The present application relates essentially to a fixed-wing aircraft made up of a fuselage (02) in the shape of an aerofoil with four wings (10) having the same aerofoil shape with aerodynamic wing behaviour contributing to the lift and minimizing the drag of the aircraft, allowing it to have a larger payload and longer flight range.
Vertical-take-off aerial vehicle with aerofoil-shaped integrated fuselage and wings
19.07.2023
Patent
Elektronische Ressource
Englisch
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