CPC B60L 58/26 (2019.02) [B60L 53/18 (2019.02); B64D 13/08 (2013.01); B64F 1/362 (2013.01); H02J 7/007194 (2020.01); B60L 2200/10 (2013.01); B64C 29/0008 (2013.01)] | 20 Claims |
1. A ground service system for an electric aircraft, the system comprising:
a charging module including a charging cable electrically connected to an energy source and configured to charge a battery of the electric aircraft;
a cooling module including a cooling channel configured to fluidly couple the electric aircraft to a first coolant source,
wherein the cooling module is configured to transmit a first coolant from the first coolant source and through the cooling channel to the electric aircraft to regulate a temperature of the battery;
a cabin soak module including a cabin soak channel configured to fluidly couple the electric aircraft and a second coolant source,
wherein the cabin soak module is configured to transmit a second coolant from the second coolant source through the cabin soak channel and into a cabin of the electric aircraft.
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