D.G. Lee
,
K.C. Jang
,
J.M. Kuk
,
I.S. Kim
金属学报(英文版)
Rotary bending fatigue tests were carried out with two kinds of materials, S43C and S50C, using the front engine and front drive shaft (FF shaft) of vehicle. The specimens were induction hardened about 1.0mm depth from the specimen surface, and the hardness value on the surface was about HRC56-60. The tested environment temperatures were -30, 25 and 80℃ in order to look over effect of the induction hardening and the environmental temperatures on the fatigue characteristics. The fatigue limit of induction hardened specimens increased more about 45% than non-hardened specimens showing that the endurances of S43C and S50C were 98.1 and 107.9MPa in non-hardened samples, 147.1 and 156.9MPa in hardened samples respectably. The maximum tensile and compressive stress on the small circular defect was about +250 and -450MPa respectively when circular defect is situated on top and bottom. The fatigue life increased 80, 25 and -30℃ in order regardless of hardening. In comparison of the fatigue lives on the basis of tested result at 25℃, the fatigue lives of non-hardened specimens decreased about 35%, but that of hardened specimens decreased about only 5% at 80℃ more than at 25℃. And fatigue life of non-hardened and hardened specimens were about 110% and 120% higher at -30℃ than that of 25℃. Based on the result of stress distribution near the defect, the tensile and compressive stress repeatedly generated by load direction were the largest on the small circular defect due to the stress concentration.
关键词:
induction hardening
,
null
,
null
TAO Zengyi LUO Jiaming Huazhong University of Science and Technology
,
Wuhan
,
China TAO Zengyi
,
Faculty of Metallic Materials
,
Dept.of Mechanical Engineering No.2
,
Huazhong University of Science and Technology
,
Wuhan 430074
,
China
金属学报(英文版)
The influence of laser surface melting and induction hardening on the surface structure,con- tact fatigue life and failure behaviour of the nodular cast iron has been investigated.The con- tact fatigue life can be improved by both laser treatment and induction hardening,but the fail- ure process and type are different from each other.The former is due to lumpy and deep spal- ling caused by crack propagation between the quenching zone and the substrate,and the latter is due to nubby and surface flaking caused by the oil wedged action into surface cracks.
关键词:
surface hardening
,
null
,
null
,
null
张毅斌
,
李德强
,
王大伟
材料开发与应用
研究了感应淬火热处理工艺对10CrNi3MoV对称球扁钢力学性能的影响.结果表明,10CrNi3MoV对称球扁钢的淬火温度随着感应淬火轨道频率的提高而显著降低,控制轨道频率7 ～11Hz,即可控制球扁钢加热温度840～890℃.感应淬火温度和淬火水量对球扁钢的力学性能存在显著影响,随着感应淬火温度的提高以及淬火水量的降低,腹板部位的屈服强度显著降低,低温韧性变化不明显.二次调质热处理时钢的屈服强度显著降低,应提高钢的奥氏体化温度及奥氏体化均匀程度.感应加热淬火时,高温停留时间短,奥氏体化程度低,淬火后获得了细小的马氏体和贝氏体混合组织,钢的屈服强度较加热炉加热显著提高.
关键词:
感应加热
,
对称球扁钢
,
调质热处理
,
力学性能
刘江
,
陈锋
,
余新泉
机械工程材料
针对轧辊表面淬硬层深度大、表层具有细小马氏体组织的要求,采用数控淬火机床、显微镜、硬度仪等研究了感应淬火工艺参数对GCr15钢表面淬硬层的影响.结果表明:对淬硬层组织和性能影响较大的是加热功速比,而冷却水流量的影响不大;随着加热功速比的增大,淬硬层深度增加,但奥氏体晶粒和马氏体尺寸随之增大;试样截面的硬度曲线总体呈梯度下降分布,在离表面3 mm处存在一个峰值;预热功速比也是调整淬硬层深度的一个参考因素,增大预热功速比,淬硬层深度也会相应增大.
关键词:
GCr15钢
,
感应淬火
,
功速比
,
淬硬层
贺连芳
,
李辉平
,
盖康
,
张春芝
,
李木森
材料热处理学报
为了利用数值模拟技术计算感应加热过程中丝杠的奥氏体化情况,利用Gleeble1500D热模拟试验机,测试了55CrMo钢试样在升温速率为0.05 ～-50 K/s时的膨胀曲线,得到了它的奥氏体化温度与加热速率的关系.根据相变膨胀曲线,利用杠杆定律得到了奥氏体转变量与温度的关系,并对非等温相变Johnson-Mehl-Avrami(JMA)方程中的动力学参数进行了线性回归分析,得到了JMA相变动力学模型.利用数值模拟技术,计算了丝杠在感应加热时的奥氏体化情况和淬火后的硬度曲线,并与实验结果进行对比.结果表明,模拟结果与实验结果吻合得较好,所得到的JMA方程能较好地描述55CrMo钢的奥氏体化过程.
关键词:
相变动力学
,
JMA方程
,
数值模拟
,
感应淬火
崔洪芝
,
李永凤
,
孙金全
,
李保民
,
陈鑫
,
白斌
材料热处理学报
通过涂覆导磁体对GCr15钢滚珠丝杠表面感应淬火进行漏磁控制,对比分析了漏磁控制前后试样淬火组织、硬度、深度及耐磨性.研究表明:GCr15淬火后的组织为马氏体+残留奥氏体,控制漏磁淬火工艺显著增加丝杠滚道处的磁力线密度,提高整个丝杠表面的温度和加热深度,增加淬火硬化层的深度,也减小硬度曲线的梯度,从而显著提高了耐磨性,相对于未淬火试样耐磨性提高了2.5 ～4倍.感应淬火试样的磨损主要是磨粒磨损和剥层磨损,未涂覆导磁体时,剥层厚且是脆性和塑性断口混杂的粗糙形貌,而涂覆导磁体后,因为组织和硬度均匀,硬化层深度大,磨削片层薄且表面光整,耐磨性好.
关键词:
GCr15钢
,
导磁体
,
耐磨性
,
漏磁控制
