ELECTRICAL POWERING OR DRIVE SYSTEM FOR A MOTOR IN AN ELECTRICALLY DRIVEN AIRCRAFT
This disclosure describes at least embodiments of a power management system for an electric or hybrid aircraft. The system can include a first motor and a second motor supported by a housing of the aircraft. The first motor can be powered by a first battery pack, and the second motor can be powered...
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Format: | Patent |
Sprache: | eng ; fre |
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