首页|第三代航空轴承钢CSS-42L的连续冷却转变曲线

第三代航空轴承钢CSS-42L的连续冷却转变曲线

Continuous cooling transformation curve of the third generation aviation bearing steel CSS-42L

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利用膨胀法在DIL805A型淬火膨胀仪对第三代航空轴承钢CSS-42L开展了临界点测定及冷却速度0.02~40 ℃/s的连续冷却转变试验,绘制了静态CCT曲线,并对室温下的显微组织以及维氏硬度进行分析.结果表明,CSS-42L钢的临界点Ac1和Ac3分别为655℃和738℃;连续冷却转变过程中,不同冷速下均只发生马氏体转变,随着冷却速度的降低,马氏体转变起始点降低;CSS-42L钢在冷却速度为1.6 ℃/s时,其硬度值最大为330 HV50.
Critical point and the continuous cooling transformation test of the third generation aviation bearing steel CSS-42L at cooling rate of 0.02-40 ℃/s were carried out by DIL805A quenching dilatometer with dilatometric method.The static CCT curve was drawn,and the microstructure and Vickers hardness at room temperature were analyzed.The results show that the critical points Ac1 and Ac3 of the CSS-42L steel are 655 ℃ and 738 ℃,respectively.In the process of continuous cooling,only martensitic transformation occurs at different cooling rates,and the starting temperature of martensitic transformation decreases with the decrease of cooling rate.The tested CSS-42L steel has a maximum microhardness of 330 HV50 at the cooling rate of 1.6 ℃/s.

CSS-42L bearing steelcritical pointcontinuous cooling transformationmicrohardness

田仲杰、张雲飞、曹文全、赵英利、王艳、白丽娟、崔毅

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河钢材料技术研究院,河北石家庄 052165

河北大河材料科技有限公司,河北石家庄 052165

钢铁研究总院有限公司特殊钢研究院,北京 100081

河钢股份有限公司,河北石家庄 050023

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CSS-42L轴承钢 临界点 连续冷却转变 显微硬度

2024

金属热处理
北京机电研究所 中国机械工程学会热处理学会 中国热处理行业协会

金属热处理

CSTPCD北大核心
影响因子:0.546
ISSN:0254-6051
年,卷(期):2024.49(12)