The disclosure relates to electrical converters for use in aircraft electrical power systems and to methods of operating such electrical converters to maintain reliable operation of semiconductor components over varying cosmic radiation levels at altitude. Exemplary embodiments include an electrical converter comprising: a converter circuit having a plurality of semiconductor devices configured to convert an input electrical supply to an output electrical supply; and a controller connected configured to receive an input altitude signal, wherein the controller is further configured to control a temperature of the plurality of semiconductor devices according to the received input altitude signal to reduce an effect of increased incident cosmic radiation on the converter circuit.

The electric vehicle according to the present disclosure is configured to be able to select a traveling mode between an MT mode in which an electric motor is controlled with torque characteristics like an MT vehicle having a manual transmission and an internal combustion engine, and an EV mode in which the electric motor is controlled with normal torque characteristics. When the selection of the travelling mode is changed by a driver, the controller of the electric vehicle determines whether a control mode can be switched, based on a condition in which the electric vehicle is placed, and switches the control mode in accordance with the determination result.

A motor vehicle has a motor performing power driving and regeneration. The motor has an inverter, a first power storage device with a large-capacity characteristic, a second power storage device with a high-power characteristic, a power converter and a circuit. The power converter has a voltage step down function during the power driving and a voltage step up function during the regeneration. In the circuit, the power converter, with the voltage step down function during the power driving, is connected to the first power storage device and the second power storage device is connected in series between a reactor of the power converter and the inverter. During the power driving of the motor, an output voltage of the first power storage device is stepped down to supply energy from the first power storage device and the second power storage device to the inverter.

It is an object of the present invention to provide a drive system including an induction generator comprising some primary windings that has a main winding and an auxiliary winding, the drive system being capable of supplying electric power required by an auxiliary inverter, even in a regenerative mode of operation in which only the auxiliary winding is energized. The maximum current value of a converter for power generating is set on the basis of the maximum output power of the auxiliary winding of the induction generator and the minimum voltage applied to the auxiliary winding unless a traction inverter is in a regenerative mode of operation, and the non-load current value of the induction generator is set such that the maximum current in the auxiliary winding under the situation of the traction inverter being in the regenerative mode of operation does not exceed the maximum current in the converter for power generating.

Systems and methods for energy storage and management may be useful for a variety of applications, including launch devices. A system can include a direct current (DC) bus configured to operate within a predetermined range of voltages. The system can also include an array comprising a plurality of ultra-capacitors connected to the DC bus and configured to supply the DC bus with energy. The system can further include an input configured to receive energy from a power grid, wherein the power grid is configured to supply fewer than 250 amps of power. The system can additionally include an output configured to supply more than 250 amps of power. The system can also include a controller configured to control charging and discharging of the array of ultracapacitors and configured to control the DC bus to remain within the predetermined range of voltages.

A control device is a control device of a moving body that includes a first accumulation unit configured to accumulate first energy, a second accumulation unit configured to accumulate second energy different from the first energy, and an electric motor configured to generate power to move using any one or both of second energy obtained by converting first energy accumulated in the first accumulation unit and second energy accumulated in the second accumulation unit, in which a required amount, which is an amount of the second energy required to move from a current place to a supply point that is a point where supply of the first energy is received, is acquired when the second energy is accumulated in the second accumulation unit and, if the required amount has been supplied to the second accumulation unit, a termination-related operation related to termination of the supply is executed.

A hierarchical vehicle control system for a vehicle powered by a distributed propulsion system (DPS) comprising plurality of propelling axles driven by plurality of motors and powered by a battery system comprising plurality of battery packs. Said hierarchical vehicle control system comprising a first controller, a second controller that generates axle command signals for operation of the propelling axles, and a third controller that generates motor command signals for operation of the electric motors wherein said third controller further comprising a DPS diagnosis/prognosis module, a DPS fault tolerance module and a power distribution management module.

A semiconductor device includes a first terminal for a battery, a second terminal for an inverter circuit, and a transistor. The semiconductor device is configured to control a voltage applied to a control terminal of the transistor to allow supply of a current from the first terminal to the second terminal and allow supply of a current from the second terminal to the first terminal. A withstand voltage between the first terminal and the second terminal is greater than or equal to a voltage between the battery and the inverter circuit.

A power converter includes a semiconductor module, a capacitor module, a control board, and an insulating plate. The capacitor module includes a smoothing capacitor, a first connection terminal electrically connected to the smoothing capacitor and a power supply outside the power converter, and a second connection terminal electrically connected to the semiconductor module. The insulating plate is located between the capacitor module and the control board so as to cover at least one of the first connection terminal and the second connection terminal.

Systems and methods for operating an electric drive system for an electric or hybrid vehicle is described. In one example, the drive system is operated to provide extra losses during select vehicle operating conditions so that greater amounts of regenerative braking may be generated without having to store larger amounts of electric energy in an electric energy storage device.