A drive system of at least one rotor of an aircraft via electrical energy in addition to or as a replacement of a mechanical system. The electrical energy is provided at least in part by at least one device for recovering thermal energy from hot gases of an internal combustion engine of the aircraft.
Aircraft propulsion architecture integrating an energy recovery system
06.02.2018
Patent
Elektronische Ressource
Englisch
Architecture Examples for Electrified Propulsion Aircraft
SAE Technical Papers | 2022
Hybrid propulsion architecture and aircraft containing such an architecture
Europäisches Patentamt | 2024
|HYBRID PROPULSION ARCHITECTURE AND AIRCRAFT CONTAINING SUCH AN ARCHITECTURE
Europäisches Patentamt | 2022
|FAULT-TOLERANT POWER SYSTEM ARCHITECTURE FOR AIRCRAFT ELECTRIC PROPULSION
Europäisches Patentamt | 2021
|FAULT-TOLERANT POWER SYSTEM ARCHITECTURE FOR AIRCRAFT ELECTRIC PROPULSION
Europäisches Patentamt | 2021
|