The present invention is a double wing aircraft with two fixed wings embodied as either a flying wing configuration or a double wing configuration having a fuselage with smaller external dimensions, larger airlifting area, thinner airfoils, and lighter airframe relative to prior art that altogether is resulting with lower drag, fuel consumption, harmful emissions, and noise, as well as higher speed and flight safety, longer range, and shorter runway when compared to prior art.
DOUBLE WING AIRCRAFT
DOPPELFLÜGELIGES FLUGZEUG
AÉRONEF À DEUX AILES
2024-08-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |