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
25.04.2024
Patent
Elektronische Ressource
Englisch
Aircraft electric motor having a stator heat pipe cooling scheme
Europäisches Patentamt | 2024
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