00Cr21Ni2Mn5N双相不锈钢的高温变形

采用Gleeble-3800热/力模拟实验等方法研究了00Cr21Ni2Mn5N奥氏体-铁索体双相不锈钢(LDSS)在温度为850～1150℃、应变速率为5～50s^-1,压下量60%的热变形行为及组织变化。结果表明,00Cr21Ni2Mn5N双相不锈钢的流变应力随温度的增加而降低,随应变速率的增加而增加,该钢的软化机制与Zener-Hollomon(Z)参数有关,00Cr21Ni2MnSN双相钢的表观应力指数为4.82,热变形表观激活能(Q)为219 kJ/mol     

00Cr25Ni7Mo4N超级双相不锈钢的高温变形行为

采用热/力模拟实验方法研究了00Cr25Ni7Mo4N超级双相不锈钢(SDSS)在900～1 200℃、应变速率为0.1～10 s-1条件下的热变形及组织变化,讨论了热变形参数对流变应力和显微组织的影响.结果表明,在上述变形条件下,00Cr25Ni7Mo4N超级双相不锈钢中铁素体的软化机制与Z参数有关,且随着Z参数减小,铁素体软化机制由动态回复向动态再结晶转变;该钢的表观应力指数为3.51,热变形表观激活能为492 kJ/mol.     

节镍型双相不锈钢00Cr21Mn5Ni1N的热加工性能

 采用热压缩和热拉伸试验方法,对节镍型双相不锈钢00Cr21Mn5Ni1N的高温变形抗力、高温塑性及高温变形时奥氏体相的数量进行了研究。结果表明,00Cr21Mn5Ni1N双相不锈钢在950~1 200 ℃之间变形时,具有良好的热加工性能,钢中奥氏体相量可以控制在适合热加工的范围。     

00Cr26Mo4超级铁素体不锈钢的热变形行为

在Gleeble-3500热模拟试验机上进行高温压缩实验,研究00Cr26Mo4超级铁素体不锈钢在变形温度为1 050～1 250℃、应变速率为0.01～10 s~(-1)条件下的热变形行为。采用幂函数、指数函数和双曲正弦模型模拟该材料的热变形参数,建立了相应的热变形本构方程。结果表明,在热压缩过程中,流变应力随变形温度的升高而降低,随应变速率的升高而增加,流变应力并未出现明显峰值,材料的软化机制仅有动态回复。探究了幂函数、指数函数和双曲线函数3种模型与00Cr26Mo4钢本构关系的相关性。结果表明,双曲正弦函数模型更符合00Cr26Mo4超级铁素体不锈钢热加工流变应力应变曲线变化规律,并基于双曲正弦函数模型建立了00Cr26Mo4钢的本构方程,计算了热变形激活能238.836 kJ/mol。     

00Cr26Mo4超级铁素体不锈钢的热变形行

在Gleeble-3500热模拟试验机上进行高温压缩实验,研究00Cr26Mo4超级铁素体不锈钢在变形温度为1050～1250℃、应变速率为0.01～10 S^-1条件下的热变形行为。采用幂函数、指数函数和双曲正弦模型模拟该材料的热变形参数,建立了相应的热变形本构方程。结果表明,在热压缩过程中,流变应力随变形温度的升高而降低,随应变速率的升高而增加,流变应力并未出现明显峰值,材料的软化机制仅有动态回复。探究了幂函数、指数函数和双曲线函数3种模型与00Cr26Mo4钢本构关系的相关性。结果表明,双曲正弦函数模型更符合00Cr26Mo4超级铁素体不锈钢热加工流变应力应变曲线变化规律,并基于双曲正弦函数模型建立了00Cr26Mo4钢的本构方程,计算了热变形激活能238.836 kJ/mol。     

00Cr22Ni5Mo3N钢的热扭转性能

研究了00Cr22Ni5Mo3N双相不锈钢的热扭转性能,比较了N和Ni元素对该钢热扭转性能的影响,并采用Themo-Calc热力学软件进行了相关计算及分析.结果表明,在1 000～1 200℃,随变形温度升高,00Cr22Ni5Mo3N钢的热扭转塑性逐渐提高,当变形温度达到1 150～1 200℃时,该钢的热扭转塑性大幅度提高,而且N比Ni元素对钢热扭转塑性的影响更加显著.     

