Blade for a turbine engine, and associated turbine engine

A blade for a turbine engine, comprising:

• an aerodynamic airfoil extending radially outwards,
• a blade tip,
• a blade root, and
• a platform connected to the root by an upper end, a maximum radial distance between the blade tip and the platform defining a maximum extent of the bearing surface of the airfoil, wherein the blade is partially covered by a protective strip configured to combat oxidation and corrosion, said strip extending between a lower limit situated on at least one portion of the platform and an upper limit situated on the blade root, the blade tip not being covered with the protective strip or any other coating, wherein the protective strip is made of material selected from the group consisting of aluminum, iron, nickel, cobalt, yttrium, rare earths or precious metals.