A landing pad for an unmanned aerial vehicle (UAV) is disclosed. The landing pad includes a support structure, a charging pad, and a plurality of movable UAV supports. The charging pad is coupled to the support structure and able to move relative to the support structure. The UAV supports are also coupled to the support structure and configured to translate along the support structure from a first position to a second position. When the UAV supports are in the first position, the charging pad supports the UAV. When the UAV supports are in the second position, the charging pad is lowered and the UAV supports then provide support to the UAV.

An unmanned aerial vehicle station includes a takeoff-landing unit for an unmanned aerial vehicle to take off and land, a parcel receiver, a parcel deliverer, a storage that stores a plurality of parcels, a replenishment hangar that houses a plurality of unmanned aerial vehicles and replenishes the housed plurality of unmanned aerial vehicles with energy, a parcel transporter that transports the plurality of parcels between the parcel receiver and the storage and between the parcel deliverer and the storage, and an aircraft transporter that transports the plurality of unmanned aerial vehicles between the takeoff-landing unit and the replenishment hangar.

A rotorcraft capable of a hover mode and a forward cruise mode including a fuselage, a first electric propulsion system, a second electric propulsion system, and an electric power control unit to control power to the first and second electric propulsion systems in the hover and forward cruise modes. The first electric propulsion system is a tip jet cold flow system that imparts rotation on a pair of rotor blades disposed above a top surface of the fuselage, and a first electric motor configured to drive the tip jet cold flow system. The second electric propulsion system includes a propeller disposed in the rear of the fuselage and a second electric motor configured to drive the propeller.

A detachable power transfer device for a rotary-wing aircraft includes a docking station integrated into the rotary-wing aircraft. A power pod of the detachable power transfer device is constructed and arranged to detachably connect to the docking station for transferring power to the rotary-wing aircraft.

Methods, devices, and systems of various embodiments are disclosed for managing a vehicle charging station having a docking terminal. In various embodiments, a priority of a first autonomous vehicle and a second autonomous vehicle may be determined for using the docking terminal when a docking request is received from the second autonomous vehicle while the first autonomous vehicle occupies the docking terminal. In some embodiments, the priorities of the first and second autonomous vehicles may be based on an available power level of each of the first and second autonomous vehicles. The first autonomous vehicle may be instructed to undock from the docking terminal in response to determining that the second autonomous vehicle has a higher priority.

A charging system may comprise: a first battery array; a bi-directional direct current (DC)/DC converter in electrical communication with the first battery array; and a charging interface in electrical communication with the bi-directional DC/DC converter, the charging interface configured to electrically couple to a second battery array of an electric vehicle.

A charging ecosystem may comprise: an interconnected battery module; a first battery system comprising a first plurality of the interconnected battery modules; and a second battery system comprising a second plurality of the interconnected battery module. The first battery system may be configured for charging the second battery system. The second battery system may be configured for powering an electric vehicle. The interconnected battery module is adaptable to various interfaces with the first system and the second system.

A mobility vehicle transfer platform includes an elevation passage provided in a structure provided with a take-off and landing site for an air mobility vehicle and having an internal space extending in the vertical direction to be connected to the take-off and landing site and to allow a ground mobility vehicle to be elevated or lowered through the internal space to be connected to or separated from the air mobility vehicle, and an elevation unit provided in the internal space of the elevation passage, having an elevation portion selectively connected to the ground mobility vehicle and configured for elevating or lowering the ground mobility vehicle in the elevation passage when the ground mobility vehicle is connected to the elevation portion.

An electric vehicle charging connector including a charging connector. The charging connector including a direct current pin and an alternating current pin. The electric vehicle charging connector also including a coupling mechanism configured to: couple the charging connector to an electric vehicle, enable a flow of electricity from the charging connector to the electric vehicle, and disable the flow of electricity from the charging connector to the electric vehicle.

An air start unit for starting and servicing jet engines in aircraft and other flying machines, wherein at least one compressor is provided for generating air and a power supply for supplying electrical power consumers. The air start unit drives the compressor with at least one electric motor, with the electric motor drawing the electrical energy for operation from a high-voltage battery. The electric motors then in turn drive the compressor, which generates compressed air from ambient air for the purpose of starting and servicing the jet engines in aircraft and other flying machines. With an appropriate battery capacity, the air start unit can also supply power consumer of these aircraft and other flying machines via the power supply.