An aircraft controlled by compressed air according to an embodiment of the present invention comprises: a fuselage (10) having main wings (20) on both sides thereof; a first nozzle (12) mounted to the roof of the fuselage (10); second nozzles (22) mounted on the top surfaces of the main wings (20); a first tank (31) disposed in the fuselage (10) or the main wings (20) and storing compressed air; and a main control valve (40) for controlling the compressed air so that the compressed air is provided to the first nozzle (12) or the second nozzles (22).
AIRCRAFT CONTROLLED BY COMPRESSED AIR
DURCH DRUCKLUFT GESTEUERTES FLUGZEUG
AÉRONEF COMMANDÉ PAR AIR COMPRIMÉ
2023-10-04
Patent
Elektronische Ressource
Englisch