AIRCRAFT HAVING A HYBRID POWER SOURCE
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United States of America
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Apr 10, 2025
app pub date -
Apr 13, 2023
filing date -
Apr 13, 2023
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Abstract
An aircraft having a hybrid power source includes horizontal drive thrusters powered by an electric motor and forming a horizontal drive unit, vertical take-off/landing rotors forming with electric motors and a corresponding stored electrical energy source a vertical drive unit comprising an electric power supply bus, power generation sources connected to the electric power supply buses and by an input of a vertical drive unit and to each horizontal drive unit via an output of each vertical drive unit. The electric power supply controller emits a power command to the power generation source according to power requirements of the vertical and/or horizontal drive units. The stored electrical energy sources supply electricity according to the difference between the power requirements of the vertical and/or horizontal drive units. The power generation source recharges the stored electrical energy sources, so that the stored electrical energy sources are passively controlled.
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