An energy storage container and a heat dissipation system for the same are provided. The heat dissipation system for the energy storage container includes a container body, and a battery module assembly and multiple air conditioning modules both located in the container body. In a length direction or a width direction of the container body, each of two side ends of the battery module assembly is provided with at least one air conditioning module. The heat dissipation system further includes an air supply duct and an air return duct, a partition plate is arranged in the air supply duct, to divide the air supply duct into a first air supply duct and a second air supply duct which are mutually independent. The above arrangement avoids increasing a height of the energy storage container, thereby effectively facilitating the transportation and installation of the energy storage container.

An aircraft hybrid cooling system is disclosed. The aircraft hybrid cooling system includes a conduit through an aircraft that is configured to allow airflow through the conduit. The aircraft hybrid cooling system additionally includes a battery assembly positioned in the conduit, configured to provide for airflow past a battery in the battery assembly in a first mode of operation and configured to provide flow of a cooling medium past the battery in a second mode of operation. In some embodiments, the battery in the battery assembly is cooled via airflow in the event the aircraft is in flight and is cooled via an applied cooling medium in the event the aircraft is grounded.

An aircraft hybrid cooling system is disclosed. The aircraft hybrid cooling system includes a conduit through an aircraft that is configured to allow airflow through the conduit. The aircraft hybrid cooling system additionally includes a battery assembly positioned in the conduit, configured to provide for airflow past a battery in the battery assembly in a first mode of operation and configured to provide flow of a cooling medium past the battery in a second mode of operation. In some embodiments, the battery in the battery assembly is cooled via airflow in the event the aircraft is in flight and is cooled via an applied cooling medium in the event the aircraft is grounded.

A thermal management system for a vehicle includes a cooling apparatus for circulating a coolant in a coolant line to cool at least one electrical component provided in the coolant line, a battery cooling apparatus for circulating the coolant to the battery module, a chiller for heat exchanging the coolant with a refrigerant to control a temperature of the coolant, a heater that heats an interior of the vehicle using the coolant, and a branch line. A condenser included in the air conditioner is connected to the coolant line so as to pass the coolant circulating through the cooling apparatus.

A thermal management system for a vehicle includes a cooling apparatus for circulating a coolant in a coolant line to cool at least one electrical component provided in the coolant line, a battery cooling apparatus for circulating the coolant to the battery module, a chiller for heat exchanging the coolant with a refrigerant to control a temperature of the coolant, a heater that heats an interior of the vehicle using the coolant, and a branch line. A condenser included in the air conditioner is connected to the coolant line so as to pass the coolant circulating through the cooling apparatus.

The present invention describes a battery system. The battery system comprises a battery housing having at least one inlet and at least one outlet, at least one battery cell positioned within the battery housing, and a battery protecting unit connected to the battery housing through the at least one inlet at one or more first predetermined positions. The battery protecting unit is adapted to detect one or more abnormalities in the at least one battery cell and provide coolant to the at least one battery cell through a dynamically determined at least one conduit. The system detects abnormalities based on receiving one or more signals received from one or more sensors. The system also comprises a controlling unit for providing the control signals based on detection abnormalities in one or more battery cells through one or more sensors configured in the battery housing.

An energy storage container and a heat dissipation system for the same are provided. The heat dissipation system for the energy storage container includes a container body, and a battery module assembly and multiple air conditioning modules both located in the container body. In a length direction or a width direction of the container body, each of two side ends of the battery module assembly is provided with at least one air conditioning module. The heat dissipation system further includes an air supply duct and an air return duct, a partition plate is arranged in the air supply duct, to divide the air supply duct into a first air supply duct and a second air supply duct which are mutually independent. The above arrangement avoids increasing a height of the energy storage container, thereby effectively facilitating the transportation and installation of the energy storage container.

There is provided a battery cooling control system capable of efficiently and effectively controlling the cooling of a battery. While an electric powered vehicle travels and/or stops, it is determined whether or not there is an indication of a battery being charged, and if it has been determined that there is the indication of charging being performed, it is determined whether or not there is a necessity for cooling the battery, and if it has been determined that there is the necessity for cooling the battery, the battery is cooled to a predetermined value during traveling. In addition, based on at least a state of charge of the battery and/or a driving range, it is determined whether or not there is an indication of charging being executed, and based on a real-time battery temperature, an increase in battery temperature caused by charging, and an upper limit value for a predetermined allowable battery temperature range, it is determined whether or not there is a necessity for cooling the battery.

There is provided a battery cooling control system capable of efficiently and effectively controlling the cooling of a battery. While an electric powered vehicle travels and/or stops, it is determined whether or not there is an indication of a battery being charged, and if it has been determined that there is the indication of charging being performed, it is determined whether or not there is a necessity for cooling the battery, and if it has been determined that there is the necessity for cooling the battery, the battery is cooled to a predetermined value during traveling. In addition, based on at least a state of charge of the battery and/or a driving range, it is determined whether or not there is an indication of charging being executed, and based on a real-time battery temperature, an increase in battery temperature caused by charging, and an upper limit value for a predetermined allowable battery temperature range, it is determined whether or not there is a necessity for cooling the battery.

A synthetic jet actuator includes a cavity layer having an internal cavity for reception of a fluid volume and an orifice providing a fluid communication between the cavity and an external atmosphere; an oscillatory membrane having a piezoelectric material adapted to deflect the oscillatory membrane in response to an electrical signal; and a controller configured to control delivery of electrical signals to the piezoelectric material for controlling operation of the oscillatory membrane based on input data received from one or more sources that informs on a temperature and/or performance level of a targeted objected for cooling. The actuator may further include a thermal element for affecting modified temperature control; and the actuator may be integrated into a surface of a thermally diffusive structure for dissipating heat from a thermal load.