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1.
热挤压AZ31镁合金的组织结构与蠕变行为   总被引:1,自引:1,他引:0  
通过对热挤压态AZ31镁合金进行组织形貌观察、内摩擦应力测定及蠕变性能测试,研究了热挤压AZ31合金的组织结构和蠕变行为.结果表明:热挤压AZ31镁合金的组织具有带状结构特征,并沿轧制方向分布,且有β-Mg17Al12相在合金中弥散析出.蠕变期间,位错运动的内摩擦力有较强的温度敏感性,随温度增加,内应力值明显降低,致使合金具有较高的蠕变速率.合金在蠕变期间,大量位错的形成与运动是蠕变初期的变形机制;蠕变稳态阶段,高密度位错逐渐束集形成位错胞,进一步发生蠕变期间的动态再结晶.随裂纹在晶界处萌生使蠕变进入第三阶段,而裂纹沿晶界韧性撕裂扩展是合金的蠕变断裂机制.  相似文献   

2.
通过对等温锻造合金进行直接时效、蠕变性能测试和组织形貌观察,研究了微量元素P、B对GH4169合金组织结构及蠕变行为的影响.结果表明:添加微量P、B可促使粒状δ相在合金中析出,且沿晶界不连续析出的δ相可抑制晶界滑移,提高合金的蠕变抗力;在试验温度和应力范围内,测定出GH4169G合金具有较高的蠕变激活能Q=594.7 ...  相似文献   

3.
通过蠕变性能测试和组织形貌观察,研究了一种Re含量为4.5%Re(质量分数,下同)的镍基单晶合金的高温蠕变行为、变形和损伤机制。结果表明,4.5%Re合金在980℃/300MPa的蠕变寿命为169h。蠕变初期,合金中立方γ′相转变为垂直于应力轴的N型筏状结构。稳态蠕变期间,合金的变形机制为位错在基体中滑移和攀移越过筏状γ′相。蠕变后期,合金的变形机制为位错在基体中滑移和剪切进入筏状γ′相。由于γ基体通道较窄,位错在基体通道中滑移所需的阻力较大。剪切进入γ′相的110超位错可由{111}面交滑移至{100}面,形成K-W锁,从而抑制位错的滑移和交滑移,这是合金具有较好蠕变抗力的主要原因。主/次滑移位错的交替开动,可致使筏状γ′相扭曲,并促使裂纹在筏状γ/γ′两相界面萌生;裂纹沿垂直于应力轴方向扩展,直至断裂,这是合金的蠕变断裂机制。  相似文献   

4.
使用透射电镜(TEM)研究了Ti65合金在600~650℃、120~160 MPa条件下的蠕变变形行为及其微观变形机制。结果表明:初级蠕变变形机制主要由受攀移控制的位错越过α2相的过程主导;稳态蠕变阶段蠕变机制主要由受界面处扩散控制的位错攀移的过程主导,且应力指数为5~7。在初级蠕变阶段α2相与位错的相互作用是α2相对合金高温强化的主要方式,在稳态蠕变阶段沿α/β相界分布的硅化物阻碍位错运动与限制晶界滑移是硅化物对合金强化的主要方式。  相似文献   

5.
The microstructure, high strain rate superplasticity and tensile creep behavior of directionally solidified (DS) NiAl-Mo(Hf) alloy have been investigated. The alloy exhibits dendritic structure, where dendritic arm is NiAl phase, interdendritic region is Ni3Al phase, and Mo-rich phase distributes in the NiAl and Ni3Al phases. The alloy exhibits high strain rate superplastic deformation behavior, and the maximum elongation is 104.2% at 1373 K and strain rate of 1.04×10-2 s-1. The balance between strain hardening (by dislocation glide) and strain softening (by dynamic recovery and recrystallization) is responsible for the superplastic deformation. All the creep curves of the DS NiAl-Mo(Hf) alloy have similar shape of a short primary creep and dominant steady creep stages, and the creep strain is great. The possible creep deformation mechanism was also discussed. The creep fracture data follow the Monkman-Grant relationship.  相似文献   

