A device for cooling at least one autonomous electric power source of an aircraft, includes: an inlet for air cooling a cooling fluid; the cooling fluid being fed towards at least one autonomous electric power source of the aircraft; a convergent hot air outlet, including moving elements for controlling the air flowrate; and supervision elements of the aircraft, which control the moving elements for controlling the air flowrate depending on the need for cooling of the autonomous electric power source. A method for cooling at least one autonomous electric power source of an aircraft and an aircraft including such a device are also described.
Dispositif et procédé de refroidissement d'au moins une source d'alimentation électrique autonome d'un aéronef
Device and method for cooling at least one autonomous power source of an aircraft
Vorrichtung und Verfahren zur Kühlung mindestens einer autonomen Stromversorgungsquelle eines Luftfahrzeugs
2020-06-10
Patent
Electronic Resource
French
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