超级奥氏体不锈钢的高温变形行为

 为了研究超级奥氏体不锈钢Cr20Ni24Mo6N钢的高温变形行为,采用Gleeble热模拟试验机进行了等温压缩试验,建立了合金的热加工图。结果表明,当变形温度为1 000～1 200 ℃时,Cr20Ni24Mo6N钢的流变曲线表现出典型的“加工硬化＋动态再结晶软化”特点;Cr20Ni24Mo6N钢的热激活能[Q]为678.656 kJ/mol。通过加工图与微观组织综合分析得出,超级奥氏体不锈钢Cr20Ni24Mo6N的合适热加工工艺为,应变速率10 s－1左右,应变量0.5～0.8,变形温度1 150～1 200 ℃。     

铈对超级双相不锈钢00Cr25Ni7Mo4N热加工性能的影响

通过Gleeble-1500D热模拟试验机对0～0.034%Ce的超级双相不锈钢00Cr25Ni7Mo4N(%:0.016～0.020C、24.50～24.72Cr、7.06～7.18Ni、3.61～3.73Mo、0.26～0.27N)进行了950～1 200℃、应变速率5×10-3s-1的热拉伸和变形量60%、应变速率1×10~0s~(-1)的热压缩试验。结果表明,适量铈的加入能提高00Cr25Ni7Mo4N钢的热塑性,铈含量为0.012%时有最好的热塑性;铈含量为0.021%以上时,该钢的峰值应力低于未加稀土钢;铈的加入有助于钢提前达到稳态流变阶段。     

2507超级双相不锈钢的热变形行为

用MMS-200热模拟实验机对2507超级双相不锈钢(/%:0.022C、0.58Si、25.35Cr、7.17Ni、4.05Mo、0.28N)12 mm热轧板在1 000～1150℃、应变速率0.01～10s^-1下进行了热压缩实验。实验结果表明,在应变速率一定的条件下,变形温度越高,2507超级双相不锈钢峰值应力越低;在变形温度一定的条件下,峰值应力随着应变速率的增加而增加。根据热变形方程计算得到压缩变形时的平均表观应力指数n=3.25,热变形激活能Q=460kJ/mol。基于实验数据构建了2507超级双相不锈钢在相应变形条件下的热变形方程。     

铸态超级双相不锈钢S32750热加工性能

 为研究热变形参数对铸态超级双相不锈钢S32750热变形行为和显微组织的影响,运用Gleeble-3800热模拟试验机对S32750进行不同温度和应变速率下的高温拉伸和压缩试验。结果表明,S32750在1000~1200℃范围内具有较好的热塑性。在变形温度较低、应变速率较低时,流变曲线表现出不同于单相不锈钢的“类屈服平台”特征;当应变速率较高或变形温度较高、应变速率较低时,流变曲线为典型的动态再结晶特征。微观组织演变显示,铁素体和奥氏体两相都发生动态再结晶,且铁素体的再结晶先于奥氏体。降低应变速率,提高变形温度,可促进动态再结晶发生。基于热变形动力学模型建立了本构方程,表观应力指数为3.99,热变形激活能为393.75kJ/mol。S32750的高温软化机制与Zener-Hollomon(Z)参数有关,随Z参数增加,热变形峰值应力增加。     

Hot ductility of DSS and its microstructure observation during hot deformation

selecting several typical DSS 00Cr22Ni5Mo3N,00Cr21Ni2Mn5N and 00Cr25Ni7Mo4N as research materials,hot ductility characteristic of DSS was studied and microstructure evolution during hot compression was observed.The results show that the optimum hot ductility temperature range of DSS is 1 050~1 200℃.00Cr25Ni7Mc4N exhibits the worst hot ductility and 00Cr21Ni2Mn5N has similar hot ductility to 00Cr22Ni5Mo3N.During hot compression,austenite of DSS mainly occurs dynamic recovery,the ferrite of 00Cr22Ni5Mo3N,00Cr21Ni2Mn5N can perform dynamic recovery and recrystallization,but only dynamic recovery can be observed in the ferrite of 00Cr25Ni7Mo4N.     

