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Investigation of the Laser Powder Bed Fusion Process of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si Alloy 被引量:1
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作者 Changchun Zhang Tingting Liu +2 位作者 Wenhe Liao Huiliang Wei Ling Zhang 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2023年第2期78-90,共13页
Laser powder bed fusion(LPBF)is an advanced manufacturing technology;however,inappropriate LPBF process parameters may cause printing defects in materials.In the present work,the LPBF process of Ti-6.5Al-3.5Mo-1.5Zr-0... Laser powder bed fusion(LPBF)is an advanced manufacturing technology;however,inappropriate LPBF process parameters may cause printing defects in materials.In the present work,the LPBF process of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy was investigated by a two-step optimization approach.Subsequently,heat transfer and liquid flow behaviors during LPBF were simulated by a well-tested phenomenological model,and the defect formation mechanisms in the as-fabricated alloy were discussed.The optimized process parameters for LPBF were detected as laser power changed from 195 W to 210 W,with scanning speed of 1250 mm/s.The LPBF process was divided into a laser irradiation stage,a spreading flow stage,and a solidification stage.The morphologies and defects of deposited tracks were affected by liquid flow behavior caused by rapid cooling rates.The findings of this research can provide valuable support for printing defect-free metal components. 展开更多
关键词 Laser powder bed fusion ti-6.5al-3.5mo-1.5zr-0.3si alloy Process parameters Heat transfer and liquid flow DEFECTS
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Constitutive equation and hot deformation characteristic of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy with equiaxed microstructure 被引量:3
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作者 HUANG Lujun,GENG Lin,LI Aibin,WANG Guisong,and SHI Lei School of Materials Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 《Rare Metals》 SCIE EI CAS CSCD 2007年第S1期88-93,共6页
The hot deformation behavior of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy with equiaxed microstructure was characterized in the temperature range of 900~1060 ℃ and strain rate range of 10-3~10 s-1.The experimental results i... The hot deformation behavior of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy with equiaxed microstructure was characterized in the temperature range of 900~1060 ℃ and strain rate range of 10-3~10 s-1.The experimental results indicate that the plastic deformation behavior of the titanium alloys is rather sensitive to temperature and strain rate.In the α+β phase temperature region,all of the stress-strain curves exhibit different degrees of the flow softening after a peak stress.In the β phase temperature region,the titanium alloy shows a stress softening at high strain rates and a steady flow stress at low strain rates.On the basis of the peak stress data,the constitutive equations were constructed in the α+β phase temperature region and β phase temperature region,respectively.Activation energy parameters were calculated to be 344.923 kJ·mol-1 in the β phase temperature region and 628.3 kJ·mol-1 in the α+β phase temperature region.Microstructure of the compressed specimens in water-quenched conditions was found to be quite dependent on the conditions of deformation. 展开更多
关键词 constitutive equation hot deformation ti-6.5al-3.5mo-1.5zr-0.3si
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Hot deformation behavior of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy with acicular microstructure 被引量:2
