A cooling system is disclosed for cooling charge air in a turbocharged diesel internal combustion engine of an aircraft. The cooling system includes a charge air cooler, a charge air bypass valve, and a bypass valve actuator. The charge air cooler is fluidly coupled between the turbocharger assembly and the intake manifold, wherein the charge air cooler is configured to cool the charge air. The charge air bypass valve is moveable between a first position and a second position. The charge air bypass valve is configured to bypass the charge air cooler when in the second position. The bypass valve actuator is configured to move the charge air bypass valve between the first position and the second position.


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    Titel :

    Charge Air Cooler Bypass Systems and Methods


    Beteiligte:

    Erscheinungsdatum :

    2022-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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