ZTC4钛合金热等静压内部缺陷弥合区组织演变OA
Microstructure evolution of internal defect healing zone in ZTC4 titanium alloy during hot isostatic pressing
采用数值模拟与实验相结合的方法,分析不同时刻热等静压ZTC4钛合金内部缩孔周边的位移变化、应力应变分布及缺陷弥合区内微观组织的演变规律.结果表明,在热等静压高温高压作用下,缩孔周边形成高应力应变区,距离缩孔表面越近,应力越大,随缩孔尺寸减小,应变集中程度增加.热等静压后缩孔位置形成放射状缩孔弥合区组织,弥合区内不同α/β集束的塑性变形程度不均匀,位错滑移系易开动的α/β集束内变形量较大,从而形成等轴晶组织.
The internal displacement change around shrinkage pores,stress and strain distribution,and microstructural evolution in the defect healing zone of ZTC4 titanium alloy during hot isostatic pressing(HIP)are investigated by numerical simulation combined with experimental methods.The results demonstrate that under the high-temperature and high-pressure conditions of HIP,high stress-strain zones form around the shrinkage pores.The stress magnitude shows an inverse relationship with the distance from pore surfaces,exhibiting higher stress levels in proximity to the pore boundaries.As the shrinkage pore size decreases,the strain concentration intensifies.After HIP,a radial pore-healing zone microstructure develops at the original shrinkage pore sites.Within this healed region,heterogeneous plastic deformation occurs among distinct α/β colonies.Colonies with more readily activated dislocation slip systems experience greater deformation magnitudes,ultimately leading to the formation of equiaxed grain structures.
高威;徐倩;殷亚军;冯新
中国航发北京航空材料研究院 铸造钛合金技术中心,北京 100095武汉轻工大学 机械工程学院,武汉 430048华中科技大学 材料成形与模具技术全国重点实验室,武汉 430074中国航发北京航空材料研究院 铸造钛合金技术中心,北京 100095
航空航天
钛合金热等静压有限元方法弥合区等轴晶
titanium alloyhot isostatic pressingfinite element methodhealing zoneequiaxed grain
《航空材料学报》 2026 (3)
18-27,10
稳定支持项目(2019-363)
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