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
2024-10-31
Patent
Electronic Resource
English
Turbofan/Turboshaft Powerplant for Composite Helicopters
SAE Technical Papers | 1967
|Seperated core turbofan engine
TIBKAT | 1996
|