Patent ID: 11962147
Assignee: H55 SA
Field: Electrical machinery, apparatus, energy (Electrical engineering)
Classification: CPC H  B  Y | IPC H

Claim 0:
1. A system which powers an aircraft, the system comprising:
a hardware controller configured to control a transducer of the aircraft;
a plurality of battery packs configured to provide an output voltage to the hardware controller;
a charging interface configured to connect to the transducer to charge the plurality of battery packs;
a plurality of diodes electrically connected to the plurality of battery packs, the charging interface, and the hardware controller, the plurality of diodes comprising a first set of diodes and a second set of diodes, the first set of diodes being oriented to prevent electrical current flowing from the plurality of battery packs to the charging interface, the second set of diodes being oriented to prevent electrical current flowing from the hardware controller to the plurality of battery packs and the charging interface and allow electrical current to flow from the charging interface to the hardware controller; and
a pre-charge circuit configured to selectively reduce an amount of electrical current flowing to the hardware controller.