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作者 刘高峰 张尚洲 陈礼清 《Journal of Central South University》 SCIE EI CAS 2011年第2期296-302,共7页
The characteristics of hot deformation of an α+β titanium alloy Ti-6.5Al-3.5Mo-1.5Zr-0.3Si with acicular microstructure were studied using isothermal hot compressive tests in a strain rate range of 0.01-10 s^-1 at ... The characteristics of hot deformation of an α+β titanium alloy Ti-6.5Al-3.5Mo-1.5Zr-0.3Si with acicular microstructure were studied using isothermal hot compressive tests in a strain rate range of 0.01-10 s^-1 at 860-1 100 ℃. The true stress-tree strain curves of alloy hot-compressed in the α+β region exhibit a peak stress followed by continuous flow softening; whereas in the β region, the flow stress attains a steady-state regime. At a strain rate of 10 s^-1 and in a wide temperature range, the alloy exhibits plastic flow instability. According to the kinetic rate equation, the apparent activation energies are estimated to be about 633 kJ/mol in the α+β region and 281 kJ/mol in the β region, respectively. The processing maps show a domain of the globularization process of a colony structure and α dynamic recrystallization in the temperature range of 860-960 ℃ with a peak efficiency of about 60%, and a domain of β dynamic recrystallization in the β region with a peak efficiency of 80%. 展开更多
关键词 titanium alloy ti-6.5al-3.5mo-1.5zr-0.3si hot compression flow behavior MICROSTRUCTURE
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Influences of residual stress and micro-deformation on microstructures and mechanical properties for Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy produced by laser powder bed fusion 被引量:4
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作者 C.C.Zhang H.L.Wei +3 位作者 T.T.Liu L.Y.Jiang T.Yang W.H.Liao 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2021年第16期174-183,共10页
Laser powder bed fusion(LPBF)yields unique advantages during the fabrication of titanium alloys.In the present work,Ti-6.5 Al-3.5 Mo-1.5 Zr-0.3 Si alloy specimens with excellent mechanical performances were fabricated... Laser powder bed fusion(LPBF)yields unique advantages during the fabrication of titanium alloys.In the present work,Ti-6.5 Al-3.5 Mo-1.5 Zr-0.3 Si alloy specimens with excellent mechanical performances were fabricated by LPBF.The as-built specimens displayed relatively high strength and ductility under modest volume energy densities(VEDs),whereas they manifested high strength with low ductility under high VEDs.To investigate the key reason of this phenomenon,the specimens were designed with two VEDs ranges of 60 J/mm^(3) and 85 J/mm^(3).Special attention was paid to the influences of residual stress and micro-deformation on microstructures and mechanical properties for the first time.The results indicated that the residual stresses and relative density of the 60 J/mm^(3) range specimens were higher than that of the 85 J/mm3 range specimens.Dislocation multiplication and dislocation movement promoted by the residual stress were hindered by the initialα’phase grain boundary(prior-α’GB),leading to the formation ofα’metastable structures.The mean tensile strength and elongation of the 60 J/mm^(3) range specimens were 1248.1 MPa and 12.3%,respectively,whereas the corresponding values for the 85 J/mm^(3) range specimens were 1405.3 MPa,5.0%,respectively.During deformation,the strength and ductility of the specimens were first improved by lamellar structures generated from prior-α’phases,and then effectively enhanced by the interaction between the{10–12}twins and dislocations.However,pores significantly reduced the ductility;hence,high VED specimens with large twins and numerous large pores increased the strength and reduce the ductility. 展开更多
