An electrical power supply device in an aircraft, the device including an enclosure, the enclosure containing at least: a fuel cell; a dihydrogen generator; a gas feed circuit connecting the dihydrogen generator to the anode of the fuel cell; an oxygen feed device feeding the cathode of the fuel cell; and a cooling circuit of the fuel cell associated with at least one heat exchanger; wherein the enclosure is mounted on an actuator system, the actuator system being configured to move the enclosure from a first position in which the enclosure is housed inside an outer wall of the aircraft, to a second position in which the enclosure projects from the outer wall.
DISPOSITIF D'ALIMENTATION EN ENERGIE DANS UN AERONEF ET PROCEDE DE REFROIDISSEMENT DE CE DISPOSITIF
DEVICE FOR SUPPLYING ENERGY IN AN AIRCRAFT AND METHOD FOR COOLING THIS DEVICE
VORRICHTUNG ZUR ENERGIEVERSORGUNG IN EINEM FLUGZEUG UND VERFAHREN ZUR KÜHLUNG DIESER VORRICHTUNG
05.08.2020
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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