A fairing assembly (114A) for an aerial vehicle (100) having a tank (202) that forms a body (110) of the vehicle and a wing (112) coupled to the tank is provided. The fairing assembly includes a substructure (164) configured to couple with a tank skin (378) of the tank, a thermal protection system (190) coupled to the substructure, and a seal assembly (192) coupled to the substructure, the seal assembly being configured to overlap at least a portion of an edge (118) of the wing.


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    Titel :

    ОБТЕКАТЕЛЬНЫЙ УЗЕЛ И СПОСОБ ДЛЯ НЕГО


    Erscheinungsdatum :

    25.11.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge