A power system, includes a first switch, a second switch, a first switched capacitor circuit, a second switched capacitor circuit, an inductive voltage conversion circuit, an input end, a first charging end, and a second charging end. An input side of the inductive voltage conversion circuit is coupled to the input end. An output side of the inductive voltage conversion circuit is coupled to the first charging end through the first switch, and is coupled to the second charging end through the second switch. The first switched capacitor circuit is coupled between the input end and the first charging end. The second switched capacitor circuit is coupled between the input end and the second charging end.

A battery fleet charging system for charging two or more battery packs simultaneously, at independently controlled charge rates. The present invention can intelligently distribute the available charge power among multiple batteries, either symmetrically or asymmetrically, as specified by a controller that specifies and regulates the charge voltage.

A power-supply and recharge group for an electric vehicle comprising: a first battery pack; a second battery pack; a first DC-to-DC converter; a second DC-to-DC converter; a low-voltage power-supply source; and a control unit configured to: detect a charge difference between a first and a second battery pack; transfer an electric current from a low-voltage power-supply source to the one of the first and second battery pack having a lower charge, until said charge difference is cancelled; connect the first and the second battery pack to one another in series and recharge them by means of a recharge station on the outside of the vehicle. A direct connection between the DC-to-DC converters can replace the auxiliary low-voltage source.

The described technology provides a method of balancing power supplied to a system load by a first battery power source and a second battery power source. The method includes sensing a first current supplied by or supplied to the first battery source. The method further includes changing a control voltage for a voltage converter circuit based on the sensed first current, an input of the voltage converter circuit being coupled to the second battery power source, an output of the voltage converter circuit being electrically coupled to the system load. The method still further includes adjusting the voltage converter circuit to modify a charge current supplied from the second battery power source to the first battery power source based on the control voltage.

A multiple-battery charger includes a switching subsystem and a control element. The switching subsystem is configured to selectively electrically connect each of a plurality of individual batteries one at a time to a constrained energy source having electrical power production that varies over time. The control element is operatively connected to the switching subsystem. The control element is configured to deliver one or more pulse width modulated signals to the switching subsystem. The one or more pulse width modulated signals establish a duty cycle with which each of the plurality of batteries is electrically connected to the constrained energy source to receive electrical power from the constrained energy source.

An electrical power system has a dual battery configuration that enables sufficient power supply for a spacecraft bus and a payload module being carried by the spacecraft. During a sunlight power mode, power is drawn from a solar array of the bus to power a low-discharge payload of the spacecraft and a high-discharge payload of a payload module. During the sunlight power mode, a low rate discharge battery and a high rate discharge battery are charged by a battery charge management unit of the spacecraft bus. During an eclipse power mode, the low rate discharge battery powers the low-discharge payload of the spacecraft and the high rate discharge battery powers the high-discharge payload of the payload module. The high-rate discharge battery may also be used to power the high-rate discharge payload in the sunlight power mode to meet its high current demands to meet a flexible mission operations.

An example foldable mobile computing device includes a first side including a first power storage device coupled to a first regulator. The device includes a second side including a second power storage device coupled to a second regulator and connected in parallel with the first power storage device. The second side is configured to articulate relative to the first side about a hinge. The device includes processing circuitry configured to determine a power storage capacity of the first power storage device and to determine a power storage capacity of the second power storage device. The device is also configured to adjust, based on the power storage capacity of the first power storage device and the power storage capacity of the second power storage device, at least one of an impedance of the first regulator or an impedance of the second regulator.

The present invention relates to a system and method for controlling inter-battery charging/discharging of a dual battery, and relates to a system and method for controlling charging/discharging between batteries to prevent a problem in which a specific battery is deteriorated due to charging/discharging between batteries due to a voltage difference when the voltage difference between the batteries of the dual batteries installed in the external system is within the appropriate range.

A system and method for balancing a battery having a plurality of cells connected in series. The system includes a plurality of reactive charge transfer units connected with the plurality of cells, a first control unit and a second control unit. The first control unit is configured to determine a state of charge of the plurality of cells, determine a reference value associated with the battery, identify an overcharged cell or a discharged cell in the battery, and determine a charge differential between state of charge of the overcharged cell or the discharged cell and the reference value associated with the battery. The second control unit is configured to arrange charge transfer between the overcharged cell or the discharged cell, and remaining pack of cells in the battery. The first and the second control units are configured to function iteratively until cell balancing is attained.

A DC energy storage unit with a plurality of energy storage modules, each energy storage module including a plurality of electrochemical energy storage devices electrically connected in series; an internal control unit in the energy storage module; a power supply for the internal control unit; and a wireless communication system; wherein the total voltage of the plurality of energy storage devices in series is greater than or equal to 40 V DC, wherein the plurality of energy storage modules are coupled together in series, or in parallel, each energy storage unit including a wireless gateway for communication between the energy storage unit controller and each energy storage module; wherein each energy storage module further has a housing, the housing at least partially having a non magnetic material.