A stator with cooling system for an electric motor of an electric aircraft and a method of manufacturing a stator of an electric motor for an electric aircraft with cooling system are disclosed. The stator may include a winding configured to provide magnetic flux and comprising an electrically conductive material. The stator may further include a soft magnet configured to hold the winding. The stator may further include a passive heat sink in thermal communication with the winding and comprising a phase change material.
STATOR WITH COOLING SYSTEM FOR AN ELECTRIC MOTOR OF AN ELECTRIC AIRCRAFT
10.07.2025
Patent
Elektronische Ressource
Englisch
STATOR WITH COOLING SYSTEM FOR AN ELECTRIC MOTOR OF AN ELECTRIC AIRCRAFT
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