A hybrid electric gas turbine engine includes a fan section having a fan, a turbine section having a turbine drivably connected to the fan through a main shaft that extends along a central longitudinal axis, a gas generating core extending along a first axis that is radially offset from the central longitudinal axis, and an electric motor drivably connected to the main shaft, wherein the electric motor is colinear with the main shaft.
Systems and methods for hybrid electric turbine engines
2022-12-06
Patent
Elektronische Ressource
Englisch
IPC: | 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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke |
SYSTEMS AND METHODS FOR HYBRID ELECTRIC GAS TURBINE ENGINES
Europäisches Patentamt | 2021
|Systems and methods for hybrid electric gas turbine engines
Europäisches Patentamt | 2022
|SYSTEMS AND METHODS FOR HYBRID ELECTRIC GAS TURBINE ENGINES
Europäisches Patentamt | 2022
|HYBRID ELECTRIC POWER FOR TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS
Europäisches Patentamt | 2024
|SYSTEMS AND METHODS FOR CONTROLLING NOISE IN AIRCRAFT POWERED BY HYBRID-ELECTRIC GAS TURBINE ENGINES
Europäisches Patentamt | 2023
|