An aircraft-mountable inflow and outflow apparatus has an accumulating sleeve, an inflow line and at least one exit opening. The regulating sleeve has an entry opening. The inflow line has a supply-line connection for a respective supply line. The accumulating sleeve forms a first supply-line portion, is designed for insertion into a respective shaft of the respective inflow and outflow apparatus and is dimensioned such that, in a state in which the insert has been inserted into the respective shaft, the entry opening of the accumulating sleeve is located in the vicinity of an opening between a respective head part and the respective shaft of the respective inflow and outflow apparatus. Furthermore, the accumulating sleeve is connected to the supply-line connection for a respective supply line via the entry line, which constitutes a second supply-line portion.


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    Title :

    INSERT FOR AN INFLOW AND OUTFLOW APPARATUS


    Contributors:
    HOFF AXEL (author)

    Publication date :

    2017-09-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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