| CPC B64U 10/25 (2023.01) [B64C 39/062 (2013.01); B64U 10/30 (2023.01); B64U 50/13 (2023.01); B64B 2201/00 (2013.01); B64U 30/10 (2023.01); B64U 50/31 (2023.01); B64U 2101/20 (2023.01)] | 12 Claims |

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1. A hybrid aircraft of the unmanned type, configured for joint and optimized use of aerostatic and aerodynamic force, comprising an inflatable body including an outer shell and a load-bearing structure inside said outer shell, said inflatable body being adapted to take a closed wing operating configuration;
wherein in said closed wing operating configuration, said inflatable body comprises a first arched portion adapted to define an arched wing having a leading edge and a trailing edge, a second straight portion adapted to define a straight wing having a leading edge and a trailing edge, a third and a fourth connecting portion arranged at opposite ends of the straight wing, which are adapted to join said arched wing and said straight wing to each other, wherein said load-bearing structure is an annular structure which extends through said arched wing, said straight wing and said third and fourth connecting portions;
wherein said load-bearing structure comprises at least one main annular spar;
wherein said at least one main spar is an inflatable spar.
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