driving the drive motor with a power of the battery, and
• operate the second propeller with a power generated from the engine being engaged with the generator via the clutch.