A power control device is provided for an aircraft. The power control device may include at least one first battery, a second battery having a lower power density and higher energy density than the at least one first battery, at least one lift motor connected, via a first electrical path, to the at least one first battery, a cruise motor connected, via a second electrical path, to the second battery, and a power control circuit configured to control the at least one first battery, the second battery, the at least one lift motor, and the cruise motor.
APPARATUS FOR CONTROLLING POWER
VORRICHTUNG ZUR LEISTUNGSREGELUNG
APPAREIL DE COMMANDE DE PUISSANCE
30.10.2024
Patent
Elektronische Ressource
Englisch
POWER-TRAIN CONTROLLING APPARATUS AND METHOD OF CONTROLLING POWER TRAIN
Europäisches Patentamt | 2020
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