The present invention relates to a tank system (150) comprising: a tank (152); a discharge line (160) fixed in a bottom portion of the tank (152) and having a discharge port (162) at each end; a funnel portion (164) for each discharge port (162) having a wall through which at least one window (166) passes; a body (172) that is translationally movable; for each funnel portion (164), a plug (170) secured to the body (172) and arranged to be movable inside said funnel portion (164) between an open position and a closed position; and an arm (174) having a first end (174a) hingedly mounted on the top portion of the tank (152) and a second end (174b) hingedly mounted on the main body (172). Such a tank system is particularly robust during operation by means of the pendulum action of the arm.

    本发明涉及一种储罐系统(150),其包括:储罐(152);排放管线(160),其固定在储罐(152)的底部部分中,并在每一端处具有排放端口(162);对于每个排放端口(162)而言的漏斗部(164),其具有壁,至少一个窗口(166)穿过该壁;主体(172),其能平移运动;对于每个漏斗部(164)而言的塞件(170),其固定到主体(172)并布置成能在所述漏斗部(164)内部在打开位置与关闭位置之间运动;以及臂(174),其第一端(174a)以铰接方式安装在储罐(152)的顶部部分,其第二端(174b)以铰接方式安装在主体(172)上。借助臂的摆锤作用,这样的储罐系统在运行中尤其稳健。


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    Titel :

    Tank system having valve in form of pendulum system


    Weitere Titelangaben:

    具有摆锤系统形式的阀的储罐系统


    Beteiligte:
    ANDREAU THOMAS (Autor:in) / MILIERI JOHN (Autor:in) / LAVIGNE JAMES (Autor:in) / LANDOLT J ¨ 1 RGEN (Autor:in)

    Erscheinungsdatum :

    26.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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