The invention relates to an aircraft (1) equipped with a fuel battery (5) and a tailboom (4) bearing a shrouded rotor (10). The aircraft (1) comprises a cooling system (35) for said fuel battery (5). The cooling system (35) is equipped with a cooling circuit (40) in which heat transfer fluid (45) circulates. The cooling circuit (40) comprises a catchment duct (42) leading into or beside the fuel battery (5) and a heat exchanger (41) in fluid communication with said catchment duct (42). A ventilation system is equipped with at least an outlet opening (60) fitted in the shrouded rotor (10) to ventilate said heat exchanger (41) at least by aspiration depending on the direction of air flow (101).


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    Title :

    AERONEF MUNI D'UN SYSTEME DE REFROIDISSEMENT POUR UNE PILE A COMBUSTIBLE EMBARQUEE


    Additional title:

    AIRCRAFT PROVIDED WITH A COOLING SYSTEM FOR AN ONBOARD FUEL CELL
    LUFTFAHRZEUG MIT EINEM KÜHLSYSTEM FÜR EINE BORDSEITIGE BRENNSTOFFZELLE


    Contributors:

    Publication date :

    2024-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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