HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

A hybrid aircraft of the unmanned type configured for joint and optimized use of aerostatic and aerodynamic force is provided. The hybrid aircraft 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 wi...

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Bibliographic Details
Main Authors BARANIELLO, Vincenzo Rosario, BORSA, Roberto, PERSECHINO, Giuseppe
Format Patent
LanguageEnglish
Published 29.02.2024
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
LIGHTER-THAN AIR AIRCRAFT
PERFORMING OPERATIONS
TRANSPORTING
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Summary:A hybrid aircraft of the unmanned type configured for joint and optimized use of aerostatic and aerodynamic force is provided. The hybrid aircraft 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.
Bibliography:Application Number: US202218263757