The invention relates to an aircraft having at least one dihydrogen delivery pipe, an embedded channel with lower grooves, an aeration orifice (610) for collecting outside air and at least one supply pipe (614) opening at an air inlet (602), a control unit, and a bypass box (601) for one or more lower grooves, the bypass tank has, for each lower groove, an inlet connected to a supply pipe (614) and an outlet connected to the lower groove, a door between each associated inlet and outlet that is alternately movable between an open position and a closed position, and a manipulation system for each door that is controlled by a control unit and moves the door. By this arrangement, the dihydrogen is automatically diluted even if the dihydrogen leaks into the embedded channel.

    本发明涉及一种飞行器,其具有至少一个二氢输送管、具有下沟槽的嵌入通道、收集外部空气的曝气孔口(610)和在进气口(602)处开口的至少一个供应管(614)、控制单元、以及对于一个或多个下沟槽的旁通箱(601),旁通箱对于每个下沟槽具有连接到供应管(614)的入口和连接到所述下沟槽的出口、在每个相关联的入口与出口之间的能够在打开位置与关闭位置之间交替运动的门、以及对于每个门的由控制单元控制并移动所述门的操纵系统。通过这种布置,即使在二氢泄漏到嵌入通道中的情况下,也会自动稀释二氢。


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    Titel :

    Aircraft having dihydrodelivery pipe, insertion channel for delivery pipe and aeration system for insertion channel


    Weitere Titelangaben:

    具有二氢输送管、用于该输送管的嵌入通道以及用于该嵌入通道的曝气系统的飞行器


    Beteiligte:
    CASTELLAN MAXIME (Autor:in) / JOBERT R ¨ (Autor:in) / MY (Autor:in)

    Erscheinungsdatum :

    2023-12-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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