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).
AERONEF MUNI D'UN SYSTEME DE REFROIDISSEMENT POUR UNE PILE A COMBUSTIBLE EMBARQUEE
AIRCRAFT PROVIDED WITH A COOLING SYSTEM FOR AN ONBOARD FUEL CELL
LUFTFAHRZEUG MIT EINEM KÜHLSYSTEM FÜR EINE BORDSEITIGE BRENNSTOFFZELLE
2024-05-29
Patent
Electronic Resource
French
AERONEF MUNI D'UN SYSTEME DE REFROIDISSEMENT POUR UNE PILE A COMBUSTIBLE EMBARQUEE
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