Fatigue Crack Propagation of P/M Soft Magnetic Materials with a High-Resistance Surface Layer

R. Tanegashima, T. Shirosaka, H. Akebono, Masahiko Kato, A. Sugeta, K. Minoshima
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Abstract

In this study, fatigue properties of PM (Powder Metallurgy) soft magnetic materials were investigated by observation of the small fatigue crack propagation. The materials to which binder resin were added (Material BA) and three kinds of materials with different density (Material LD, MD and HD) were used in this study. Reversed plane bending fatigue tests were conducted at room temperature and small fatigue crack growths were studied in detail by means of replication technique. The fatigue strength became higher in the order, material HD, MD, LD, BA. In all specimens, cracks initiated at multi sites and each crack propagated with frequent deflection. Furthermore, cracks were coalesced repeatedly and specimen reached final fracture. Moreover, the difference between the materials was not recognized clearly in the da/dN-Kmax relationship. The maximum defect size, √area max, which was estimated by the statistics of extreme value became higher in the order, material BA, LD, MD, HD. As a result, the addition of the binder resin to PM alloy was not effective in improvement of fatigue strength. Furthermore, densification by increasing compacting pressure was effective in improvement of fatigue strength because the maximum defect size in each material became smaller. The ΔK0-Nf/√area max was estimated to consider whether the evaluation by the statistics of extreme value had propriety to the fatigue strength. Then, their curves were not corresponded. The disagreement was originated in the difference of coalescence frequency until the specimen reached to final fracture.
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高阻表层P/M软磁材料的疲劳裂纹扩展
通过观察粉末冶金软磁材料的小裂纹扩展,研究了其疲劳性能。本研究采用添加粘结树脂的材料(材料BA)和三种不同密度的材料(材料LD、MD和HD)。在室温条件下进行了反平面弯曲疲劳试验,并采用复制技术对小裂纹扩展进行了详细研究。材料的疲劳强度依次为HD、MD、LD、BA。在所有的试样中,裂纹在多个位置开始,每个裂纹以频繁的挠曲扩展。裂纹反复合并,试样最终断裂。此外,在da/dN-Kmax关系中,材料之间的差异没有被清楚地识别出来。根据极值统计估计的最大缺陷尺寸√面积max依次为BA、LD、MD、HD。结果表明,在PM合金中添加粘结树脂不能有效提高合金的疲劳强度。此外,增加压实压力的致密化可以有效地提高疲劳强度,因为每种材料的最大缺陷尺寸都变小了。估算了ΔK0-Nf/√面积最大值,以考虑极值统计评价是否符合疲劳强度。然后,它们的曲线不对应。这种差异主要是由于试样在最终断裂前的聚结频率不同造成的。
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