Method for configurable aircraft USB power level management
Abstract:
Within examples, systems for power distribution within the cabin of an aircraft are provided and methods for operation. The system includes a passenger seat of the aircraft. The passenger seat includes a charging module. The charging module is configured to supply power to a connected device of the passenger seat. The passenger seat also includes a passenger control unit (PCU) coupled to the charging module. The passenger control unit is configured to determine a power requirement for the connected device. Additionally, the passenger seat is associated with a seat grouping of the aircraft. The seat grouping of the aircraft includes at least one passenger seat. Further, the power distribution system includes a power supply configured to supply power to at least one charging module based on the determined power requirement.
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