An aircraft engine system configured with a high pressure stage turbocharger assembly and a supplemental stage turbocharger assembly disposed in series with respect to said high pressure stage turbocharger, wherein the supplemental stage turbocharger assembly provides a compressor unit of the high pressure stage turbocharger with substantially constant critical altitude pressure input.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Multistage turbocharging system for providing constant original critical altitude pressure input to high pressure stage turbocharger


    Beteiligte:
    FASS YEHUDA (Autor:in) / FELDMAN JACOB (Autor:in)

    Erscheinungsdatum :

    09.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02B INTERNAL-COMBUSTION PISTON ENGINES , Brennkraftmaschinen mit innerer Verbrennung mit Verdrängerwirkung / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    TCX - the new high pressure turbocharger for two stage turbocharging

    Klima,J. / Hort,V. / Haidn,M. et al. | Kraftfahrwesen | 2013


    MULTISTAGE TURBOCHARGING SYSTEM

    FASS YEHUDA / FELDMAN JACOB | Europäisches Patentamt | 2018

    Freier Zugriff

    Turbocharger and Turbocharging 82

    Garrett,K. / Garrett,US. / Holset,US | Kraftfahrwesen | 1982



    Constant-pressure turbocharging for medium-speed four stroke engines

    Schnurbein,E.von / MAN,Augsburg | Kraftfahrwesen | 1978