There is provided a supercharging system for an aircraft reciprocating engine, comprising: a plurality of compressors for supplying compressed air to the aircraft reciprocating engine; at least one turbine for obtaining rotational power for at least one of the plurality of compressors, and a plurality of motors for respectively providing rotational power to the plurality of compressors. An object of the present invention is to reduce turbo lag in a reciprocating engine for an aircraft in which multiple-stage supercharging is performed by the turbocharger.


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    Titel :

    SUPERCHARGING SYSTEM FOR AIRCRAFT RECIPROCATING ENGINE, AIRCRAFT RECIPROCATING ENGINE, AND AIRCRAFT


    Beteiligte:
    KOTANI KAZUAKI (Autor:in) / NAKAZATO NOBUYUKI (Autor:in) / MURATA IWAO (Autor:in)

    Erscheinungsdatum :

    2019-09-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Supercharging system for aircraft reciprocating engine, aircraft reciprocating engine, and aircraft

    KOTANI KAZUAKI / NAKAZATO NOBUYUKI / MURATA IWAO | Europäisches Patentamt | 2020

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