Patent classifications
H01M10/667
BATTERY MODULE AND VEHICLE INCLUDING THE SAME
A battery module, a vehicle, and a method of manufacturing a battery module, the battery module including a housing accommodating a plurality of secondary batteries; and a thermoelectric element assembly on the housing and in contact with the plurality of secondary batteries through at least one contact opening in the housing, the thermoelectric element assembly being configured to heat or cool the plurality of secondary batteries.
BATTERY MODULE AND VEHICLE INCLUDING THE SAME
A battery module, a vehicle, and a method of manufacturing a battery module, the battery module including a housing accommodating a plurality of secondary batteries; and a thermoelectric element assembly on the housing and in contact with the plurality of secondary batteries through at least one contact opening in the housing, the thermoelectric element assembly being configured to heat or cool the plurality of secondary batteries.
THERMAL MANAGEMENT SYSTEM FOR BATTERY PACK AND THERMAL MANAGEMENT SYSTEM FOR ELECTRIC VEHICLE
This application discloses a thermal management system for a battery pack and a thermal management system for an electric vehicle. the thermal management system for the battery pack includes: a thermal management device for the battery pack, a processor, and a solenoid valve network connected to the thermal management device for the battery pack. An external port of the solenoid valve network is connected to an external cooling system. The processor is configured to control operating status of a solenoid valve in the solenoid valve network, so that the thermal management device for the battery pack heats the battery pack by using heat generated by the external cooling system.
TEMPERATURE CONTROL SYSTEM FOR LITHIUM ION BATTERY CELLS
The present invention relates to a temperature control system for effective cooling and heating of rechargeable battery cells, in particular lithium (Li) ion batteries, wherein the temperature control module comprises an outer shell (1) made of a polymer material, which surrounds at least one heat-conducting layer made of unidirectional carbon fibre composite (2) and has, on each of two opposing edge regions of the main surfaces thereof, a conduit (3) for conveying a heat transfer medium, the conduits (3) extending along the edge regions from one end to the other; at least two layers of unidirectional carbon fibre composite (2) arranged one above the other are preferably provided, and an intermediate layer (7) having throughflow channels (8) which connect the conduits (3) to one another is located between the layers.
TEMPERATURE CONTROL SYSTEM FOR LITHIUM ION BATTERY CELLS
The present invention relates to a temperature control system for effective cooling and heating of rechargeable battery cells, in particular lithium (Li) ion batteries, wherein the temperature control module comprises an outer shell (1) made of a polymer material, which surrounds at least one heat-conducting layer made of unidirectional carbon fibre composite (2) and has, on each of two opposing edge regions of the main surfaces thereof, a conduit (3) for conveying a heat transfer medium, the conduits (3) extending along the edge regions from one end to the other; at least two layers of unidirectional carbon fibre composite (2) arranged one above the other are preferably provided, and an intermediate layer (7) having throughflow channels (8) which connect the conduits (3) to one another is located between the layers.
Thermal system layout designed for high cooling capacity at idle condition
An air conditioning and battery cooling arrangement is provided having an A/C coolant circuit and an electric drive train coolant circuit as well as a refrigeration circuit, wherein the A/C coolant circuit and the electric drive train coolant circuit are coupled to each other via a 4/2-way coolant valve in such a manner that the A/C coolant circuit and the electric drive train coolant circuit are configured to be operated separately or for serial through-flow.
ENERGY STORAGE SYSTEM AND TEMPERATURE CONTROL METHOD THEREOF
An energy storage system and a temperature control are provided in this application, and the energy storage system includes a main control module, a battery module, and a temperature control apparatus. The battery module includes a battery monitoring unit and a battery pack, the battery monitoring unit includes a battery management system and a DC/DC power converter, and the main control module is configured to control the temperature control apparatus to choose to transport a heat conduction medium to the battery module along at least one of a first path and a second path. The heat conduction medium along the first path reaches the battery pack after passing through the battery monitoring unit, and the heat conduction medium along the second path reaches the battery monitoring unit after passing through the battery pack.
HEATSINK CONFIGURATION AND ARRANGMENT FOR INVERTER AND SYSTEMS, COMPONENTS, AND METHODS THEREOF
A heatsink or heat exchanger for one or more power modules of an inverter or a converter comprises a coolant flow channel, comprised of a plurality of coolant flow channel portions that form a switchback or serpentine flow path, and that is adapted to circulate coolant inside the heat exchanger or heatsink. One or more vents can be provided inside the heat exchanger or heatsink to pass air from one coolant flow channel portion to an adjacent coolant flow channel portion.
HEATSINK CONFIGURATION AND ARRANGMENT FOR INVERTER AND SYSTEMS, COMPONENTS, AND METHODS THEREOF
A heatsink or heat exchanger for one or more power modules of an inverter or a converter comprises a coolant flow channel, comprised of a plurality of coolant flow channel portions that form a switchback or serpentine flow path, and that is adapted to circulate coolant inside the heat exchanger or heatsink. One or more vents can be provided inside the heat exchanger or heatsink to pass air from one coolant flow channel portion to an adjacent coolant flow channel portion.
ELECTRIC PROPULSION SYSTEM OF AN AIRCRAFT
An electric propulsion system of an aircraft includes an electrical generator and a cooling device of the electrical generator. It further includes at least one thermoacoustic engine and a heat transfer circuit configured to transport heat dissipated by the electrical generator to the thermoacoustic engine. The cooling device of the electrical generator is at least partially powered by energy from the thermoacoustic engine.