An electric vehicle includes: a third power supply line that supplies power from a quick charger placed outside the vehicle body to a battery, a positive-side line being on an upstream side of a current flowing from the quick charger to the battery, a negative-side line being on a downstream side the current flowing from the quick charger to the battery; a third protection circuit that is capable of cutting off the power via the third power supply line by electrically disconnecting the positive-side line and/or the negative-side line; and a control section that executes control for electrically disconnecting between the battery and the third power supply line when determining, based on a detection result of a third detection section, that the third protection circuit is in a state where each of the positive-side line and the negative-side line is not disconnectable.

A system comprises: an inverter configured to convert DC power from a battery to AC power to drive a motor, wherein the inverter includes: a power switch including a drain terminal, a source terminal, and a gate terminal; and a controller configured to detect a change in current at the source terminal of the power switch using a complex impedance of a metal trace connected to the source terminal of the power switch, and control a gate control signal to the gate terminal based on the detected change in current.

A power switching circuit is connected to a first power supply, a second power supply, a first circuit and a second circuit. The power switching circuit has a first main path, a second main path, a first switching path, and a second switching path. The power switching circuit has a control circuit that forms a power supply path by controlling each of the first main path, the second main path, the first switching path, and the second switching path in either a conducting or non-conducting state. When a failure is generated in one of the first circuit and the second circuit, the control circuit forms a power supply path that does not affect the operation of the other of the first circuit and the second circuit.

A control device for mounting in electrical heated wearables for controlling power to electrical heating wires secured in the heated wearables and capable of charging one or more portable batteries associate therewith and communicating data relative thereto. The control device has a finger-operable switch integrated with electronic circuits mounted on a pcb board. The electronic circuits include a communication circuit to interface with a wearer person to provide message information to the wearer person. The electronic circuits has power input terminals adapted to receive operating voltage from the one or more portable batteries. The pcb board with the finger-operable switch, the wiring connections and the electronic circuits are encapsulated by waterproof material. A female USB symmetrical input connecting port is mounted at a user accessible location on the control device and isolated from the pcb board and the electronic circuits by a further waterproof material. The female USB symmetrical input connecting port has a cable connection capable of transmitting power and data to the electronic circuits and power input terminals. The female USB symmetrical input connecting port is oriented to provide access to a symmetrical male plug connector secured to a power supply cable capable for supplying voltage from an auxiliary battery supply or charger and for the transmission of data information.

Disclosed is a method for controlling battery charging/discharging current in an off-grid mode of a hybrid energy storage inverter that is based on photovoltaic and a lithium battery. If photovoltaic energy is sufficient and a battery is not fully charged, the photovoltaic energy is supplied to a load and excess energy is supplied to the battery, to achieve maximum power point tracking of an output power of a photovoltaic component achieves maximum power point tracking; if photovoltaic energy is sufficient and a battery has been fully charged, the photovoltaic energy is supplied to a load, the excess photovoltaic energy is prohibited from charging the battery to prevent overcharging of the lithium battery; if photovoltaic energy is insufficient, the photovoltaic energy and battery energy are jointly supplied to a load, to achieve maximum power point tracking of an output power of a photovoltaic component.

The present disclosure relates generally to electric aircraft, and more specifically to electric power distribution for electric aircraft. In one embodiment, an electric aircraft is disclosed, comprising: a fuselage; two wings mounted on opposite sides of the fuselage; a plurality of first electric propulsion units, arranged on both sides of the fuselage, aft of the wings during forward flight; a plurality of second electric propulsion units arranged on both sides of the fuselage, forward of the wings during forward flight; and a plurality of battery packs, each battery pack configured to power at least: a portion of one of the first electric propulsion units on one side of the fuselage, and a portion of one of the second electric propulsion units on the other side of the fuselage.

A power supply unit for an aerosol generation device includes: a power supply configured to supply power to a heater configured to heat an aerosol source; a step-up system configured to function by a stepped-up voltage supplied from the power supply; a step-down system configured to function by a stepped-down voltage supplied from the power supply; and a direct-coupling system configured to function by a voltage supplied from the power supply.

A battery system may include a battery pack including a plurality of battery modules, a switching circuit connecting the plurality of battery modules in series or in parallel, and a battery management system (BMS) configured to control the switching circuit so as to connect the plurality of battery modules in series in a discharge mode to supply power from the battery pack to an external device and in a charge mode to charge the battery pack by receiving the power from the external device. In addition, the BMS may be configured to control entering a module balancing mode when a voltage difference among the plurality of battery modules exceeds a predetermined reference value, and control the switching circuit so as to connect the plurality of battery modules in parallel in the module balancing mode.

An aircraft, such as a rotary-wing aircraft, may be selectably fitted with power modules that may be installed in or removed from corresponding openings in the aircraft fuselage. The power modules may be interchangeable with other power modules, The power modules may utilize different technologies or thermodynamic cycles to generate power, including electrical batteries, fuel cells, a turbine powered generator, a reciprocating engine-powered generator, a turbine engine, a reciprocating engine, or other electrical or mechanical sources of power. The power modules may transfer electrical or mechanical power to the aircraft to maintain the aircraft in flight or to provide propulsion to the aircraft. An aircraft control system may detect the installed power modules and adjust inceptors and displays to correspond to the installed power modules.

An electric working machine includes an electric device, electric circuitry, battery packs to be connected sequentially to the electric device such that they are connected in parallel, and a controller. The electric circuitry includes external relays corresponding to the respective battery packs. The controller is configured or programmed to specify each battery pack as being a battery pack requiring a test process to examine opening and closing actions of internal relay(s) of the battery pack or a battery pack not requiring the test process, and in connecting the battery packs to the electric device, perform the test process on battery pack(s) that have been specified as requiring the test process to examine the opening and closing actions, and not perform the test process on battery pack(s) that have been specified as not requiring the test process to examine the opening and closing actions.