Developing the modification of nickel cathodes for applying the ion-plasma coatings on the parts of aircraft engines

Abstract

surface to the high-temperature effects of the oxidative environment [1, 2] as the destruction of a turbine's blades mostly originates from the surface. One of the main ways to improve the resistance of blades to various types of hot corrosion is to 1. Introduction The operational reliability of the gas turbine engine (GTE) blades depends primarily on the resistance of the MATERIALS SCIENCE