An aircraft with a fuselage that defines at least an interior region and a drive system accommodating region, the drive system accommodating region being arranged inside the fuselage and comprising at least one fire protection zone that is defined by at least one associated firewall arrangement, the at least one fire protection zone accommodating at least one engine within the at least one associated firewall arrangement such that the associated firewall arrangement defines a fire-resistant separation between the at least one engine and the interior region of the fuselage, wherein the at least one associated firewall arrangement comprises at least one air duct for ducting a hot air flow that is generated in operation of the aircraft independent from heat generation of the at least one engine.


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    Titel :

    AIRCRAFT WITH A FUSELAGE THAT DEFINES AT LEAST AN INTERIOR REGION AND A DRIVE SYSTEM ACCOMMODATING REGION


    Beteiligte:
    MORES SEBASTIAN (Autor:in) / LOESER FRANK (Autor:in) / FRESE JOHANNES (Autor:in) / BRAEUTIGAM RALF (Autor:in) / WEHLE CHRISTIAN (Autor:in)

    Erscheinungsdatum :

    2016-08-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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