A hybrid aircraft of the unmanned type configured for joint and optimized use of aerostatic and aerodynamic force has an inflatable body having an outer shell and a load-bearing structure inside the outer shell, the inflatable body being adapted to assume a closed wing operating configuration.
HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE
HYBRIDES AUFBLASBARES FLUGZEUG DES UNBEMANNTEN TYPS
AÉRONEF GONFLABLE HYBRIDE DU TYPE SANS PILOTE
2023-12-13
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |