GCr19SiMnMo锻后组织转变分析及工艺优化

Analysis of microstructure transformation and process optimization after forging of GCr19SiMnMo

  • 摘要: 研究GCr19SiMnMo轴承套圈锻件锻后冷却及正退火过程中的组织转变,与GCr15SiMn对比分别做工艺试验,对比两种材质的组织转变过程,分析不同组织对锻件质量的影响。优化工艺,控制锻件组织,使锻件内部质量满足要求,降低显微裂纹风险。试验结果表明,薄壁(壁厚≤40mm)GCr19SiMnMo轴承套圈在900-1000℃终锻风冷易形成粗大马氏体组织,且正火后出现了粗大晶粒组织遗传;而不是像GCr15SiMn锻后冷却形成索氏体或屈氏体,有较大的显微裂纹风险,且正火后出现了粗大晶粒组织遗传。通过工艺改进,使GCr19SiMnMo锻件锻后组织转变为珠光体,减小锻后组织应力,减少显微裂纹倾向,阻断粗大晶粒遗传。

     

    Abstract: Abstract: The microstructure transformation of GCr19SiMnMo bearing ring forgings during post-forging cooling and normalizing annealing was studied. Process tests were conducted in comparison with GCr15SiMn to contrast the microstructure evolution of the two materials, and the effects of different microstructures on forging quality were analyzed. The process was optimized to control the microstructure of forgings, so as to meet the internal quality requirements of forgings. The test results show that air cooling after finish forging at 900–1000 ℃ tends to form coarse martensite in thin-walled GCr19SiMnMo bearing rings (wall thickness ≤40 mm), and coarse grain inheritance occurs after normalizing. GCr15SiMn forms sorbite or troostite after post-forging cooling. Through process improvement, the post-forging microstructure of GCr19SiMnMo forgings is transformed into pearlite, which reduces post-forging structural stress and inhibits coarse grain inheritance.

     

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