Airbus (sas)

Airbus Group Sas

Airbus Corporation

Antonin Sanitas

Emmanuel Joubert

Benoit Ferran

Benoît Ferran

Germain Morin

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.

Device and method for cooling at least one autonomous electric power source of an aircraft

The aircraft () includes: at least one electric motor (); at least one stand-alone electrical power supply () supplying power to the electric motor; propulsion elements () referred to as 'auxiliary propulsion elements', included in the group including: a stand-alone electrical power supply () supplying power to the electric motor, a power supply converting thermal energy into electrical energy and supplying power to the electric motor, and an internal combustion engine; and a structure () configured to integrate each electric motor, each stand-alone electrical power supply and the auxiliary propulsion elements, the parameters of the structure being substantially identical regardless of the auxiliary propulsion elements. A method of fitting out such an aircraft is also described.

Aircraft and method of fitting out such an aircraft

Growing community of inventors

Sollies-Pont, France

Antonin Sanitas