System for protecting an outer surface of an aircraft comprising at least two fuel cells (112, 212) from icing, characterized in that it comprises a first and a third liquid circuit (114, 214) each causing a cooling liquid of the fuel cells (112, 212) to flow, a second and a fourth liquid circuit (118a, 118b) each causing an icing protection liquid to flow, at least two icing protection heat exchangers (120a-d, 220a-d) arranged on the outer surface of the aircraft and having each icing protection liquid pass through them when it flows in the second or fourth liquid circuit (118a, 118b), and two liquid-liquid heat exchangers (116, 216) in which the cooling liquids form a hot pass and the icing protection liquids form a cold pass to reheat the icing protection liquid by the heat from the cooling liquids.


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    Titel :

    SYSTÈME DE PROTECTION GIVRAGE À PILE À COMBUSTIBLE


    Weitere Titelangaben:

    SYSTEM FOR PROTECTING A FUEL CELL FROM ICING
    SYSTEM ZUM SCHUTZ EINER BRENNSTOFFZELLE VOR VEREISUNG


    Beteiligte:
    PRINCE KARINE (Autor:in) / LAVERGNE DAVID (Autor:in)

    Erscheinungsdatum :

    16.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

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



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