BRANDSCHUTZWAND, DIE EINE ANSCHLUSSVORRICHTUNG EINER KANALISATION SOWIE EIN WÄRMESCHUTZSCHILD UMFASST, UND LUFTFAHRZEUG, DAS MINDESTENS EINE SOLCHE BRANDSCHUTZWAND UMFASST

摘要

The invention relates to an aircraft firewall separating a first zone (52.1) corresponding to a fire zone and a second zone (52.2). The fire wall (54) comprises a tubular body (60) made of a thermally conductive material, straddling either side of the fire wall (54), and at least one heat shield (70), positioned in the first zone (52.1), covering the tubular body (60) while being spaced from said tubular body (60) so as to create an air space (72) between the heat shield (70) and the tubular body (60 ). This configuration slows the spread of heat towards the second zone (52.2).