A fluid tank for integration into a structure of an unmanned aircraft includes a shell having a first axial wall, an oppositely arranged second axial wall, an upper side, a lower side, and an enclosed interior, at least one receiving chamber in the interior for storing fluid, and a collection chamber, which is arranged on the lower side and which is fluidically connected to the at least one receiving chamber. The collection chamber includes a bottom surface, through which there extends a drain, wherein a covering surface is arranged above the bottom surface and covers at least a portion of the collection chamber. At least one flow opening could be arranged on an upper side of the collection chamber, which flow opening allows gas bubbles to escape in the direction of the upper side of the fluid tank.


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    Title :

    FLUIDTANK ZUR INTEGRATION IN EINE STRUKTUR EINES UNBEMANNTEN FLUGGERÄTS


    Additional title:

    FLUID TANK FOR INTEGRATION INTO A STRUCTURE OF AN UNMANNED AIRCRAFT
    RÉSERVOIR DE FLUIDE DESTINÉ À ÊTRE INTÉGRÉ DANS UNE STRUCTURE D'UN AÉRONEF SANS PILOTE


    Contributors:

    Publication date :

    2022-08-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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