HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

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) be...

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Bibliographic Details
Main Authors BARANIELLO, Vincenzo Rosario, BORSA, Roberto, PERSECHINO, Giuseppe
Format Patent
LanguageEnglish
Published 27.07.2023
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary: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.
Bibliography:Application Number: AU20220217503