There is described a hybrid aircraft (1) of the unmanned type, configured for the joint and optimized use of aerostatic and aerodynamic force, comprising an inflatable body (10) including an outer shell (11) and a load-bearing structure (20) inside said outer shell (11), said inflatable body (10) being adapted to assume a closed wing operating configuration.
HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE
2024-09-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |