The problem addressed by the present invention is that of enhancing the functionality and efficiency of a lightweight aircraft designed for use on short-haul routes. The technical effect to be achieved by the use of the invention is that of allowing the loading and unloading and the transport of different freight having maximum possible dimensions for this aircraft class. At the same time, maximum stiffness and strength of the fuselage and good aerodynamic properties of the aircraft are achieved.
RUMPF EINES LEICHTEN TRANSPORTFLUGZEUGS
FUSELAGE OF A LIGHTWEIGHT TRANSPORT AIRCRAFT
FUSELAGE D'UN AÉRONEF DE TRANSPORT LÉGER
2021-12-22
Patent
Electronic Resource
German
IPC: | B64C AEROPLANES , Flugzeuge |
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