An inlet assembly for an auxiliary power unit for an aircraft, including a particle separator and a plenum having first and second inlets. A first duct configured to deliver air to an engine of the auxiliary power unit is in fluid communication with an outlet of the plenum. A second duct configured to deliver air to a compartment containing the auxiliary power unit is in fluid communication with the outlet of the plenum. The assembly is selectively configurable between a first configuration where the plenum is in fluid communication with the environment of the aircraft through the second inlet and through the particle separator, and a second configuration where the plenum is in fluid communication with the environment of the aircraft through the first inlet independently of the particle separator. An auxiliary power unit assembly and a method of feeding air to an auxiliary power unit assembly are also discussed.


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    Titel :

    AUXILIARY POWER UNIT INLET ASSEMBLY WITH PARTICLE SEPARATOR


    Weitere Titelangaben:

    HILFSAGGREGATEINLASSANORDNUNG MIT PARTIKELABSCHEIDER
    ENSEMBLE D'ENTRÉE D'UNITÉ DE PUISSANCE AUXILIAIRE AVEC SÉPARATEUR DE PARTICULES


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

    Erscheinungsdatum :

    25.11.2020


    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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