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
PARALLELHYBRIDKRAFTWERK MIT MANTELSTROMTRIEBWERKKERN
GROUPE MOTOPROPULSEUR HYBRIDE PARALLÈLE ÉQUIPÉ D'UN COEUR DE MOTEUR À TURBINES
2024-11-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen |
Turbofan/Turboshaft Powerplant for Composite Helicopters
SAE Technical Papers | 1967
|Seperated core turbofan engine
TIBKAT | 1996
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