Hot corrosion behavior of two powder metallurgy superalloys
作者
单位
(1 航空材料先进腐蚀与防护重点实验室、中国航发北京航空材料研究院、北京 100095、2 先进高温结构材料重点实验室、中国航发北京航空材料研究院、北京 100095)
关键词
收录来源
International Corrosion Congress · 第22届国际腐蚀大会
摘要
Hot corrosion behavior of a powder metallurgy superalloy and FGH96 at 700 °C, 750 °C and 800 °C are investigated with weight gain measurement s, X-ray diffraction (XRD), scanning electron microscopy (SEM), and electron probe micro analysis (EPMA). The results show that the gas hot corrosion mechanism of the two alloys is accelerated oxidation, while the hot corrosion with corrosive salts mechanism is combined oxidation and sulfuration. Compared with FGH96, the increased Co and Al content in the new alloy with better hot corrosion resistance, especially at 800 °C. The increased Co and Al content in the new alloy promoted the rapid formation of continuous Cr2O3 and Al2O3 protective films on the alloy surface. Moreover, the high Co content can inhibit internal oxidation of Al and reduced internal diffusion of S through the third element effect, making Al2O3 oxide film complete and continuous, thereby protecting the alloy matrix and reducing the rate of alloy oxidation of sulfuration.