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.


    Access

    Download


    Export, share and cite



    Title :

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


    Contributors:

    Publication date :

    2020-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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 | European Patent Office | 2019

    Free access