Aircraft having a hybrid power source with power generation sources controlled according to drive unit power requirements
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United States of America Patent
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May 21, 2024
Grant Date -
Dec 14, 2023
app pub date -
Jan 4, 2022
filing date -
Jan 6, 2021
priority date (Note) -
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Abstract
An aircraft having a hybrid power source includes two horizontal drive units, four vertical drive units, a vertical drive unit comprising a power supply bus the output of which may be connected to a single horizontal drive unit which may be connected to at least two vertical drive units via a switch, two power generation sources connected, on the one hand, to each of the power supply buses by a respective input of the corresponding vertical drive unit and, on the other hand, to each horizontal drive unit via the respective output of each vertical drive unit, and a power supply command arranged to send a power command to the power generation sources according to the power requirements of the vertical drive units and/or horizontal drive units. The power generation sources are also suitable for recharging power sources of the vertical drive units.
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