A hybrid aircraft powerplant includes a turbine engine having a first shaft configured to output power from the turbine engine, a bypass fan, and an electric machine. The hybrid aircraft powerplant further includes a first mechanism configured to selectively engage the first shaft with a second shaft connected to the electric machine such that the power is output from the turbine engine to the electric machine. The hybrid aircraft powerplant further includes a second mechanism configured to selectively engage the first shaft with a third shaft connected to the bypass fan to output the power from the turbine engine to the bypass fan.
PARALLEL HYBRID POWERPLANT WITH TURBOFAN ENGINE CORE
31.10.2024
Patent
Elektronische Ressource
Englisch
Parallel hybrid power device with turbofan engine core
Europäisches Patentamt | 2024
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