A thermal management system for electric aircraft is disclosed, designed to control the temperature of battery packs during the charging process. The system includes a thermal conditioning system for maintaining coolant at a first temperature, a coolant circulator for transferring the coolant between the thermal conditioning system and the aircraft, and a temperature adjuster for blending coolant flows to achieve a desired combined temperature. A control unit receives battery temperature information and adjusts the temperature adjuster accordingly. The system can operate in various modes, including cooling, heating, or variable temperature modes, based on target temperature parameters. The system is further configured to transition between modes in response to the battery pack's thermal requirements during charging.
TEMPERATURE REGULATED COOLANT SYSTEM FOR ELECTRIC VEHICLES
31.07.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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