A hybrid aerodynamic thrust system as a prime mover for aircraft or other high-speed vehicles. An arrangement of dual thrust resources to alternately accommodate low and high airspeed regimes. Electromotive force is used in lieu of hot section power turbines to achieve engine air compression or alternately perform thrust work at low velocities.
Hybrid gas turbine propulsion system
15.12.2015
Patent
Elektronische Ressource
Englisch
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / 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 |
Europäisches Patentamt | 2020
|Distributed hybrid propulsion system with turbine engine and aircraft
Europäisches Patentamt | 2023
|Cooling system in hybrid electric propulsion gas turbine engine
Europäisches Patentamt | 2020
|COOLING SYSTEM IN HYBRID ELECTRIC PROPULSION GAS TURBINE ENGINE
Europäisches Patentamt | 2019
|AIRCRAFT INCLUDING PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM
Europäisches Patentamt | 2018
|