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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    Title :

    ОБТЕКАТЕЛЬНЫЙ УЗЕЛ И СПОСОБ ДЛЯ НЕГО


    Publication date :

    2019-11-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge