An auxiliary power unit assembly for an aircraft, including an engine assembly including an internal combustion engine, a first duct in fluid communication with an inlet of the internal combustion engine and configured to be in fluid communication with an environment of the aircraft, and a second duct configured to be in fluid communication with the environment. The second duct may be in fluid communication with an inlet of a compressor drivable by the internal combustion engine or with a compartment receiving the engine assembly. A filter extends across the first duct. The filter is removable from the first duct through an opening in a wall of the first duct, the opening accessible from an exterior of the engine assembly.


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    Titel :

    AUXILIARY POWER UNIT ASSEMBLY WITH REMOVABLE INLET FILTER


    Weitere Titelangaben:

    DISPOSITIF DE MODULE D'ALIMENTATION AUXILIAIRE DOTE D'UN FILTRE D'ENTREE AMOVIBLE


    Beteiligte:
    DIONNE LUC (Autor:in) / VILLENEUVE BRUNO (Autor:in) / COURTOIS MAXIME (Autor:in) / HAGSHENAS BEHZAD (Autor:in) / JULIEN ANDRE (Autor:in)

    Erscheinungsdatum :

    14.04.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02M Zuführen von Brennstoff-Luft-Gemischen oder deren Bestandteilen bei Brennkraftmaschinen allgemein , SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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