Protective coatings for aeronautic and power generation turbines components deposited by plasma spray

Coatings produced by aluminium diffusion, called aluminide are employed to increase the oxidation and corrosion resistance, increasing the life of Ni and Co base superalloys components at temperatures comprised between 900 and 1050 degrees C. Consequently these coatings are frequently employed in aeronautic and Fewer generation turbines as well as in the chemical industry. Aluminides are industrially produced by pack cementation or CVD and recently it has been demonstrated that its resistance significantly increases when Cr is added (chrome-aluminides). During this work, a feasibility study has been carried out in order to determine if plasma spray can be employed for depositing this type of coatings on turbine blades. Therefore, aluminium and aluminium/chromium layers were deposited on Ni base IN100 superalloy specimens that were subsequently subjected to a diffusion heat treatment under Ar flow Characterisation and analysis of the coatings were carried out by metallography, SEM and EDS. Cyclic oxidation tests were carried out at 1050 degrees C while molten sulphate hot corrosion was performed at 900 degrees C. The results of this preliminary study are promising and indicate that plasma spray can be developed as an industrial process for production of aluminide and chrome-aluminide coatings.