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
2015-12-31
Patent
Electronic Resource
English
Electric vertical take-off and landing tilt rotor aircraft
European Patent Office | 2025
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