首页|热处理工艺对65Mn材料组织和性能的影响

热处理工艺对65Mn材料组织和性能的影响

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采用落实硬度计和光学显微镜对真空炉淬火+井式炉回火和盐浴炉淬火+井式炉回火两种热处理后65Mn材料的性能和组织进行对比分析.结果表明:真空炉淬火+井式炉回火后材料硬度低,为HRC30~35,组织为马氏体、贝氏体、铁素体及碳化物;盐浴炉淬火+井式炉回火后材料硬度高,为HRC50~35,组织为马氏体和少量铁素体及碳化物;分析造成真空炉淬火+井式炉回火硬度低的原因为:真空炉淬火时淬火转移时间长(淬火转时间约40s),造成材料奥氏体化不充分,淬火后零件硬度低.
Influence of Heat Treatment Process on Microstructure and Properties of 65Mn Material
The properties and microstructure of 65Mn materials after vacuum furnace quenching+vertical pit furnace tempering and salt-bath furnace quenching+vertical pit furnace tempering were compared and analyzed by using a Rockwell hardness tester and an optical microscope.The results show that after vacuum furnace quenching and vertical pit furnace tempering,the hardness of material is low,which is HRC30~35,and the microstructure is martensite,bainite,ferrite and carbide.After salt bath furnace quenching and vertical pit furnace tempering,the hardness of material is high,which is HRC50~55,and the microstructure is martensite and a small amount of ferrite and carbide.The reason for the low hardness caused by vacuum furnace tempering and vertical pit furnace tempering is that the quenching transfer time during vacuum furnace quenching is long(about 40s),resulting in insufficient austennitization of the material and low hardness of the parts after quenching.

martensitequenching transfer timehardness

杨海川、张家奎

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航空工业新乡航空工业集团有限公司,新乡 453049

马氏体 淬火转移时间 硬度

2024

航空精密制造技术
北京航空精密机械研究所

航空精密制造技术

CSTPCD
影响因子:0.228
ISSN:1003-5451
年,卷(期):2024.60(2)