A hybrid propulsion system for use with an aircraft includes a gas turbine engine, at least one propulsor, and an electric power system. The electric power system is coupled to the gas turbine engine to generate electrical energy and the propulsor to provide electrical energy to drive the propulsor. The electric power system includes a thermal management system configured to cool a heat load generated by the electric power system.


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    Title :

    Aircraft hybrid propulsion system including cold plate for a high density power converter



    Publication date :

    2023-11-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    COLD PLATE FOR HIGH DENSITY POWER CONVERTER

    SIVALINGAM KRISHNAMOORTHI / GAJANAYAKE CHANDANA J / KUMARAVEL JEYARAMAN et al. | European Patent Office | 2022

    Free access




    HYBRID AIRCRAFT PROPULSION POWER PLANTS

    DUBREUIL JEAN / ULLYOTT RICHARD | European Patent Office | 2020

    Free access