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Microstructural homogeneity and properties of TC4 titanium alloy ingots produced via electron-beam cold hearth melting
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作者 WANG Meichen CHU Shuangjie +2 位作者 LIANG Gaofei ZHANG Qifei MAO Bo 《Baosteel Technical Research》 2025年第3期41-48,共8页
TC4 titanium alloy(Ti-6Al-4V),known for its excellent specific strength,corrosion resistance,and weldability,is extensively applied in aerospace,marine engineering,and advanced manufacturing.This study focuses on the ... TC4 titanium alloy(Ti-6Al-4V),known for its excellent specific strength,corrosion resistance,and weldability,is extensively applied in aerospace,marine engineering,and advanced manufacturing.This study focuses on the microstructural uniformity and mechanical properties of TC4 ingots fabricated via the electron-beam cold hearth melting(EBCHM)process.A comprehensive analysis was performed using optical microscopy,scanning electron microscopy,electron backscatter diffraction,and energy-dispersive spectroscopy to investigate the ingot’s morphology,α-phase lamellar structure,and elemental distribution.Mechanical characterization included tensile testing,and microhardness and impact toughness assessments.Results reveal that EBCHM produces a well-defined and homogeneous microstructure,with the averageαlamellae thickness varying between 1.53 and 1.71μm and minimal fluctuations across the ingot regions,indicating high process consistency.Major alloying elements(Al and V)and impurity elements(O,N,H,C,and Fe)are evenly distributed,with no observable macrosegregation.The mechanical properties are stable and reliable,with a yield strength of 694.6-701.2 MPa,a tensile strength of 711.1-716.6 MPa,an elongation of 3.35%-3.84%,and an average impact toughness of 94.7 J/cm^(2).These results provide valuable data and technical references for the application of EBCHM in manufacturing premium-quality Ti-6Al-4V ingots. 展开更多
关键词 tc4 titanium alloy EBCHM microstructural characterization mechanical performance HOMOGENEITY
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Effect of Compound Energy Field with Laser and Ultrasonic Assisted Molding on Bending Performance of TC4 Titanium Alloy
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作者 GAO Tiejun ZHAO Kexiang +2 位作者 LI Weijie WANG Kaifeng WANG Xiaokang 《Journal of Wuhan University of Technology(Materials Science)》 2025年第3期852-858,共7页
Aiming at solve the difficulty and low dimensional accuracy in bending titanium alloy specimens at room temperature,we proposed a compound energy field(CEF)with laser and ultrasonic forming method.Through the conventi... Aiming at solve the difficulty and low dimensional accuracy in bending titanium alloy specimens at room temperature,we proposed a compound energy field(CEF)with laser and ultrasonic forming method.Through the conventional bending,laser-assisted energy field bending and CEF-assisted bending experiments on TC4 titanium alloy,the effects of bending