关键词 Laser powder bed fusion ti-6.5al-3.5mo-1.5zr-0.3si alloy Residual stress Twin Mechanical properties
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基于Murty判据的Ti-6.5Al-3.5Mo-1.5Zr-0.3Si钛合金α+β相区热变形机制及工艺优化(英文) 被引量:6
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作者 李鑫 鲁世强 +3 位作者 王克鲁 傅铭旺 李臻熙 曹春晓 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2008年第4期577-583,共7页
根据Murty失稳判据,利用原始等轴组织的TC11钛合金在780~990℃和0.001~70s^-1范围内的等温恒应变速率压缩实验数据,建立了该合金的加工图。依据加工图研究了TC11钛合金的变形机制和变形缺陷与变形热力参数之间的关系。结果表明,在... 根据Murty失稳判据,利用原始等轴组织的TC11钛合金在780~990℃和0.001~70s^-1范围内的等温恒应变速率压缩实验数据,建立了该合金的加工图。依据加工图研究了TC11钛合金的变形机制和变形缺陷与变形热力参数之间的关系。结果表明,在780~990℃和0.001~0.01s^-1范围是超塑性变形区;在780~990℃和高于0.0ls^-1范围,易出现口相裂纹和空洞、局部流动以及绝热剪切等流变失稳现象。根据加工图分析,结合微观组织观察结果,并考虑变形抗力的大小,确定出了较佳的变形热力参数范围为850~940℃和0.001~0.01s^-1,最佳的变形热力参数在900℃和0.001s^-1附近。 展开更多
关键词 钛合金 ti-6.5A1-3.5mo-1.5zr-0.3si 工艺优化 Murty失稳判据 变形机制
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Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金本构关系的BP神经网络模型 被引量:6
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作者 王克鲁 鲁世强 +2 位作者 李鑫 董显娟 杨化娟 《特种铸造及有色合金》 CAS CSCD 北大核心 2008年第8期575-578,共4页
利用THERMEcMASTOR-Z型热力模拟试验机,在变形温度为7801080℃,应变速率为0.001~70.0S。条件下对Ti6.5A1-3.5Mo-1.5Zr-0.3Si合金进行等温恒应变速率压缩试验,获得不同变形温度、不同应变速率和不同真应变下的流动应力数据。... 利用THERMEcMASTOR-Z型热力模拟试验机,在变形温度为7801080℃,应变速率为0.001~70.0S。条件下对Ti6.5A1-3.5Mo-1.5Zr-0.3Si合金进行等温恒应变速率压缩试验,获得不同变形温度、不同应变速率和不同真应变下的流动应力数据。结合试验数据和神经网络知识,构建了采用BP算法的人工神经网络,训练结束后的神经网络即成为Ti-6.5A3.5Mo-1.5Zr-0.3Si合金的一个知识基的本构关系模型。利用所建立的BP网络模型对材料的流动应力进行了预测,发现预测值与试验数据吻合良好,说明该BP网络本构关系模型具有较高的精度.可用于指导Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金热加工工艺的制定。 展开更多
关键词 ti-6.5al-3.5mo-1.5zr-0.3si合金 BP神经网络 本构关系 流动应力
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Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金β加工动态再结晶行为研究 被引量:4
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作者 王克鲁 鲁世强 +2 位作者 李鑫 杨化娟 董显娟 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2009年第2期219-223,共5页
利用Thermecmastor—Z热模拟试验机,在变形温度1020~1080℃和应变速率0.001~70S。范围内对原始等轴组织的Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金进行等温恒应变速率压缩实验,分析高温流动行为,构建基于动态材料模型的功率耗散图,... 利用Thermecmastor—Z热模拟试验机,在变形温度1020~1080℃和应变速率0.001~70S。范围内对原始等轴组织的Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金进行等温恒应变速率压缩实验,分析高温流动行为,构建基于动态材料模型的功率耗散图,并结合微观组织观察对其β加工的动态再结晶行为进行研究。结果表明,Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金在声单相区变形时,不同温度和应变速率下的流动应力曲线均呈稳态流动特征,但仅根据流动应力曲线并不能确定是否发生动态再结晶。根据功率耗散图分析和微观组织观察可知,Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金卢加工易发生动态再结晶的热力参数范围为:变形温度1020-1080℃,应变速率0.01-0.1s^-1,此区域功率耗散功率η值都大于0.4,为实际β加工时优化的热力参数范围;应变速率过高或过低,均不易发生动态再结晶。 展开更多
关键词 ti-6.5al-3.5mo-1.5zr-0.3si合金 动态再结晶 β组织 动态材料模型 功率耗散图
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Grain growth behavior of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy during isothermal β heat treatments 被引量:6
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作者 De-Lai Ouyang Hai-Ming Du +2 位作者 Xia Cui Shi-Qiang Lu Xian-Juan Dong 《Rare Metals》 SCIE EI CAS CSCD 2019年第3期233-237,共5页
Isothermal β heat treatments of Ti-6.5 Al-3.5 Mo-1.5 Zr-0.3 Si alloy were performed at the temperature of1040-1240 ℃ to examine the influence of heating conditions on grain growth of the alloy. The results show that... Isothermal β heat treatments of Ti-6.5 Al-3.5 Mo-1.5 Zr-0.3 Si alloy were performed at the temperature of1040-1240 ℃ to examine the influence of heating conditions on grain growth of the alloy. The results show that the grain size increases with heating temperature and holding time increasing. Rapid β grain growth of the alloy takes place at the temperature of over 1140 ℃. The grain growth kinetics for the alloy follows the classical isothermal grain growth law.The growth time exponent(n) of 0.5651 and activation energy(Q) of 129.6 kJ mol-1 are determined. Finally, in order to determine the grain size under different heating conditions,the grain growth model of the alloy was established. 展开更多
关键词 ISOTHERMAL heating ti-6.5al-3.5mo-1.5zr-0.3si alloy GRAIN growth Model
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Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金β晶粒生长及片层组织转变 被引量:4
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作者 欧阳德来 崔霞 +1 位作者 鲁世强 徐勇 《塑性工程学报》 CAS CSCD 北大核心 2019年第2期206-213,共8页
利用可控冷却速度热处理装置研究了Ti-6. 5Al-3. 5Mo-1. 5Zr-0. 3Si合金β热处理过程中的β晶粒生长及片层组织转变规律。结果表明,合金在β单相区固溶时,随着温度升高和保温时间延长,β晶粒尺寸增大,且加热温度高于1140℃时,β晶粒快... 利用可控冷却速度热处理装置研究了Ti-6. 5Al-3. 5Mo-1. 5Zr-0. 3Si合金β热处理过程中的β晶粒生长及片层组织转变规律。结果表明,合金在β单相区固溶时,随着温度升高和保温时间延长,β晶粒尺寸增大,且加热温度高于1140℃时,β晶粒快速生长。计算了β相区晶粒生长激活能为129. 6 k J·mol-1,并建立了β晶粒生长模型。随冷却速度变化,合金出现全马氏体组织和(α+β)片状组织。原始β晶界在全马氏体组织和(α+β)片状组织中均清晰可见,原始β晶粒呈等轴状特征。(α+β)片以取向各异"集束"形式存在于原始β晶粒内,(α+β)集束内的α片几乎相互平行。(α+β)片层组织特征参数(原始β晶粒尺寸、α片厚度及(α+β)集束尺寸)均随冷却速度降低而增加。α片层可在β晶界和晶内形核,以集束形式生长,但不能穿过β晶界。原始β晶界能对α片层的生长起到约束作用。 展开更多
关键词 ti-6.5al-3.5mo-1.5zr-0.3si合金 β热处理 β晶粒生长 片层结构
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Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金的应变补偿本构方程及组织演变
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作者 李鑫 刘杰 +2 位作者 王克鲁 鲁世强 杨峰 《特种铸造及有色合金》 CAS 2024年第11期1536-1541,共6页
在变形温度为750~950℃和应变速率为0.001~10 s^(−1)范围内,利用热模拟试验机对Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金进行了高度压缩率为50%的试验。通过对流动应力曲线的分析,以Arrhenius型双曲正弦方程为基础,建立了应变隐含在材料常数中... 在变形温度为750~950℃和应变速率为0.001~10 s^(−1)范围内,利用热模拟试验机对Ti-6.5Al-3.5Mo-1.5Zr-0.3Si合金进行了高度压缩率为50%的试验。通过对流动应力曲线的分析,以Arrhenius型双曲正弦方程为基础,建立了应变隐含在材料常数中的精度较高的应变补偿本构方程。采用金相显微镜研究了应变速率和变形温度对微观组织的影响,并利用TEM手段分析了球化机理。结果表明,在试验变形温度下,当应变速率大于0.01 s^(−1)时,α片层以弯折、拉长为主,球化不明显。当应变速率减至0.01 s^(−1)时,α片层开始球化,且随应变速率降低和变形温度升高,球化分数增加。此外,随变形温度升高,α相尺寸增大,且发生了α→β相变。球化机制为界面劈开、剪切和动态再结晶。 展开更多
关键词 ti-6.5al-3.5mo-1.5zr-0.3si合金 本构方程 组织演变 球化机制
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A method for prediction of unstable deformation in hot forging process by simulation
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作者 鲁世强 李鑫 +2 位作者 王克鲁 刘诗彪 傅铭旺 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2013年第12期3739-3747,共9页
A method is proposed for prediction of the unstable deformation in hot forging process using both the determined thermomechnical parameter windows of the unstable deformation zones and finite element simulation. Takin... A method is proposed for prediction of the unstable deformation in hot forging process using both the determined thermomechnical parameter windows of the unstable deformation zones and finite element simulation. Taking Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy as the testing material, the thermomechnical parameter windows of the unstable deformation zones for the Ti-alloy are integrated into a commercial finite element simulation software platform. The distribution and variation of the unstable deformation zones of the alloy in hot compression process are simulated and predicted using the tailor-made finite element codes in the finite element platform. The simulation results tally with the physical experiments and the proposed method for simulation and prediction of the unstable deformation is thus verified and its efficiency is validated. 展开更多
关键词 instability map unstable deformation instability deformation simulation ti-6.5al-3.5mo-1.5zr-0.3si titanium alloy
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