The present application discloses an aircraft. The present application discloses a method of assembling or disassembling an aircraft. The assembly method includes mounting a first engine nacelle to a first wing, mounting a second engine nacelle to a second wing, causing the first wing to be extended relative to a fuselage mount, causing the second wing to be extended relative to the fuselage mount, and mounting the fuselage to the fuselage mount.
DISSASSEMBLY FOR DUAL ENGINE VERTICAL TAKE OFF AND LANDING COLLAPSIBLE FIXED WING AIRCRAFT
08.08.2024
Patent
Elektronische Ressource
Englisch
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