force,laser-assisted energy field and CEF on the springback angle and fillet radius of TC4 titanium alloy specimens in V-shape bending were analyzed.The impact of the CEF-assisted bending process on the microstructure of TC4 titanium alloy was also investigated.The results show that CEF-assisted bending process has the advantages of high energy density,simple operation process and small influence area of the microstructure performances.It is effective in reducing the springback and fillet radius of bending specimens.Thus,CEF-assisted bending effectively improves the formability and surface quality of titanium alloy specimens. 展开更多
关键词 tc4 titanium alloy laser and ultrasonic compound energy field bending performances MICROSTRUCTURE
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Microstructure and mechanical properties of TC4 titanium alloy laser beam welded joint 被引量:2
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作者 Zhang Shuquan Wang Shouwu +3 位作者 Wang Liyue Xu Kai Ge Junwei Zhang Wei 《China Welding》 2024年第4期58-64,共7页
The fiber laser welding tests for 3 mm thick TC4 titanium alloy plates are carried out,and the microstructures of the joints are analyzed by the OM and SEM,and the mechanical properties of the joints are described by ... The fiber laser welding tests for 3 mm thick TC4 titanium alloy plates are carried out,and the microstructures of the joints are analyzed by the OM and SEM,and the mechanical properties of the joints are described by tensile and hardness tests,and the SEM morpho-logies of the tensile fracture are observed.The results show that the weld zone is composed of columnarβphase with coarse grains and acicular martensiteα',and small secondaryα'phases in different directions are formed acicular martensiteα'.The microstructure at the boundary between the HAZ and the weld is composed ofα'andαphases,the microstructure at the boundary between the HAZ and the base metal is composed of the initial(αandβ)andαphases,and the microstructure of the middle transition zone of the HAZ is composed of a small amount ofα'andαphase of high temperatureβphase’transformation and initial(αandβ)phases.The average tensile strength of TC4 titanium alloy laser beam welded joints is 1056 MPa,and the average elongation is 9.0%,which are lower than the tensile strength and the elongation of the base metal respectively.The fracture is ductile fracture,and the hardness of the weld zone is the highest and that of the HAZ is the lowest. 展开更多
关键词 tc4 titanium alloy laser beam welded joint MICROSTRUCTURE mechanical properties fracture morphology
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Hot deformation behavior and microstructure evolution of TC4 titanium alloy 被引量:22
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作者 孙圣迪 宗影影 +1 位作者 单德彬 郭斌 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2010年第11期2181-2184,共4页
The hot deformation behavior of Ti-6Al-4V (TC4) titanium alloy was investigated in the temperature range from 650℃ to 950℃ with the strain rate ranging from 7.7×10^-4 s^-1 to 7.7×10^-2 s^-1. The hot tens... The hot deformation behavior of Ti-6Al-4V (TC4) titanium alloy was investigated in the temperature range from 650℃ to 950℃ with the strain rate ranging from 7.7×10^-4 s^-1 to 7.7×10^-2 s^-1. The hot tension test results indicate that the flow stress decreases with increasing the deformation temperature and increases with increasing the strain rate. XRD analysis result reveals that only deformation temperature affects the phase constitution. The microstructure evolution under different deformation conditions was characterized by TEM observation. For the deformation of TC4 alloy, the work-hardening is dominant at low temperature, while the dynamic recovery and dynamic re-crystallization assisted softening is dominant at high temperature. 展开更多
关键词 tc4 titanium alloy flow stress hot tension MICROSTRUCTURE
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Effect of grain size on high-temperature stress relaxation behavior of fine-grained TC4 titanium alloy 被引量:18
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作者 He-li PENG Xi-feng LI +4 位作者 Xu CHEN Jun JIANG Jing-feng LUO Wei XIONG Jun CHEN 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2020年第3期668-677,共10页
In order to analyze the effect of grain size on stress relaxation(SR) mechanism,the SR tests of TC4 alloy with three kinds of grain size were performed in a temperature range of 650-750℃.A modified cubic delay functi... In order to analyze the effect of grain size on stress relaxation(SR) mechanism,the SR tests of TC4 alloy with three kinds of grain size were performed in a temperature range of 650-750℃.A modified cubic delay function was used to establish SR model for each grain size.A simplified algorithm was proposed for calculating the deformation activation energy based on classical Arrhenius equation.The grain size distribution and variation were observed by microstructural methods.The experimental results indicate that smaller grains are earlier to reach the relaxation limit at the same temperature due to lower initial stress and faster relaxation rate.The SR limit at 650℃ reduces with decreasing grain size.While the effect of grain size on SR limit is not evident at 700 and 750℃ since the relaxation is fully completed.With the increase of grain size,the deformation activation energy is improved and SR mechanism at 700℃ changes from grain rotation and grain boundary sliding to dislocation movement and dynamic recovery. 展开更多
关键词 stress relaxation grain size fine-grained microstructure tc4 titanium alloy DISLOCATION
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Improving performance of macro electrolyte jet machining of TC4 titanium alloy:Experimental and numerical studies 被引量:1
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作者 Minglu WANG Ningsong QU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2022年第8期280-294,共15页
Electrolyte jet machining(EJM)is a promising method for shaping titanium alloys due to its lack of tool wear,thermal and residual stress,and cracks and burrs.Recently,macro-EJM has attracted increasing attention for i... Electrolyte jet machining(EJM)is a promising method for shaping titanium alloys due to its lack of tool wear,thermal and residual stress,and cracks and burrs.Recently,macro-EJM has attracted increasing attention for its high efficiency in machining wide grooves or planes.However,macro-EJM generates large amounts of electrolytic products,thereby increasing the difficulty of rapid product removal with a standard tool and reducing the surface quality.Therefore,for enhanced product transport,a novel tool with a back inclined end face was proposed for macroEJM of TC4 titanium alloy.For comparison,also proposed were ones with a standard flat end face,a front inclined end face,and both front and back inclined end faces.The flow field distributions of all proposed tools were simulated numerically,and experiments were also conducted to validate the simulation results.The results show that one with a 5°back inclined end face can decrease the lowvelocity flow zone in the machining area and increase the high-velocity flow zone at the back end of tool,thereby promoting rapid product removal.A relatively smooth bright-white groove surface was obtained.The same tool also resulted in the highest machining depth and material removal rate among the tested ones.In addition,rapid product removal was beneficial to the subsequent processing.Because of its rapid product removal,the machining depth and material removal rate during deep groove machining using the tool with a 5°back inclined end face were respectively 7%and14%higher than those produced using a standard one.Moreover,the lowest bottom height difference of 0.027 mm can be obtained when the step-over value was 8.2 mm,and a plane with a depth of0.285 mm and a bottom height difference of 0.03 mm was fabricated using the tool with a 5°back inclined end face. 展开更多
关键词 Electrochemical machining Macro electrolyte jet machining Product removal tc4 titanium alloy Tool end structure
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Effect of high density electropulsing treatment on formability of TC4 titanium alloy sheet 被引量:19
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作者 宋辉 王忠金 高铁军 《中国有色金属学会会刊:英文版》 EI CSCD 2007年第1期87-92,共6页
An annealed TC4 titanium alloy sheet was treated by high density electropulsing(Jmax=(5.09-5.26)×103A/mm2,tp=110μs)under ambient conditions.The effect of electropulsing treatment(EPT)on the plastic deformation b... An annealed TC4 titanium alloy sheet was treated by high density electropulsing(Jmax=(5.09-5.26)×103A/mm2,tp=110μs)under ambient conditions.The effect of electropulsing treatment(EPT)on the plastic deformation behavior of TC4 titanium alloysheet was studied using uniaxial tension tests.The experimental results indicate that electropulsing treatment significantly changesthe mechanical properties of sheet metal:the uniform elongation is increased by 35%,the yield stress is decreased by 19.8%and theyield to tensile ratio is decreased by 17.6%.It is of significant meaning to improve the formability of TC4 titanium alloy sheet.Theoptical microscope and scanning electron microscope(SEM)were used to examine the changes of the microstructure and the fracturemorphology before and after the electropulsing treatment.It is found that recrystallization occurs in the sheet metal and dimples infracture surface are large and deep after the electropulsing treatment.The research results show that the electropulsing treatment is aneffective method to improve the formability of titanium alloy sheets. 展开更多
关键词 钛合金 电脉冲技术 机械性能 扫描电镜
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Double-sided gas tungsten arc welding process on TC4 titanium alloy 被引量:3
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作者 高洪明 白岩 杨天东 《中国有色金属学会会刊:英文版》 EI CSCD 2005年第5期1081-1084,共4页
TC4 titanium alloy was welded by double-sided gas tungsten arc welding(GTAW) process in comparison with conventional GTAW process, the microstructure and mechanical performance of weld were also studied. The results i... TC4 titanium alloy was welded by double-sided gas tungsten arc welding(GTAW) process in comparison with conventional GTAW process, the microstructure and mechanical performance of weld were also studied. The results indicate that double-sided GTAW is superior over regular single-sided GTAW on the aspects of increasing penetration, reducing welding deformation and improving welding efficiency. Good weld joint was obtained, which can reach 96.14% tensile strength and 70.85% elongation percentage of the base metal. The grains in heat-affected zone(HAZ) are thin and equiaxed and the degree of grain coarsening increases as one moves to the weld center line, and the interior of grains are α and α′ structures. The coarse columned and equiaxed grains, which interlace martensitic structures α′ and acicular α structures, are observed in weld zone. The fracture mode is ductile fracture. 展开更多
关键词 焊接工艺 定位焊接 钛合金 气压焊接 微观结构
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预测TC4钛合金高温流动行为的两种本构模型对比研究
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作者 贾海深 古妮娜 +2 位作者 罗文翠 张继林 易湘斌 《热加工工艺》 北大核心 2025年第16期104-111,共8页
为了建立准确预测钛合金TC4高温流动行为的本构模型,采用Gleeble-3800热模拟试验机,对其在温度550~950℃、应变速率0.01~1 s^(-1)下进行了热压缩试验。基于试验数据,建立了修正的Z-A和修正的J-C两种本构模型。通过统计参数相关性系数R... 为了建立准确预测钛合金TC4高温流动行为的本构模型,采用Gleeble-3800热模拟试验机,对其在温度550~950℃、应变速率0.01~1 s^(-1)下进行了热压缩试验。基于试验数据,建立了修正的Z-A和修正的J-C两种本构模型。通过统计参数相关性系数R、平均绝对相对误差ARRE和相对误差RE,对两种本构模型的可预测性进行了对比分析。结果表明:修正的J-C本构模型较准确地预测了TC4钛合金在上述变形条件下的流动行为,该模型的相关系数R、平均绝对相对误差ARRE和相对误差RE分别为0.9997、1.4536%和0.0457。研究结果为初期设计预测钛合金TC4高温流动行为的数值模型提供了一定参考依据,对其热成形工艺过程的数值模拟和参数优化方面具有重要意义。 展开更多
关键词 tc4钛合金 高温流动行为 本构模型
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TC4表面镍基涂层的微观组织及高温抗变形性能
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作者 付宇明 李长城 +1 位作者 闫茂荣 郑立娟 《华南理工大学学报(自然科学版)》 北大核心 2025年第1期108-117,共10页
为研究TC4表面激光熔覆涂层的耐高温抗变形性能,采用激光熔覆技术,以GH4169镍基高温合金粉末为基粉,HfC、ZrC、TaC、NbC过渡族碳化物为增强相,在TC4基材上制备不同比例的镍基金属-多元陶瓷复合涂层,通过组织表征和性能测试系统研究了不... 为研究TC4表面激光熔覆涂层的耐高温抗变形性能,采用激光熔覆技术,以GH4169镍基高温合金粉末为基粉,HfC、ZrC、TaC、NbC过渡族碳化物为增强相,在TC4基材上制备不同比例的镍基金属-多元陶瓷复合涂层,通过组织表征和性能测试系统研究了不同多元陶瓷粉末含量涂层的微观组织、涂层硬度和高温抗变形能力。研究结果表明:碳化物陶瓷增强相的添加使涂层微观组织细化,硬度得到提升,当陶瓷增强相添加量为15%时涂层硬度最高,是基材的2.54倍;随温度升高,纯镍基熔覆涂层内部枝晶组织发生了溶解和分离,并逐渐等轴化;添加15%陶瓷粉末的镍基熔覆涂层中出现了枝晶破碎情况,熔覆层中弥散分布的陶瓷增强相发生了聚集长大现象;在3种高温压缩试验温度(700、800、900℃)下,试件的最大等效应力和最大等效应变均出现在基材内部,相比于TC4试件,激光熔覆试件在涂层结合区产生应力突变,涂层的抗变形能力有所增强。 展开更多
关键词 tc4钛合金 激光熔覆 微观组织 显微硬度 高温压缩
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激光抛光TC4钛合金高粗糙度表面及表面耐磨损行为
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作者 戴峰泽 安春桥 +2 位作者 霍坤 何娟 陈希章 《排灌机械工程学报》 北大核心 2025年第3期291-298,共8页
针对离心泵薄壁钛合金叶轮叶片表面粗糙度控制困难以及在使用过程中砂石对叶片表面的磨损问题,分别在氩气和空气氛围下采用纳秒脉冲激光器对铣削后具有高粗糙度的TC4钛合金表面进行抛光,发现在氩气氛围下能获得更好的抛光效果,能使工件... 针对离心泵薄壁钛合金叶轮叶片表面粗糙度控制困难以及在使用过程中砂石对叶片表面的磨损问题,分别在氩气和空气氛围下采用纳秒脉冲激光器对铣削后具有高粗糙度的TC4钛合金表面进行抛光,发现在氩气氛围下能获得更好的抛光效果,能使工件表面算术平均高度下降56.12%、表面硬度提高21.94%;而在空气环境下,工件表面获得了高硬度的氮化钛,表面算术平均高度下降了51.89%,硬度比原始表面提高了176.79%.摩擦磨损试验结果表明:原始的工件表面和氩气氛围下抛光的工件表面均以磨粒磨损为主,其中在氩气氛围下抛光的工件由于抛光过程中获得了硬度较高的α′-Ti马氏体,因此表面的磨痕宽度更窄;而在空气氛围下则由于重熔层获得了高硬度氮化钛使得工件表面平均动摩擦系数从0.46降至0.16,显著提高了工件表面的耐磨性,磨痕宽度大幅降低,在与GCr15陶瓷球对磨过程中工件表面则主要表现为黏着磨损. 展开更多
关键词 tc4钛合金 激光抛光 激光氮化 硬度 摩擦磨损
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高斯脉冲激光灼烧TC4钛合金时变温度场特性
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作者 李隆 贺政隆 +5 位作者 李昕阳 宁江浩 纪玉潇 杨恒鑫 石镨 张春玲 《应用光学》 北大核心 2025年第3期604-611,共8页
TC4钛合金具有优良的耐蚀性、低密度、高比强度及较好的韧性和焊接性等一系列优点,在航空航天领域起到越来越重要的作用。以有限元分析方法为基础,利用热传导方程对TC4钛合金圆盘温度场进行了数值计算。分析了脉冲激光加工金属材料的工... TC4钛合金具有优良的耐蚀性、低密度、高比强度及较好的韧性和焊接性等一系列优点,在航空航天领域起到越来越重要的作用。以有限元分析方法为基础,利用热传导方程对TC4钛合金圆盘温度场进行了数值计算。分析了脉冲激光加工金属材料的工作特点,建立了符合实际加工特点的热模型,数值分析了TC4钛合金温度场随激光功率、光斑半径及激光脉宽的影响规律。研究结果表明:若使用中心激光波长为1 064 nm,激光功率为2 kW,光斑半径为2 mm,激光脉宽为8 ms,脉冲重复频率为1 kHz,尺寸直径为Φ5.0 cm,厚度为5 mm的TC4钛合金,其在50 ms间具有的峰值温升为1 209.80 K;在相同条件下,当光斑半径分别为1.5 mm、2.0 mm、2.5 mm、5 mm时,钛合金端面的最高热形变量为30.033μm。研究结果将为激光加工钛合金时准确设置激光加工参数提供理论依据。 展开更多
关键词 激光技术 tc4钛合金 脉冲激光 温度场
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固溶时效工艺下TC4钛合金锻件残余应力分析及其参数优化
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作者 方秀荣 刘鑫乐 +2 位作者 刘军毅 徐慧慧 刘留 《热加工工艺》 北大核心 2025年第16期119-123,共5页
为改善固溶时效后TC4钛合金锻件残余应力的大小及分布,从而进一步提高锻件后续加工质量及其服役性能,首先建立了锻后固溶时效数值模型,并进行了实验验证,然后通过数值模拟分析了固溶温度、固溶时间、时效温度和时效时间对锻件残余应力... 为改善固溶时效后TC4钛合金锻件残余应力的大小及分布,从而进一步提高锻件后续加工质量及其服役性能,首先建立了锻后固溶时效数值模型,并进行了实验验证,然后通过数值模拟分析了固溶温度、固溶时间、时效温度和时效时间对锻件残余应力的影响规律,最后采用正交实验设计与极差分析法,确定了各工艺参数对锻件残余应力的影响程度,并得出最优工艺参数组。结果表明,随着固溶温度、时效温度以及时效时间的增加,可显著降低锻件中心部位的残余应力。此外,固溶温度对锻件残余应力的影响最为显著,其次是时效时间、时效温度、固溶时间,在固溶温度900℃、固溶时间80 min、时效温度500℃、时效时间8 h时锻件的残余应力最小,为生产实践提供合理依据。 展开更多
关键词 tc4钛合金锻件 固溶时效 残余应力 正交实验
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TC4钛合金钎焊界面组织及力学性能研究
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作者 张丽霞 丁彦华 +6 位作者 朱鑫鑫 张博彧 孙湛 常青 张博 钟素娟 龙伟民 《现代交通与冶金材料》 2025年第2期91-97,共7页
为了保证钛合金板翅式换热器中接头的高温强度要求,本文设计并制备了Ti_(23.75)Zr_(23.75)Ni_(23.75)Cu_(23.75)Sn_(5)高熵非晶钎料,并利用所制备钎料对TC4钛合金进行真空钎焊,对不同工艺参数下接头的显微组织和力学性能进行了研究。结... 为了保证钛合金板翅式换热器中接头的高温强度要求,本文设计并制备了Ti_(23.75)Zr_(23.75)Ni_(23.75)Cu_(23.75)Sn_(5)高熵非晶钎料,并利用所制备钎料对TC4钛合金进行真空钎焊,对不同工艺参数下接头的显微组织和力学性能进行了研究。结果表明,930℃/10 min的工艺条件下接头的组织主要由(Ti,Zr)_(2)(Ni,Cu)和少量的Zr_(5)Sn_(3)金属间化合物、α-Ti+(Ti,Zr)_(2)(Ni,Cu)共析组织及针状α-Ti组成;随着钎焊温度的升高,元素扩散更加充分,焊缝内部的脆性化合物相逐渐消失,形成以针状α-Ti为主的焊缝组织。随着保温时间延长,接头组织内部的针状α-Ti逐渐生长,保温时间过长会造成α-Ti组织粗大,对接头强度有害,970℃/30 min工艺条件下,最高室温抗剪强度与450℃高温抗剪强度分别为494 MPa与408 MPa;(Ti,Zr)_(2)(Ni,Cu)脆性相是接头的薄弱环节,接头断裂形式为脆性断裂。 展开更多
关键词 tc4钛合金 高熵非晶钎料 显微组织 力学性能
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碎钛料对TC4合金铸锭微观组织与力学性能的影响
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作者 贺同正 吴敬玺 +3 位作者 罗国军 沈选金 唐丽英 陈玉勇 《钢铁钒钛》 北大核心 2025年第2期39-45,82,共8页
采用钛板切边、钛屑、钛坯切头及高纯原料制备了TC4合金铸锭,从成分、微观组织、硬度等方面系统分析了不同类型碎钛料对离心铸造技术的适用性。结果表明,四类铸锭中N、O、H等杂质元素的含量均符合GB/T6614−2014要求;但是,由于碎钛料在... 采用钛板切边、钛屑、钛坯切头及高纯原料制备了TC4合金铸锭,从成分、微观组织、硬度等方面系统分析了不同类型碎钛料对离心铸造技术的适用性。结果表明,四类铸锭中N、O、H等杂质元素的含量均符合GB/T6614−2014要求;但是,由于碎钛料在不同的热加工过程中会发生物理和化学变化,从而对合金凝固过程产生重要影响,使铸锭微观组织和性能存在一定差异。四类铸锭的硬度均满足GB/T6614−2014要求,这进一步证实了离心铸造技术可以较好地适用于碎钛料回收。热处理后,4^(#)合金的微观组织均匀化程度显著改善,异常组织区域完全消失。真空气淬工艺Ⅰ处理后试样的硬度值(HRC)最大,为32.5。 展开更多
关键词 碎钛料 tc4合金 微观组织 硬度 真空热处理
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TC4钛合金热拉伸变形行为及本构模型的建立
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作者 刘大海 刘康 +2 位作者 杨亮 秦海 钱世伟 《精密成形工程》 北大核心 2025年第4期104-112,共9页
目的综合分析变形温度、应变速率和微观组织对薄板TC4钛合金变形行为的影响机理;考虑温度与应变速率的影响,建立适用于宽温度范围、低应变速率(准静态)条件的本构模型。方法在温度为25~900℃、应变速率为0.00053 s^(−1)和温度为700~900... 目的综合分析变形温度、应变速率和微观组织对薄板TC4钛合金变形行为的影响机理;考虑温度与应变速率的影响,建立适用于宽温度范围、低应变速率(准静态)条件的本构模型。方法在温度为25~900℃、应变速率为0.00053 s^(−1)和温度为700~900℃、应变速率为0.00023~0.00080 s^(−1)的条件下,进行0.6 mm TC4钛合金单轴热拉伸试验。通过观察材料热拉伸变形后的微观组织变化情况,研究微观组织对热拉伸性能的影响。基于Hooke定律和Grosman方程建立此合金的本构模型。结果当温度由25℃升高到900℃时,屈服点应变由1.21%降低至0.52%。在700~900℃和0.00023~0.00080 s^(−1)条件下拉伸时,温度对材料的流变应力影响最大。通过分析微观组织形貌可知,原始TC4钛合金板材存在沿轧制方向分布的(α+β)组织。在700℃、0.00026 s^(−1)条件下拉伸时,得到细小均匀的等轴(α+β)组织;当温度上升至900℃时,得到较为粗大均匀的等轴(α+β)组织。结论当TC4钛合金在高温、低应变速率(准静态)条件下变形时,高温软化作用大于形变硬化作用,温度对合金流变应力的影响占主导地位,但应变速率对流变应力也有一定的影响,证明TC4钛合金为温度应变速率敏感型合金。在700℃、0.00026 s^(−1)条件下拉伸时,材料微观组织均匀细小,其综合力学性能相对最好。基于Hooke定律和Grosman方程建立此合金在700~900℃和0.00023~0.00080 s^(−1)条件下的本构模型,相关性系数R大于0.96,证明该模型能较好地描述TC4钛合金在宽温度范围、低应变速率(准静态)下的高温变形行为。 展开更多
关键词 tc4钛合金 热拉伸 力学性能 微观组织 本构模型 低应变速率
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适用于高温精冲的TC4钛合金本构模型及损伤模型
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作者 刘艳雄 龚宇澄 +1 位作者 纪开盛 张涵 《塑性工程学报》 北大核心 2025年第10期136-143,共8页
在910℃下开展了应变速率为0.03、 0.06和0.09 s^(-1)的TC4钛合金拉伸实验研究,分析了应变速率对TC4钛合金力学性能的影响规律,构建了考虑应变量、应变速率和材料软化的材料本构模型;基于Oyane损伤模型,构建了用于TC4钛合金高温精冲工... 在910℃下开展了应变速率为0.03、 0.06和0.09 s^(-1)的TC4钛合金拉伸实验研究,分析了应变速率对TC4钛合金力学性能的影响规律,构建了考虑应变量、应变速率和材料软化的材料本构模型;基于Oyane损伤模型,构建了用于TC4钛合金高温精冲工艺的损伤模型。研究结果表明:当应变速率增加时, TC4钛合金的塑性变形性能降低,抗拉性能和屈服性能得以提升;与实验结果相比,构建的本构模型和损伤模型误差均小于5%,可以用于预测高温下TC4精密冲裁的变形行为。 展开更多
关键词 tc4钛合金 精密冲裁 高温拉伸 本构模型 损伤模型
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锥度球头刀四轴铣削TC4残余应力梯度分布反解
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作者 周金华 齐琪 +1 位作者 任军学 詹梅 《中国机械工程》 北大核心 2025年第4期770-779,共10页
