B60L50/00

METHOD AND DEVICE FOR MANAGING THE ENERGY SUPPLIED BY A HYBRID POWER PLANT FOR A ROTORCRAFT
20220081122 · 2022-03-17 · ·

A method for managing the energy supplied by a hybrid power plant for propelling a rotorcraft, the hybrid power plant comprising two heat engines, two electric motors and an electrical energy source. The method includes a step of acquiring at least one first characteristic of the electrical energy source and/or the electric motors and a step of determining a mechanical power requirement of the rotorcraft. The method then includes a step of determining a first power distribution between each heat engine and electric motor as a function of the first characteristic and the mechanical power requirement of the rotorcraft, then a step of controlling each heat engine and electric motor according to several operating modes, including a distributed operating mode applying the first power distribution.

Auxiliary electrical traction motor for vehicles

A vehicle traction device having at least one energy storage component; at least one traction component; at least one acceleration sensor including a pressure sensor, a motion sensor, a gyroscopic sensor, an accelerometer, and/or a piezoelectric sensor; and at least one deceleration sensor including a pressure sensor, a motion sensor, a gyroscopic sensor, an accelerometer, and/or a piezoelectric sensor. The at least one acceleration/deceleration sensor is responsive to an operator input, and when the operator input is applied to the at least one acceleration/deceleration sensor, the energy traction device is signaled to transfer energy from the at least one energy storage component to the forward propulsion of the vehicle, or vice versa, using the at least one traction component. The vehicle traction device may be incorporated into, for example, a wheel, a motor, and/or a transmission.

Auxiliary electrical traction motor for vehicles

A vehicle traction device having at least one energy storage component; at least one traction component; at least one acceleration sensor including a pressure sensor, a motion sensor, a gyroscopic sensor, an accelerometer, and/or a piezoelectric sensor; and at least one deceleration sensor including a pressure sensor, a motion sensor, a gyroscopic sensor, an accelerometer, and/or a piezoelectric sensor. The at least one acceleration/deceleration sensor is responsive to an operator input, and when the operator input is applied to the at least one acceleration/deceleration sensor, the energy traction device is signaled to transfer energy from the at least one energy storage component to the forward propulsion of the vehicle, or vice versa, using the at least one traction component. The vehicle traction device may be incorporated into, for example, a wheel, a motor, and/or a transmission.

DEVICE FOR ENERGY DISTRIBUTION AND/OR ENERGY CONVERSION

The invention relates to a device for energy storage, energy distribution and/or energy conversion in a hybrid or electric vehicle, comprising at least one high-voltage system having at least one high-voltage unit. In order to provide a simple, efficient and safe device, according to the invention, the high-voltage system has a hermetically encapsulated housing having at least one wall, in which housing at least one unit chamber for receiving the high-voltage unit and at least one interface chamber for receiving at least one interface region are arranged.

Power storage device
11267347 · 2022-03-08 · ·

A power storage device includes a plurality of power storage units which are stacked and disposed in a predetermined direction, a plurality of terminal portions which are provided in the plurality of power storage units, and a plurality of conductive members which extend in the predetermined direction along the plurality of power storage units and are connected to the plurality of terminal portions. Each of the plurality of conductive members includes a connection portion attached to the terminal portion, a main body portion provided integrally with the connection portion, and an electrically insulating coating covering a surface of the main body portion. In each of the plurality of conductive members, a length of the connection portion in the predetermined direction is formed to change with a trend of increasing as a length of the main body portion in the predetermined direction increases.

Power supply system for driving vehicle

The present invention discloses a power supply system capable of supplying electric power to a vehicle, in particular, an electric vehicle, while reducing the number of components and improving stability. An embodiment of the present invention discloses a power supply system comprising: a battery comprising battery cells; a first switching device formed between one electrode of the battery and a power load unit comprising a motor that receives power from the battery; a pre-charge resistor having one end electrically connected to the other electrode of the battery; and a second switching device formed between the other end of the pre-charge resistor and the other electrode of the battery.

Power supply system for driving vehicle

The present invention discloses a power supply system capable of supplying electric power to a vehicle, in particular, an electric vehicle, while reducing the number of components and improving stability. An embodiment of the present invention discloses a power supply system comprising: a battery comprising battery cells; a first switching device formed between one electrode of the battery and a power load unit comprising a motor that receives power from the battery; a pre-charge resistor having one end electrically connected to the other electrode of the battery; and a second switching device formed between the other end of the pre-charge resistor and the other electrode of the battery.

Methods and apparatus to charge electric vehicles

Methods and apparatus to charge electric vehicles are disclosed. An example method includes monitoring, via a processor, a battery charge level of an electric vehicle receiving a battery charge from a mobile charging unit. The example method includes determining, via the processor, a remaining trip distance of the electric vehicle from a location of the battery charge to a trip destination. The example method further includes determining, via the processor, a target charge level for the battery charge. The target charge level corresponds to when the battery charge level provides a first probability that the electric vehicle will reach the trip destination without an additional battery charge. The example method also includes generating, via the processor, a signal to stop the battery charge when the battery charge level reaches the target charge level.

DC INVERTER/CONVERTER CURRENT BALANCING FOR PARALLELED PHASE LEG SWITCHES
20210313906 · 2021-10-07 ·

Current imbalances between parallel switching devices in a power converter half leg are reduced. A gate driver generates a nominal PWM gate drive signal for a respective half leg. A first feedback loop couples the nominal PWM gate drive signal to a gate terminal of a respective first switching device. The first feedback loop has a first mutual inductance with a current path of a first parallel switching device and has a second mutual inductance with a current path of a second parallel switching device. The first and second mutual inductances are arranged to generate opposing voltages in the first feedback loop, so that when all the parallel switching devices carry equal current then the voltages cancel.

SYSTEMS AND METHODS FOR RESTRICTING POWER TO A LOAD TO PREVENT ENGAGING CIRCUIT PROTECTION DEVICE FOR AN AIRCRAFT
20210309110 · 2021-10-07 · ·

A system for restricting power to a load to prevent engaging a circuit protection device for an electric aircraft includes an energy source. The energy source is communicatively coupled to a load, wherein the load includes a portion of a propulsion system. The system includes sensors configured to sense an electrical parameter. The system includes an aircraft controller communicatively connected to the energy source, wherein the aircraft controller is configured to receive an electrical parameter, compare the electrical parameter to a current allocation threshold, detect that the electrical parameter has reached a current allocation threshold, generate a current allocation threshold notification as a function of the detection, wherein the current allocation threshold notification indicates that the electrical parameter has reached the current allocation threshold.