METHOD FOR TREATMENT OF WORKING SURFACES OF PARTS OF BLADED MACHINES

FIELD: technological processes.SUBSTANCE: invention relates to material science, particularly to methods of sputtering of heat shielding coating, and can be used in aircraft building and other fields of industry in production of parts of turbine engines and plants. Procedure for application of heat shielding coating on working surfaces of parts of blade machine includes application of plasma sputtering onto a prepared surface of parts from nickel-based alloy coating out of zirconium oxide stabilised by yttrium, wherein coating is created in it gradient transition layer by means of two magnetrons, wherein by means of first magnetron is sputtered a first target from nickel-based alloy, which corresponds to composition of alloy parts, and by second magnetron is sputtered a second target made of zirconium with additives of stabilising element yttrium, wherein sputtering of first target is carried out in an argon atmosphere so that intensity of atomic stream formed from first target exceeds intensity of atomic stream formed from second target, after formation of solid metal layer oxygen is fed into working chamber of sputtered coating zirconium oxide, during deposition of partial oxygen pressure is smoothly increased to 1.5*10Pa and first power of magnetron is decreased until its complete disconnection, sputtering is continued until formation of zirconium oxide stabilised by yttrium, required thickness to produce nanostructured coating containing metal phase with composition corresponding to composition of alloy protected surface part, and phase of zirconium oxide stabilised by yttrium, with increasing of part surface fraction phase of zirconium oxide.EFFECT: use of disclosed method is aimed at formation of smooth transition from metallic material to oxide without interphase boundaries of macroscopic size, which enables to form on working surfaces of parts coating, having sufficiently high value of adhesion and cohesion.1 cl Изобретение относится к области материаловедения, в частности к способам напыления теплозащитных покрытий, и может найти применение в авиастроении и других областях машиностроения при производстве деталей турбинных двигателей и установок. Способ нанесения теплозащитного покрытия на рабочие поверхности детали лопастной машины включет нанесение плазменным напылением на предварительно подготовленные поверхности детали из сплава на основе никеля покрытия из оксида циркония, стабилизированного иттрием, причем нанесение покрытия осуществляют созд