商用航空发动机大型复合材料风扇叶片前缘金属加强边的内外型面精加工采用定制化锥度球头刀四轴铣削方式完成,该阶段引入的加工残余应力常常引起过大的弯扭变形而导致零件尺寸超差。针对锥度球头刀四轴铣削钛合金TC4,提出了一种基于薄... 商用航空发动机大型复合材料风扇叶片前缘金属加强边的内外型面精加工采用定制化锥度球头刀四轴铣削方式完成,该阶段引入的加工残余应力常常引起过大的弯扭变形而导致零件尺寸超差。针对锥度球头刀四轴铣削钛合金TC4,提出了一种基于薄板加工变形测试的铣削残余应力梯度分布逆向辨识方法。采用双曲正切模型对铣削残余应力梯度分布进行参数化表征,将残余应力梯度分布的求解转换为对两个待定系数k和ω的反解,通过测试钛合金试块加工表面的残余应力计算确定模型系数k,通过测试钛合金薄板铣削弯曲变形挠度反解出模型系数ω,以此确定残余应力梯度分布曲线。开展了4组钛合金TC4试块铣削验证实验,测试结果表明,铣削残余应力梯度分布的平均预测准确率高达99.35%。与传统X射线测试法相比,所提出的方法避免了采用电解腐蚀剥层来测试亚表层残余应力,同时也充分考虑了铣削加工残余应力在已加工表面的分布不均匀性问题,即铣削加工残余应力离散度问题。 展开更多
关键词 锥度球头刀 钛合金tc4 四轴铣削 残余应力 逆向辨识 离散度
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Improvement of strength and ductility of TC4_(p)/AZ91D magnesium matrix composites by modifying the extrusion ratio
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作者 Zuying Yu Kaihong Zheng +4 位作者 Xintao Li Jun Xu Jianxin Sun Nan Zhou Fusheng Pan 《Journal of Magnesium and Alloys》 2025年第2期746-759,共14页
In this study,AZ91D(Mg-9Al-Zn)alloys reinforced with 2 vol%TC4(Ti-6Al-4V)particles fabricated by semi-solid stir casting were extruded at different ratios,resulting in observed grain refinement effects.The research fi... In this study,AZ91D(Mg-9Al-Zn)alloys reinforced with 2 vol%TC4(Ti-6Al-4V)particles fabricated by semi-solid stir casting were extruded at different ratios,resulting in observed grain refinement effects.The research findings demonstrate that both TC4 andβ-Mg_(17)Al_(12) phases contribute to promoting dynamic recrystallization(DRX)nucleation.With increasing extrusion ratio,theβ-phase(Mg_(17)Al_(12))gradually fractures into smaller particles,leading to progressive grain refinement.Furthermore,the transition from〈01-10〉fiber texture to non-basal texture in theα-Mg matrix after hot extrusion is attributed to improved DRX behavior and activation of non-basal slip.As the extrusion ratio increases,the tensile strength and elongation(EL)of TC4_(p)/AZ91D composite improve significantly,reaching optimum comprehensive mechanical properties at an extrusion of 40:1 with a yield strength(YS)of 257 MPa,an ultimate tensile strength(UTS)of 357 MPa,and an EL of 9.7%.This remarkable strengthening effect is primarily attributed toβ-phase reinforcement,grain refinement strengthening,and strain hardening. 展开更多
关键词 Magnesium matrix composites Mechanical properties tc4 titanium alloy Extrusion process
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超高真空环境下TC4钛合金和ZrO_(2)陶瓷的出气性能研究 被引量:1
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作者 焦纪强 蒙峻 +5 位作者 谢文君 刘建龙 魏宁斐 罗成 郭方准 王润成 《材料导报》 北大核心 2025年第1期281-285,共5页
内衬超薄壁真空腔体是离子加速器真空系统的核心元件,为了获得超高真空环境,对内衬材料的出气性能有较高要求。基于新型双通道出气率实验装置,完成了TC4钛合金和ZrO_(2)陶瓷在常温抽气、不同烘烤温度及烘烤结束后不同温度下的出气率实验... 内衬超薄壁真空腔体是离子加速器真空系统的核心元件,为了获得超高真空环境,对内衬材料的出气性能有较高要求。基于新型双通道出气率实验装置,完成了TC4钛合金和ZrO_(2)陶瓷在常温抽气、不同烘烤温度及烘烤结束后不同温度下的出气率实验;通过数值拟合方法获得了材料在不同加热温度下的出气率表达式;搭建了钛合金内衬超薄壁真空腔体压力实验装置,通过实验和仿真对比分析了不同工况下的压力分布。结果表明,烘烤温度越高,最终出气率越低,250℃烘烤时出气率较150℃时降低了约21%。经过高温烘烤后,当材料温度从50℃升高至210℃时,两种材料的出气率呈指数增加趋势,但钛合金的出气率低于陶瓷的出气率。常温抽气和烘烤过程中真空腔体压力梯度较小,对其进行升温时中间位置压力变化幅度较大,当温度为100℃,中间位置压力从初始值1.41×10^(-9)Pa升高至4.51×10^(-9)Pa;压力仿真结果和实验结果一致,平均相对偏差为6.86%。以上结果填补了钛合金和陶瓷出气率数据库,能够预测及评估真空腔体不同工况下的极限压力,为超高、极高真空获取提供数据支撑。 展开更多
关键词 离子加速器 超高真空 tc4钛合金 ZrO_(2)陶瓷 出气率 压力分布
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