Solid particle erosion and oxidation-assisted erosion at temperatures above 400 °C severely affect Ti6Al4V components such as gas turbine compressor blades. To address this issue, an erosion- and oxidation-resistant Cr/Cr₂N multilayer coating with gradient interfaces (thickness ~ 11 μm, bi-layer period ~8 nm) was developed on Ti6Al4V. The phase of the as-deposited coating by magnetron sputtering was Cr/CrN; further annealing of this coating at 400 °C resulted in Cr/Cr2N. Initially, individual Cr, CrN, and Cr/CrN films (thickness ~ 1.5 μm) were deposited to study crystallographic properties. The as-deposited multilayer film exhibited a broad XRD peak related to Cr/CrN phase. However, after annealing at 400 °C, the film phase transformed into a well-crystallized Cr/Cr₂N structure. The erosion resistance of the ~11 μm thick coating was studied from room temperature to 800 °C following ASTM-G76 standard. The average erosion resistance of the coated Ti6Al4V (at different impinging angles) was ~76 times higher than that of bare Ti6Al4V at 400 °C @ 30 m/s erodent speed. In addition, the coated Ti6Al4V exhibited superior erosion resistance up to 800 °C, compared to bare Ti6Al4V. Bare Ti6Al4V exhibited oxidation-induced brittle cracking at temperatures ≥600 °C, whereas the coating did not show any cracks. Oxidation tests at 800 °C for 30 min revealed severe material loss (~11 μm) for bare Ti6Al4V, while a thin, stable Cr₂O₃ layer (~1 μm) formed on Cr/Cr₂N coating, confirming its excellent high-temperature oxidation and erosion resistance performance at higher temperatures. Additionally, the high-temperature erosion mechanism for both coated and uncoated Ti6Al4V is also explained.
扫码关注我们
求助内容:
应助结果提醒方式:
