A ventilation system for an aircraft having a structure bearing an exterior wall and an interior covering. At least one duct intended to be installed between the interior covering and the exterior wall. The duct includes one first pipe and at least one second pipe which is able to slide telescopically in relation to the first pipe between a retracted position and an extended position.


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    Title :

    Aircraft ventilation system


    Contributors:

    Publication date :

    2016-11-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16L PIPES , Rohre / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F24F Klimatisierung , AIR-CONDITIONING



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