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.

    L'invention concerne un aéronef hybride (1) du type sans pilote, configuré pour permettre l'utilisation conjointe optimisée de la force aérostatique et de la force aérodynamique, comprenant un corps gonflable (10) présentant une coque externe (11) et une structure porteuse (20) à l'intérieur de ladite coque externe (11), ledit corps gonflable (10) étant conçu pour adopter une configuration de fonctionnement à aile fermée.


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    Title :

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE


    Additional title:

    AÉRONEF GONFLABLE HYBRIDE DU TYPE SANS PILOTE



    Publication date :

    2022-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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