An aircraft thermal management system comprising a high temperature loop and a low temperature loop. The high temperature loop is configured to manage a temperature of a fuel cell stack in a nacelle using a nacelle heat exchanger. The low temperature loop is configured to cool a number of heat loads in a nacelle using a heat capacity of liquid hydrogen.


    Access

    Download


    Export, share and cite



    Title :

    FUEL CELL AIRCRAFT THERMAL MANAGEMENT SYSTEM


    Additional title:

    WÄRMEVERWALTUNGSSYSTEM FÜR EIN BRENNSTOFFZELLENFLUGZEUG
    SYSTÈME DE GESTION THERMIQUE D'AÉRONEF À PILE À COMBUSTIBLE


    Contributors:

    Publication date :

    2025-02-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Fuel Cell Aircraft Thermal Management System

    BALAN CHELLAPPA / STOIA MICHAEL F / AGUILAR CHARLES et al. | European Patent Office | 2025

    Free access

    FUEL CELL AIRCRAFT THERMAL MANAGEMENT SYSTEM

    CHELLAPPA BALAN / MICHAEL F STOIA / CHARLES AGUILAR et al. | European Patent Office | 2025

    Free access

    Fuel cell aircraft thermal management system

    BARAN CHELLAPPAN / STOIA MICHAEL F / AGUILAR CHARLES et al. | European Patent Office | 2025

    Free access

    Improving Aircraft Fuel-Thermal Management

    Hitzigrath, Richard W. | SAE Technical Papers | 1993


    Integrated Aircraft Fuel Thermal Management

    Levin, Mark L. / Hudson, William A. | SAE Technical Papers | 1986