A cooling system for an engine of an aircraft of a having hybrid-electric propulsion system including a nacelle body including a bottom cooling air intake disposed below a propeller hub for supplying air to an oil-air cooler, wherein the bottom cooling air intake includes a splitter dividing the bottom cooling air intake into a first channel and a second channel.


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    Title :

    COOLING SYSTEM CONFIGURATIONS FOR AN AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM


    Additional title:

    KÜHLSYSTEMKONFIGURATIONEN FÜR EIN FLUGZEUG MIT EINEM HYBRID-ELEKTRISCHEN ANTRIEBSSYSTEM
    CONFIGURATIONS DE SYSTÈME DE REFROIDISSEMENT POUR UN AÉRONEF AYANT UN SYSTÈME DE PROPULSION HYBRIDE-ÉLECTRIQUE


    Contributors:
    BECKER FRANK (author) / LATULIPE ERIC (author) / WANG XI (author)

    Publication date :

    2022-11-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    COOLING SYSTEM CONFIGURATIONS FOR AN AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM

    BECKER FRANK / LATULIPE ERIC / WANG XIAOQIN | European Patent Office | 2023

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    COOLING SYSTEM CONFIGURATIONS FOR AN AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM

    BECKER FRANK / LATULIPE ERIC / WANG XI | European Patent Office | 2020

    Free access

    COOLING SYSTEM CONFIGURATIONS FOR AN AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM

    BECKER FRANK / LATULIPE ERIC / WANG XI | European Patent Office | 2020

    Free access

    COOLING SYSTEM CONFIGURATIONS FOR AN AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM

    BECKER FRANK / LATULIPE ERIC / WANG XI | European Patent Office | 2020

    Free access

    Cooling system configurations for an aircraft having hybrid-electric propulsion system

    BECKER FRANK / LATULIPE ERIC / WANG XI | European Patent Office | 2022

    Free access