6.
通过对热连轧GH4169合金进行固溶和时效处理、组织形貌观察和蠕变性能测试,研究了固溶和时效处理合金的组织结构和蠕变特征。结果表明,经固溶和时效处理合金由较大尺寸晶粒组成,并具有明显的孪晶特征,且细小γ′、γ″相在晶内弥散析出,可提高合金的蠕变抗力;在实验应力和温度范围内,测得该合金的蠕变激活能为537.8kJ/mol,且对施加应力和温度具有敏感性;在蠕变期间,热连轧GH4169合金的变形特征是位错的单双取向滑移和孪晶变形,随着蠕变进行,裂纹沿晶界萌生和扩展到发生沿晶断裂是该合金的蠕变断裂机制。  相似文献   

7.
The deformation mechanism in high-strain-rate superplastic P/M7475 before and after continuous dynamic recrystallization (CDRX) was investigated. The recrystallization process in P/M7475 differed from that in conventional superplastic material, I/M7475. In I/M7475, the fine-grained microstructure was obtained by static recrystallization before deformation. On the other hand, the substructure in P/M7475 evolved into fine grains during deformation by CDRX. The percentage of high-angle and random boundaries was low at an initial stage of deformation. However, it increased with strain in P/M7475. The microstructural change in P/M7475 influenced a deformation mechanism and affected grain boundary sliding (GBS). The ratio of contribution of GBS to total elongation was low at an early stage of deformation in P/M7475. However, it increased with deformation progressed. It is suggested that the deformation behavior in P/M7475 changed from dislocation creep to superplasticity as the dominant deformation mechanism changed to GBS. The activation energy for superplastic flow in P/M7475 was close to that for lattice self-diffusion in pure aluminum. It is therefore concluded that the dominant deformation mechanism after CDRX in P/M7475 is GBS accommodated by dislocation movement controlled by lattice self-diffusion, similar to that in I/M7475.  相似文献   

8.
通过对含4.5%Re/3.0%Ru单晶镍基合金进行高温蠕变性能测试,并采用扫描电镜(SEM)、透射电镜(TEM)对不同蠕变期间的试样进行组织形貌观察,研究了该合金的高温蠕变行为。结果表明,本实验所选用的单晶合金在高温蠕变期间具有良好的蠕变抗力,在1040℃/160MPa的蠕变寿命达到725h。高温蠕变初期,合金中γ′相沿垂直于应力轴方向转变成筏状结构,其稳态蠕变期间的变形机制是位错在基体中滑移和攀移越过筏状γ′相。高温蠕变后期,合金的变形机制是位错在基体中滑移和剪切筏状γ′相。位错的交替滑移使筏形γ′相扭曲,并在γ/γ′两相界面发生裂纹的萌生与扩展直至断裂,是合金在高温蠕变后期的断裂机制。  相似文献   

9.
目的 研究变应变速率高温变形过程中GH4169合金动态再结晶行为和晶粒组织的演变机理.方法 在不同变应变速率工况下对GH4169合金进行高温压缩实验,分析了变形参数对动态再结晶行为与晶粒组织的影响规律,建立变应变速率工艺下GH4169动态再结晶动力学和晶粒尺寸预测模型.结果 随着第一阶段真应变的增加或第一阶段/第二阶段...  相似文献   

10.
The superplasticity of Ti-43Al-9V-0.2Y alloy sheet hot-rolled at 1100 ℃ was systematically investigated in the temperature range of 750-900 ℃ under an initial strain rate of 10-4 s-1.A bimodal γ grain-distribution microstructure of TiA1 alloy sheet,with abundant nano-scale or sub-micron γ laths embed-ded inside β matrix,exhibits an impressive superplastic behaviour.This inhomogeneous microstructure shows low-temperature superplasticity with a strain-rate sensitivity exponent of m =0.27 at 800 ℃,which is the lowest temperature of superplastic deformation for TiAl alloys attained so far.The maximum elongation reaches ~360% at 900 ℃ with an initial strain rate of 2.0 × 10-4 s-1.To elucidate the softening mechanism of the disordered β phase during superplastic deformation,the changes of phase composi-tion were investigated up to 1000 ℃ using in situ high-temperature X-ray diffraction (XRD) in this study.The results indicate that β phase does not undergo the transformation from an ordered L20 structure to a disordered A2 structure and cannot coordinate superplastic deformation as a lubricant.Based on the microstructural evolution and occurrence of both y and β dynamic recrystallization (DR) after tensile tests as characterized with electron backscatter diffraction (EBSD),the superplastic deformation mecha-nism can be explained by the combination of DR and grain boundary slipping (GBS).In the early stage of superplastic deformation,DR is an important coordination mechanism as associated with the reduced cavitation and dislocation density with increasing tensile temperature.Sufficient DR can relieve stress concentration arising from dislocation piling-up at grain boundaries through the fragmentation from the original coarse structures into the fine equiaxed ones due to recrystallization,which further effectively suppresses apparent grain growth during superplastic deformation.At the late stage of superplastic de-formation,these equiaxed grains make GBS prevalent,which can effectively avoid intergranular cracking and is conducive to the further improvement in elongation.This study advances the understanding of the superplastic deformation mechanism of intermetallic TiAl alloy.  相似文献   

