Light weight materials are interesting for high temperature applications in the aerospace as well as automotive industries. Especially for highly stressed components, where materials with low density are requested, c-TiAl based alloys are attractive to replace the heavy steels and nickel-based alloys because of their good mechanical properties including high specific stiffness, high tensile strength and good creep resistance in a temperature range from 700°C up to 900°C. [1][2][3] Titanium aluminides based on c-TiAl were tested successfully as parts of automotive engines [2,3] as well as components in aeroengines, [4] such as low pressure turbine blades. However, application of titanium aluminides is limited to service temperatures below about 750°C due to insufficient oxidation resistance at higher temperatures caused by the formation of fast growing and porous titania. [5][6][7][8][9] To improve the oxidation behaviour of TiAl the formation of non protective TiO 2 has to be prevented. A method to increase the oxidation resistance of c-TiAl is the use of coatings. [10,11] As reported in the literature, Si-based coatings can form stable titanium silicide phases with good oxidation resistance. [12][13][14][15][16][17] In this work Ti-Si coatings were deposited on c-TiAl based material, and their protection capability was evaluated.
ExperimentalThe material used was c-TiAl based Ti-45Al-8Nb alloy (in at%), provided by GfE, Germany. From extruded rods discshaped specimens with 15 mm diameter and 1 mm thickness were machined; their surfaces were ground using SiC paper up to 4000 grit, polished and cleaned. On the samples a 10 lm thick Si-25 at% Ti coating was deposited by magnetron sputtering using a dual source equipment [18,19] with an elemental silicon target on a RF-source and an elemental titanium target on a DC-source.After coating deposition the samples were annealed under high-vacuum conditions (10 -6 mbar) at 1000°C for 100 h in order to form surface layers of stable titanium silicides by interdiffusion. Besides high-vacuum annealing, some of the coated specimens were pre-oxidised in air at 750°C for 100 h.The oxidation resistance of the pre-treated coated specimens was studied performing mass gain measurements during thermal cycling at 900°C in air. One cycle consisted of 1h heating and 10 min cooling down to 60°C. To study the evolution of microstructure and phase formation during exposure the samples were examined after different exposure time periods (10, 100 and 1000 cycles) using scanning electron microscopy (SEM) and energy-dispersive X-ray (EDX) spectroscopy.
Results and DiscussionCross-sections of coated samples which were high-vacuum annealed or pre-oxidised in air are shown in Figures 1 and 2. No oxidation was observed during the annealing process at 1000°C. Owing to interdiffusion between substrate and Si-25Ti-coating a 13 lm thick titanium silicide layer formed, consisting of a broad Ti 5 Si 3 layer and a thinner outer Ti 5 Si 4 film (Fig. 1). In comparison to high-vacuum annealed samples, the p...