An aircraft includes a fuselage extending along a first x-axis and a wing assembly including a first wing an a second wing. A first power assembly of the aircraft includes a first propulsion element and a first electric motor while a second power assembly includes a second propulsion element and a second electric motor. The aircraft further includes a third power assembly positioned aft of the first power assembly and the second power assembly. The third power assembly includes a third propulsion element and an internal combustion engine.
Hybrid aircraft and landing launch/recovery system
20.05.2025
Patent
Elektronische Ressource
Englisch
Launch and recovery electrical control system of aircraft landing gear
Europäisches Patentamt | 2015
|METHOD FOR LANDING A TETHERED AIRCRAFT AND LAUNCH AND LAND SYSTEM
Europäisches Patentamt | 2020
|