Electric Driver for aeronautical applications

The invention relates to a stranded electrical conductor comprising at least one strand made of aluminum or aluminum alloy core (10, 20, 30, 40A, 50A) and a plurality of conductive strands (11, 21, 31, 41, 51) arranged in at least one layer around the core strand. According to the invention, the ratio between the diameter of said core wire made of aluminum or aluminum alloy and the diameter of said peripheral conductive strands is strictly greater than 1.