11.
采用Gleeble-1500D热力模拟试验机研究新型Al-Zn-Mg-Cu高强铝合金在变形温度为300~450℃,应变速率为0.001~10s~(-1)条件下的热变形组织演化。利用光学显微镜(OM)和透射电子显微镜(TEM)观察合金不同热变形条件下的组织形貌特征。结果表明:随着变形温度的升高和应变速率的减小,位错密度减小,亚晶粒尺寸增大;合金热压缩变形过程中主要的软化机制为动态回复和动态再结晶。变形温度为300~400℃时,主要发生动态回复;变形温度为450℃,应变速率为0.001~10s~(-1)时,软化机制以动态再结晶为主,存在晶界弓出、亚晶长大、亚晶合并3种再结晶形核机制。  相似文献   

12.
通过高温拉伸实验研究TC18钛合金在温度为720~950℃,初始应变速率为6.7×10~(-5)~3.3×10~(-1)s~(-1)时的超塑性拉伸行为和变形机制。结果表明:TC18钛合金在最佳超塑性变形条件下(890℃,3.3×10~(-4)s~(-1)),最大伸长率为470%,峰值应力为17.93MPa,晶粒大小均匀。在相变点Tβ(872℃)以下拉伸,伸长率先升高后下降,在温度为830℃,初始应变速率为3.3×10~(-4)s~(-1)时取得极大值373%,峰值应力为31.45MPa。TC18钛合金在两相区的超塑性变形机制为晶粒转动与晶界滑移,变形协调机制为晶内位错滑移与攀移;在单相区的超塑性变形机制为晶内位错运动,变形协调机制为动态回复和动态再结晶。  相似文献   

13.
脉中电流对2091铝锂合金动态再结晶动力学的影响   总被引:3,自引:0,他引:3  
研究了脉冲电流对2091铝锂合金超塑变形中动态再结晶及动力学的影响结果表明,脉冲电流加速动态再结晶,减小形核时的平均晶粒直径.脉冲电流能加快位错墙的形成并使其角度增大,使再结晶形核率提高.脉冲电流加快位错在晶界上的攀移及消失、减小形核界面两边的能量差,降低形核界面的迁移速率及再结晶形核的长大速率分析了脉冲电流作用下的动态再结晶动力学行为  相似文献   

14.
1.IntroductionVerysmallrecrystallizedgrainswereobservedintheadiabaticshearbandsinmetalswhentheywereheavilydeformedathighstrainrates,whichwerezonesofhighlylocalizedplasticdeformation[1~5].Pak[1]foundthatshearbandsinacommerciallypuretitaniumwereconsistedofsmallgrainsof5o~3Oonmindiameterwithwell-definedboundaries.Chokshi[2],And.ade[3jandHinesI4Jalsoobservedtherecrystal-lizedgrainswith1oO~2Oonmdiameterswithintheshearbandsofcopper.Cho151showedthattherewereequiaxedcellswiththesizesof2oo~5oonminth…  相似文献   

15.
脉冲电流对2091铝锂合金动态再结晶动力学的影响   总被引:6,自引:1,他引:5  
研究了脉冲电流对2091铝锂合金超塑变形中动态再结晶及动力学的影响,结果表明,脉冲电流加速动态再结晶,减少形核时的平均晶粒,脉冲电流能加快位错墙的形成并使其角度增大,使再结晶形核率提高,脉冲电流加快位错在晶界上的攀移及消失,减少形核界面两边的能量差,降低形核界面的迁移速率及再结晶形核的长大速率,分析了脉冲电流作用下的动态再结晶动力学行为。  相似文献   

