The present invention provides a novel system and method for a power management strategy for series hybrid power systems, such as for vehicles, with limited electrical energy storage capacity that distributes instantaneous power between a source of chemical energy and a small energy storage system (ESS) efficiently. The invention provides for minimizing the energy storage system while simultaneously allowing the chemical to electrical energy converter, e.g., an internal combustion motor/engine paired with an electrical generator and/or a fuel cell power source, to operate in pre-defined efficient regions of the power user's, or vehicle's, fuel efficiency map.

A circuit can include a CAN bus and multiple nodes. The multiple nodes can reboot at the same time so that a Time 0 is set at boot for each node. Each node can store an ID node and determine from its ID node one time slot of a plurality of periodic time slots starting from Time 0 in which to transmit on the CAN bus. Each node can transmit messages on the CAN bus in its determined time slot subsequent to Time 0.

A capacitive circuit with a supercapacitor is connected in series with a traction battery to provide a current sensor to produce a sensed signal that is linear across the operating range of the traction battery. The linear response of the capacitive circuit is an improvement over merely measuring the voltage across the battery, which is not linear over some ranges, e.g., 20% to 80% state of charge.

A power management system for a hybrid vehicle including an engine includes a vehicle power bus distributing power from a battery to vehicle loads. A capacitor includes one of a plurality of supercapacitors and a plurality of ultracapacitors. A starter/generator controller communicates with the capacitor and the battery. A power management module is configured to supply current from the capacitor to the starter/generator controller during cranking of the engine; and supply current from the battery to the starter/generator controller during the cranking of the engine. The power supplied by the battery is greater than or equal to 2% and less than or equal to 20% of a total power supplied to the starter/generator controller during the cranking of the engine.

Electronic architecture (3) for controlling a DC/AC voltage converter (2), said converter (2) comprising a plurality of arms mounted in parallel, each arm comprising two controllable switching cells (21), in series and separated by a mid-point, the arms being paired in H-bridges (20), the architecture (3) comprising: a main control unit (36), configured to communicate through a potential barrier (61) with a remote control unit (35), and a plurality of secondary control units (37), each secondary control unit (37) being dedicated to controlling a respective H-bridge (20), and comprising: a processing unit (40) for processing the information received from the main control unit (36), and a monitoring unit (41) for monitoring the controllable switching cells (21) of said H-bridge (20), said monitoring unit (41) being configured to modify the state of all or some of said switching cells (21) of said H-bridge (20) at least on the basis of information received from the corresponding processing unit (40).

A vehicle may include an inverter, a motor coupled to the inverter, and a traction battery coupled to the inverter and having a terminal voltage equal to a rail voltage between rails of the inverter such that the rail voltage is unregulated. The vehicle may also include a voltage converter configured to reduce the terminal voltage below an intermediate bus voltage threshold on an intermediate bus, and an auxiliary converter configured to draw power from the intermediate bus to supply auxiliary loads.

A storage apparatus includes a plurality of storage cells connected in series. Each storage cell comprises a storage element that stores a charge, a container that houses the storage element, a reception antenna capable of receiving power transmitted from a transmission antenna of a feeding facility provided in a wireless power transfer system, and a charging control circuit that charges the storage element using the power received by the reception antenna. The plurality of storage cells are charged concurrently and wirelessly, and therefore charging can be performed on all of the storage cells without overcharging or undercharging.

A control system and method method for a powertrain unit of a pedal assisted electrical bicycle, the powertrain unit including an electrical motor, a DC/AC converter to supply the motor from a battery wherein the following steps are taken: starting the electrical machine in order to rotate the rotor; estimating a back electromotive force produced by the electrical machine; estimating the angular position of the rotor with respect to the stator winding starting from the estimation of the back electromotive force; controlling the DC/AC converter based on said estimated angular position in order to make it supply the stator winding so that said electrical machine delivers a torque.

A management method for the energy range of a rechargeable battery pack of an assisted pedal electrical bicycle (1) including an electrical machine controllable for supplying a torque according to a pedal assistance factor, said torque being summed to the one generated by a cyclist through the pedaling, the management method including the following steps: a) selecting a route to be traveled by the electrical bicycle (1) starting from an initial position; b) obtaining data representative of the altitude profile of the selected route and dividing the route in a plurality of segments each being characterized by a respective altitude parameter; c) calculating a value correlated to the maximum percentage of battery pack (20) discharge on the selected route as a function of the altitude profile and of a limit pedal assistance factor K_limit, preferably calculating a value for each segment representative of the percentage of battery pack (20) discharge on the segment as a function of a limit assistance factor K_limit associated to each segment based on the altitude parameter associated to the segment; d) verifying whether the battery pack (20) has a residual positive charge or not at N the end of the route; wherein, if following that step d) of verifying it is determined that the battery pack (20) does not have a residual positive charge at the end of the route, then the management method iteratively repeats the steps c) and d) modifying the limit assistance factor K_limit based on one or more adjustment curves each allowing to obtain a new limit assistance factor for each segment as a function of the segment slope.

An aircraft has a fuel cell, a battery configured to be charged by the fuel cell, a supercapacitor configured to be charged by the fuel cell, and a power management unit configured to receive electrical power from the fuel cell, the battery, and the supercapacitor.