方位(导航)
航空航天
材料科学
冶金
非金属夹杂物
复合材料
工程类
航空航天工程
计算机科学
人工智能
作者
Lele Wang,Zhouhua Jiang,Chenggang Jiang,Ji Ren,Jialong Tian,Zhimin You
标识
DOI:10.1002/srin.202400079
摘要
Herein, laboratory experiments and thermodynamic calculations are conducted to study the influence of Mg treatment on the inclusion behavior of M50 aerospace bearing steels under different S/O mass ratios (mass ratios of S content to O content). The type, morphology, and distribution of inclusions in ingots with and without Mg treatment are characterized by the scanning electron microscope, energy‐dispersive X‐Ray spectroscopy, and ASPEX automated inclusions analysis system. In addition, the phase distributions of inclusions in M50 steels are simulated using FactSage software to clarify the mechanism of inclusion evolution during the smelting and solidification processes. For both high and low S/O mass ratio steels, the primary spinel and Al 2 O 3 inclusions can be completely modified into MgO inclusions and MnS can be partially transformed into MgS inclusions by Mg treatment. After Mg treatment, the size and number density of inclusions show a noticeable increase in high S/O mass ratio steel resulted from a mass of MgS formation but a slight decrease in low S/O mass ratio steel due to the MgO removal by floatation. Based on the present study, an optimal S/O mass ratio for tight control of detrimental inclusions in Mg‐treated M50 steels is obtained.
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