03Cr18NiMoN节镍双相不锈钢的热变形行为及热加工图

关键词：双相不锈钢; 流变曲线; 本构方程; 热加工图     

00Cr25Ni7Mo4N超级双相不锈钢热加工性能的研究

通过Gleeble热模拟机对真空感应炉熔炼的00Cr25Ni7Mo4N锻材进行高温拉伸和单道次及连续4道次压缩试验。结果表明,在900～1 250℃的范围内随温度提高和在950～1 100℃时随道次递增,00Cr25Ni7Mo4N钢的最大变形抗力逐渐下降;在1 050～1 250℃时,00Cr25Ni7Mo4N钢的变形抗力较低,断面收缩率高于60%,具有较好的热塑性;当应变速率为10/s且温度高于1 000℃,及应变速率为50/s且温度高于1 100℃时,钢的热加工性较好。     

Hot Ductility of DSS and Its Microstructure Observation During Hot Deformation

By selecting several typical duplex stainless steels (DSS), i. e., 00Cr22Ni5Mo3N, 00Cr21Ni2Mn5N and 00Cr25Ni7Mo4N, as research materials, hot ductility characteristic of DSS was studied by thermal simulation method and microstructure evolution during hot compression was observed through TEM. The results show that the optimum hot ductility temperature range of DSS is 1050–1200°C. 00Cr25Ni7Mo4N exhibits the worst hot ductility and 00Cr21Ni2Mn5N has similar hot ductility to 00Cr22Ni5Mo3N. During hot compression, the dynamic recovery of austenite occurs in DSS while the dynamic recovery and reerystallization of ferrite take place in 00Cr22NioMo3N and 00Cr21Ni2Mn5N, but only the dynamic recovery of ferrite can be observed in 00Cr25Ni7Mo4N.     

Microstructure Evolution and Dynamic Softening Mechanism of 00Cr22Ni5Mo3N DSS During Hot Compression

 Through plane strain compression, hot ductility of 00Cr22Ni5Mo3N DSS is studied under plane strain condition, and the dynamic softening mechanism is investigated through microstructure observation under TEM. The results show that the deformation temperature can markedly influence the peak stress of 00Cr22Ni5Mo3N specimens. And being different from DSS softening mechanism generally reported, ferrite can be softened through dynamic recovery and recrystallization, but austenite can be softened only through dynamic recovery during hot deformation. The unfavourable effect of N on softening capacity of austenite is greater than that of Ni.     

00Cr22Ni5Mo3N钢大口径厚壁无缝管热穿孔工艺的开发

研究了00Cr22Ni5Mo3N钢的热扭转性能,结果表明,通过对化学成分和扭转温度的合理控制,可以使00Cr22Ni5Mo3N钢获得良好的热塑性,并使其变形抗力小于1Cr18Ni9Ti钢.根据试验结果制订了生产工艺,采用热穿孔工艺成功试制出00Cr22Ni5Mo3N钢大口径厚壁无缝管.     

Constitutive Modeling for Elevated TemperatureFlow Behavior of 30Cr2Ni4MoV Ultra-super-crit- ical Rotor Steel

In order to perform numerical simulation of forging and determine the hot deformation processing parameters for 30Cr2Ni4MoV steel, the compressive deformation behaviors of 30Cr2Ni4MoV steel were investigated at the temperatures from 970 to 1270 ℃ and strain rates from 0. 001 to 0.1 s-1 on a Gleeble-3500 thermo-mechanical simulator. The flow stress constitutive equations of the work hardening-dynamical recovery period and dynamical recrystallization period were established for 30Cr2Ni4MoV steel. The stress-strain curves of 30Cr2Ni4MoV steel predicted by the proposed model well agreed with experimental results, which confirmed that the proposed equations can be used to determine the hot deformation processing parameters for 30Cr2Ni4MoV steel.