公开(公告)号：US10150570B2

公开(公告)日：2018-12-11

申请号：US14965926

申请日：2015-12-11

Applicant: AIRBUS SAS

Inventor： Emmanuel Joubert ,  Benoit Ferran ,  Antonin Sanitas

IPC: B64D33/08 ,  H01M10/625 ,  H01M10/6563 ,  B64D27/24 ,  B64D33/10

Abstract: 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.