An urban air mobility power supply system includes an urban air mobility (UAM) device and a power supply drone docked with the UAM device using electromagnetic force to supply external power, and a power supply method, in which the UAM device 200 and the power supply drone are accurately aligned with each other using electromagnets provided in the UAM device and the power supply drone to supply power, and the UAM device and the power supply drone can be easily separated from each other using electromagnetic force.

An urban air mobility power supply system includes an urban air mobility (UAM) device and a power supply drone docked with the UAM device using electromagnetic force to supply external power, and a power supply method, in which the UAM device 200 and the power supply drone are accurately aligned with each other using electromagnets provided in the UAM device and the power supply drone to supply power, and the UAM device and the power supply drone can be easily separated from each other using electromagnetic force.

A vertiport includes a main body, an elevating device configured to move up and down with respect to the main body, a take-off and landing portion disposed on an upper portion of the elevating device, wherein the take-off and landing portion is configured to operate to allow an aircraft equipped with a magnet unit in a lower portion of a fuselage to take off, land, and move, and a coil unit disposed in the take-off and landing portion and configured to interact electromagnetically with the magnet unit of the aircraft.

A vertiport includes a main body, an elevating device configured to move up and down with respect to the main body, a take-off and landing portion disposed on an upper portion of the elevating device, wherein the take-off and landing portion is configured to operate to allow an aircraft equipped with a magnet unit in a lower portion of a fuselage to take off, land, and move, and a coil unit disposed in the take-off and landing portion and configured to interact electromagnetically with the magnet unit of the aircraft.

A method for operating an unmanned aircraft of a motor vehicle charging station which has at least one charging point for a motor vehicle is disclosed, and may include projecting by a projector of an aircraft, at least temporarily, an image aimed at supporting a user of the motor vehicle onto a projection surface. An unmanned aircraft for a motor vehicle charging station and a motor vehicle charging station are further disclosed.

A method for operating an unmanned aircraft of a motor vehicle charging station which has at least one charging point for a motor vehicle is disclosed, and may include projecting by a projector of an aircraft, at least temporarily, an image aimed at supporting a user of the motor vehicle onto a projection surface. An unmanned aircraft for a motor vehicle charging station and a motor vehicle charging station are further disclosed.

Aspects of the present disclosure generally relate to systems and methods for the configuration and control of charging and cooling systems for aircrafts driven by electric propulsion systems and in other types of vehicles. In some embodiments, a method of charging an aircraft is disclosed comprising: receiving a mode of operation indicating whether battery packs of the aircraft are connected in parallel prior to joining a charging bus, receiving charging protocol information, and controlling charging operations of the battery packs based on the mode of operation and the charging protocol information.

Aspects of the present disclosure generally relate to systems and methods for the configuration and control of charging and cooling systems for aircrafts driven by electric propulsion systems and in other types of vehicles. In some embodiments, a method of charging an aircraft is disclosed comprising: receiving a mode of operation indicating whether battery packs of the aircraft are connected in parallel prior to joining a charging bus, receiving charging protocol information, and controlling charging operations of the battery packs based on the mode of operation and the charging protocol information.

An apparatus for facilitating the landing and takeoff of electric vertical takeoff and landing aircraft (EVTOL) can comprise a moveable landing platform, a moveable charging assembly comprising a high voltage cable adapted for electrical, magnetic induction positioned within a vertically moveable column having a magnetic plate and multiple access connections, and weight sensors positioned on the landing platform. The weight sensors are operatively connected to the charging assembly such that when the sensors detect the landing of an EVTOL on the platform, the sensors trigger the charging assembly to rise up to contact the EVTOL and begin charging the EVTOL.

An apparatus for facilitating the landing and takeoff of electric vertical takeoff and landing aircraft (EVTOL) can comprise a moveable landing platform, a moveable charging assembly comprising a high voltage cable adapted for electrical, magnetic induction positioned within a vertically moveable column having a magnetic plate and multiple access connections, and weight sensors positioned on the landing platform. The weight sensors are operatively connected to the charging assembly such that when the sensors detect the landing of an EVTOL on the platform, the sensors trigger the charging assembly to rise up to contact the EVTOL and begin charging the EVTOL.