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.


    Access

    Download


    Export, share and cite



    Title :

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE



    Publication date :

    2024-09-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Unmanned hybrid inflatable aircraft

    PERSECCHINO GIUSEPPE / BALANIERO VINCENZO ROSARIO / BORSA ROBERTO | European Patent Office | 2023

    Free access

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

    PERSECHINO GIUSEPPE / BARANIELLO VINCENZO ROSARIO / BORSA ROBERTO | European Patent Office | 2024

    Free access

    Hybrid inflatable aircraft of the unmanned type

    PERSECHINO GIUSEPPE / BARANIELLO VINCENZO ROSARIO / BORSA ROBERTO | European Patent Office | 2025

    Free access

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

    PERSECHINO GIUSEPPE / BARANIELLO VINCENZO ROSARIO / BORSA ROBERTO | European Patent Office | 2023

    Free access

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

    PERSECHINO GIUSEPPE / BARANIELLO VINCENZO ROSARIO / BORSA ROBERTO | European Patent Office | 2022

    Free access