B64F1/35

PARALLEL POWER SOURCE FOR AIRCRAFT
20250236416 · 2025-07-24 ·

A GPU output from a ground power unit (GPU) can be converted to power suitable for starting a jet engine of an aircraft by an auto-transformer rectifier unit (ATRU) of the aircraft. Multiple ATRUs, each connected to a corresponding GPU, may output multiple ATRU outputs, and combining these multiple ATRU outputs can generate a combined power, which can satisfy the power requirements for starting a jet engine when they exceed what can be supplied by a single GPU. The combining is possible when the outputs of the ATRUs are synchronized, which can require generating and sharing a sync signal between the ATRUs that is synchronous with an ATRU designated as the master (i.e., reference) for the other ATRUs.

PARALLEL POWER SOURCE FOR AIRCRAFT
20250236416 · 2025-07-24 ·

A GPU output from a ground power unit (GPU) can be converted to power suitable for starting a jet engine of an aircraft by an auto-transformer rectifier unit (ATRU) of the aircraft. Multiple ATRUs, each connected to a corresponding GPU, may output multiple ATRU outputs, and combining these multiple ATRU outputs can generate a combined power, which can satisfy the power requirements for starting a jet engine when they exceed what can be supplied by a single GPU. The combining is possible when the outputs of the ATRUs are synchronized, which can require generating and sharing a sync signal between the ATRUs that is synchronous with an ATRU designated as the master (i.e., reference) for the other ATRUs.

MACHINE AND PROCESS FOR DRIVING AN ELECTRIC MOTOR

An aircraft adaptive battery charging system is provided. The adaptive battery charging system comprises: a battery system; a bidirectional converter, wherein the bidirectional converter is capable of an inverter mode and a rectifier mode; an alternating current (AC) motor; a number of controllable contactors that control electrical current between the battery system, bidirectional converter, AC motor, and a power source wherein the controllable contactors can be switched between a closed position to allow electrical current flow and an open position to prevent electrical current flow; a motor controller; a battery charging system controller configured to send control signals to the battery system, motor controller, and controllable contactors in response to system command signals; and a vehicle system controller that sends system command signals to the motor controller and battery charging system controller.

SYSTEM AND METHOD FOR MANAGING SMART BUILDING FOR INTEGRATED OPERATION OF HETEROGENEOUS MOBILITY DEVICES
20250282493 · 2025-09-11 ·

A system comprises a smart building with a vertiport zone and a complex zone; and a managing device. The managing device is configured to: establish movement route information, of the aerial mobility device in the vertiport zone, based on management information associated with a transport object or flight of the aerial mobility device. If the movement route information indicates to move to at least one designated area of the vertiport zone and a charging permission condition is satisfied, the movement route information is set to add a charging site as a layover point. The aerial mobility device is controlled to move to the charging site according to the set movement route information and to be charged. If the movement route information indicates to move to the complex zone, the aerial mobility device is controlled to move to an exit area of the vertiport zone approaching the complex zone.

SYSTEM AND METHOD FOR MANAGING SMART BUILDING FOR INTEGRATED OPERATION OF HETEROGENEOUS MOBILITY DEVICES
20250282493 · 2025-09-11 ·

A system comprises a smart building with a vertiport zone and a complex zone; and a managing device. The managing device is configured to: establish movement route information, of the aerial mobility device in the vertiport zone, based on management information associated with a transport object or flight of the aerial mobility device. If the movement route information indicates to move to at least one designated area of the vertiport zone and a charging permission condition is satisfied, the movement route information is set to add a charging site as a layover point. The aerial mobility device is controlled to move to the charging site according to the set movement route information and to be charged. If the movement route information indicates to move to the complex zone, the aerial mobility device is controlled to move to an exit area of the vertiport zone approaching the complex zone.

Unmanned aerial vehicle base station and unmanned aerial vehicle system
12415634 · 2025-09-16 · ·

The embodiments of the present disclosure involve the technical field of unmanned aerial vehicles, and disclose an unmanned aerial vehicle base station and an unmanned aerial vehicle system. The unmanned aerial vehicle base station includes a bracket, a tarmac, a charging component, and a temperature adjusting component. The bracket is provided with an accommodating cavity, the tarmac separates the accommodating cavity into an upper compartment chamber and a lower compartment chamber, the temperature adjusting component includes a semiconductor module, a first ventilation assembly, a second ventilation assembly, and a third ventilation assembly, and the semiconductor module is partially provided on the first ventilation assembly and partially provided on the second ventilation assembly.

Unmanned aerial vehicle base station and unmanned aerial vehicle system
12415634 · 2025-09-16 · ·

The embodiments of the present disclosure involve the technical field of unmanned aerial vehicles, and disclose an unmanned aerial vehicle base station and an unmanned aerial vehicle system. The unmanned aerial vehicle base station includes a bracket, a tarmac, a charging component, and a temperature adjusting component. The bracket is provided with an accommodating cavity, the tarmac separates the accommodating cavity into an upper compartment chamber and a lower compartment chamber, the temperature adjusting component includes a semiconductor module, a first ventilation assembly, a second ventilation assembly, and a third ventilation assembly, and the semiconductor module is partially provided on the first ventilation assembly and partially provided on the second ventilation assembly.

SYSTEMS AND METHODS FOR SHIELDING USING DRONES
20250315065 · 2025-10-09 ·

Disclosed herein are systems comprising: a swarm of unmanned aerial vehicles (UAV); a payload comprising a surface material; and a controller configured to perform operations comprising: connecting each UAV of the swarm to a plurality of connecting points of the payload, such that the swarm of UAVs is configured to collectively support and move the payload; deploying the payload to a selected location and at a selected shape above an environment to provide a selected degree of shade to the environment by directing each UAV of the swarm to hover at a selected location; and adjusting the selected location and/or the selected shape of the payload to track a trajectory of the sun by adjusting the selected location of each UAV of the swarm.

SYSTEMS AND METHODS FOR SHIELDING USING DRONES
20250315065 · 2025-10-09 ·

Disclosed herein are systems comprising: a swarm of unmanned aerial vehicles (UAV); a payload comprising a surface material; and a controller configured to perform operations comprising: connecting each UAV of the swarm to a plurality of connecting points of the payload, such that the swarm of UAVs is configured to collectively support and move the payload; deploying the payload to a selected location and at a selected shape above an environment to provide a selected degree of shade to the environment by directing each UAV of the swarm to hover at a selected location; and adjusting the selected location and/or the selected shape of the payload to track a trajectory of the sun by adjusting the selected location of each UAV of the swarm.

Charging port of an electric aircraft
12444960 · 2025-10-14 · ·

Aspects relate to a charging port of an electric aircraft and methods of use terminating a charging connection between a charger and the electric aircraft. A charging port includes a controller that is configured to receive a control signal from a remote device and terminate the charging connection in response to the control signal.