The present application discloses an aircraft. The aircraft comprises a first wing and a second wing, a fuselage to which the first wing and the second wing are mounted, a first engine operatively mounted to the first wing, and a second engine operatively mounted to the second wing. The aircraft is configured to vertically take-off and land. The first engine and the second engine are used for both (i) vertical take-off and landing, and (ii) horizontal flight
DUAL ENGINE VERTICAL TAKE OFF AND LANDING COLLAPSIBLE FIXED WING AIRCRAFT
2024-08-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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