Described herein is an aircraft that includes a fuselage with a higher portion and a lower portion. The aircraft also includes two fixed wings that are coupled to and extend from opposing sides of the lower portion of the fuselage. Additionally, the aircraft includes a tilt-rotor assembly that is coupled to each of the two fixed wings.
TILT-ROTOR VERTICAL-LIFT AIRCRAFT
31.12.2015
Patent
Elektronische Ressource
Englisch
Electric vertical take-off and landing tilt rotor aircraft
Europäisches Patentamt | 2025
|