AIRCRAFT PART OF A COMPOSITE MATERIAL WITH PROTECTION AGAINST THE EFFECTS OF ALUMINUM LIGHTNING.

摘要

The invention relates to an aircraft structural component formed of a structural part made of a composite material based on carbon fibers, which comprises on one side of this structural part, at least on one side of the part likely to be subjected to to lightning strikes, a network of electrically conductive elements. These elements are in direct contact with the structural part of the composite material of the part, over substantially their entire surface. They are formed of aluminum or aluminum alloy and they have on the surface a corrosion protection layer resulting from a surface treatment by an anodizing step followed by at least one, preferably two, clogging steps.