首页|利用SMAT和SPS在纯铁表面制备铁镍合金层

利用SMAT和SPS在纯铁表面制备铁镍合金层

Preparation of Iron-nickel Alloy Layer on Surface of Pure Iron by SMAT+SPS

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利用放电等离子烧结(SPS)技术实现了镍粉在纯铁表面铁镍合金层的制备,通过纯铁表面机械研磨(SMAT)的预处理获得表面纳米层和梯度结构有效促进了铁镍的扩散,提升了合金层厚度和结合强度.通过XRD、SEM、EDS、硬度和摩擦磨损实验等,表征铁镍合金层形貌、组成,测试了力学性能.结果表明:纯铁试样经过SMAT预处理和SPS后,在表面获得了约 50 μm的铁镍合金层,沿着深度方向镍元素含量梯度变化,而在未经SMAT预处理的纯铁表面仅有 25 μm的合金层,本方法实现了合金层厚度明显增加.SMAT预处理后的SPS试样硬度提升,表面磨损量和犁沟槽深度减少,结合力增强,耐磨性提升明显.
The spark plasma sintering(SPS)technology was used to realize the preparation of the iron-nickel alloy layer on the surface of pure iron with nickel powder paving on the iron surface.The surface nano-layer and graded structure obtained by the pre-surface mechanical attrition treatment(pre-SMAT)on the pure iron surface effectively promotes the diffusion of iron and nickel during SPS,and the thickness and bonding strength of the alloy layer improves.By XRD,SEM,EDS,hardness,and friction and wear tests,the morphologies and composition were characterized,and the mechanical properties of the iron-nickel alloy layer were tested.The results show that after SMAT+SPS,an iron-nickel alloy layer with the thickness of about 50 μm on the pure iron sample has been prepared.And in the depth direction,the nickel content shows a gradient change.However,the alloy layer depth on the surface of pure iron without SMAT pretreatment is just 25 μm.Therefore,the method can achieve a significant increase in the thickness of the alloy layer.After SMAT pretreatment,the hardness of the surface alloy layer increases,the wear mass loss of surface and the depth of the plough groove reduce.The bonding strength increases.The wear resistance obviously improves.

spark plasma sintering(SPS)surface mechanical attrition treatment(SMAT)pure ironFe-Ni alloyinghardness

安艳丽、范帅君

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山西医科大学 基础医学院,山西 太原 030001

太原理工大学 材料科学与工程学院,山西 太原 030024

兴县经开区铝镁新材料研发有限公司,山西 吕梁 035300

放电等离子烧结 表面机械研磨处理 纯铁 铁镍合金化 硬度

国家自然科学基金区域创新基金重点项目山西省中央引导地方科技发展资金项目山西省重大专项山西省重大专项吕梁市引进高层次科技人才重点研发项目

20181101014MC2016-06201603D111004201805003RC2020-107

2024

热加工工艺
中国船舶重工集团公司热加工工艺研究所 中国造船工程学会船舶材料学术委员会

热加工工艺

CSTPCD北大核心
影响因子:0.55
ISSN:1001-3814
年,卷(期):2024.53(10)