An air mobility vehicle comprising: a fixed wing; a plurality of booms; at least a battery, wherein the at least a battery is mounted in the fixed wing; a plurality of motors; a plurality of inverters; a plurality of rotary wings wherein each rotary wing is associated to a motor of the plurality of motors and to an inverter of the plurality of inverters, and wherein the rotary wings are mounted on the plurality of booms so that the motor and the inverter of each of the rotary wings is located inside a corresponding boom; a plurality of air flaps, wherein at least an air flap of the plurality of air flaps is located under a mounting position of each of the rotary wings and rotatably mounted inside at least an opening provided in the air mobility vehicle to guide a flow direction of air flowing to a region under each of the rotary wings or air flowing above the at least an opening to an inside of the air mobility vehicle, and wherein each of the at least an air flap is mounted on a boom of the plurality of booms; a plurality of actuators wherein each actuator is coupled to the at least an air flap and configured to rotate the at least an air flap to guide the air having passed through the at least an air flap to the motor, the inverter, or the motor and the inverter of each of the rotary wings, or the at least a battery, wherein each of the at least an air flap is rotated by operation of each coupled actuator to guide the air flowing to the region under each of the rotary wings to an inside of the boom or to an inside of the fixed wing via the inside of the boom; and a controller wherein each actuator of the plurality of actuators is electrically connected to the controller and the controller is configured to control a flow of the air having passed through the at least an air flap by controlling the actuator according to a driving state of the air mobility vehicle or temperatures of the motor, the inverter, or the motor and the inverter of each of the rotary wings or a temperature of the at least a battery; wherein, when the at least an air flap is rotated toward the rotary wings in a first direction, the air flowing to the region under each of the rotary wings passes through the at least an air flap and flows to the inside of the booms to cool the motor and the inverter; wherein when the at least an air flap is rotated in a second direction opposite to the first direction, the air flowing in the region in a front of the at least an air flap passes through the at least an air flap and flows to the inside of the fixed wing via the inside of the booms to cool the at least a battery. a fixed wing; a plurality of booms; at least a battery, wherein the at least a battery is mounted in the fixed wing; a plurality of motors; a plurality of inverters; a plurality of rotary wings wherein each rotary wing is associated to a motor of the plurality of motors and to an inverter of the plurality of inverters, and wherein the rotary wings are mounted on the plurality of booms so that the motor and the inverter of each of the rotary wings is located inside a corresponding boom; a plurality of air flaps, wherein at least an air flap of the plurality of air flaps is located under a mounting position of each of the rotary wings and rotatably mounted inside at least an opening provided in the air mobility vehicle to guide a flow direction of air flowing to a region under each of the rotary wings or air flowing above the at least an opening to an inside of the air mobility vehicle, and wherein each of the at least an air flap is mounted on a boom of the plurality of booms; a plurality of actuators wherein each actuator is coupled to the at least an air flap and configured to rotate the at least an air flap to guide the air having passed through the at least an air flap to the motor, the inverter, or the motor and the inverter of each of the rotary wings, or the at least a battery, wherein each of the at least an air flap is rotated by operation of each coupled actuator to guide the air flowing to the region under each of the rotary wings to an inside of the boom or to an inside of the fixed wing via the inside of the boom; and a controller wherein each actuator of the plurality of actuators is electrically connected to the controller and the controller is configured to control a flow of the air having passed through the at least an air flap by controlling the actuator according to a driving state of the air mobility vehicle or temperatures of the motor, the inverter, or the motor and the inverter of each of the rotary wings or a temperature of the at least a battery; wherein, when the at least an air flap is rotated toward the rotary wings in a first direction, the air flowing to the region under each of the rotary wings passes through the at least an air flap and flows to the inside of the booms to cool the motor and the inverter; wherein when the at least an air flap is rotated in a second direction opposite to the first direction, the air flowing in the region in a front of the at least an air flap passes through the at least an air flap and flows to the inside of the fixed wing via the inside of the booms to cool the at least a battery.