16.
Effects of strain on microstructure behavior of 7050-H112 aluminum alloy was investigated by means of hot compression conducted at 450 °C and strain rate of 1 s−1. The true stress–true strain behavior shows that it appears dynamic soft after acquired peak stress. The microstructure evolutions are mainly characterized by dislocation substructures with low misorientations which increase with deformation at low to medium strains, but decrease at high strain. It is concluded that the main soft mechanism is dynamic recovery with partial dynamic recrystallization at low to moderate strain, and then dynamic recrystallization at high strain. At last, the substructure behavior which is mainly affected by dislocation migrations is discussed in detail. At low deformation, dislocation migration can destroy grain boundaries and their junctions, resulting in formation of low angle boundaries. However, the interactions of dislocations increase with increasing of deformation, leading to a evolution of high-angle boundaries.  相似文献   

17.
With a new two-pass deformation, a fine-grained AA7050 alloy was obtained owing to small particles which can affect the grain refinement. The banded structures were produced in the elongated grain interiors after the 1st-pass deformation at 300 °C. And deformation bands containing dislocation arrays and small spherical particles were obtained. A few new fined grains appeared along the elongated grain boundaries. After the 2nd-pass deformation at 430 °C, isolated chains of new fine grains were developed in the elongated grain interiors. The boundary glide and the increase of grain boundary misorientation due to cumulative strain could refine the elongated grains. The pinning effect of the particles accelerated the formation of deformation bands. The increase of deformation temperature promoted the rapid evolution of grain refinement during the deformation. The strength of the fine-grained AA7050 alloy was enhanced while the ductility was decreased.  相似文献   

18.
This paper focuses on the effect of deep cryogenic treatment (−196 °C) on microstructure and mechanical properties of AZ91 magnesium alloy. The execution of deep cryogenic treatment on samples changed the distribution of β precipitates. The tiny laminar β particles almost dissolved in the microstructure and the coarse divorced eutectic β phase penetrated into the matrix. This microstructural modification resulted in a significant improvement on mechanical properties of the alloy. The steady state creep rates were measured and it was found that the creep behavior of the alloy, which is dependent on the stability of the near grain boundary microstructure, was improved by the deep cryogenic treatment. For the AZ91 alloy, the results indicate a mixed mode of creep behavior, with some grain boundary effects contributing to the overall behavior. However for the deep cryogenic samples dislocation climb controlled creep is the dominant deformation mechanism. After the deep cryogenic treatment the sliding of grain boundaries was greatly suppressed due to morphological changes. As a result, the grain boundaries are less susceptible for grain boundary sliding at high temperatures. Dry sliding wear tests were also applied and the wear resistance of the alloy improved remarkably after deep cryogenic treatment.  相似文献   

19.
戴青松  欧世声  邓运来  付平  张佳琪 《材料导报》2017,31(14):143-146, 152
通过等温压缩实验、光学显微镜与透射电镜研究了变形温度300~450℃、应变速率0.01~1s-1、真应变0.36~1.2范围内变形条件对5083铝合金热变形组织演变的影响。结果表明:升高热变形温度或降低应变速率均可促进5083铝合金的动态再结晶发生,使变形后5083铝合金位错密度降低,再结晶晶粒尺寸增大;随着应变量的增加,变形后合金的位错密度降低,动态再结晶程度增大。根据唯象理论的指数模型,利用线性回归方法建立了5083铝合金动态再结晶晶粒度模型,模型计算值与实测值吻合良好,平均相对误差仅为4.6%。  相似文献   

20.
通过对一种等温锻造GH4169镍基合金进行直接时效处理,蠕变性能测试及组织形貌观察,研究了该合金的组织结构与蠕变行为。结果表明,GH4169合金的组织结构由γ基体,γ′相、γ″相和δ相组成,且各相之间保持共格界面。测定出合金在660℃/700MPa条件下的蠕变寿命为123h。合金在680℃/700MPa的蠕变寿命为39h,在实验温度和应力范围内,计算出直接时效合金的蠕变激活能为588.0kJ/mol。合金在蠕变期间的变形机制是位错滑移和孪晶变形,其中,沿晶界析出的粒状碳化物,可抑制晶界滑移,是使合金具有较好蠕变抗力的主要原因。随蠕变进行,开动的滑移系中位错运动至晶界受阻,并塞积于该区域引起应力集中,当应力集中值大于晶界的结合强度时,可促使其在与应力轴垂直的晶界处发生裂纹的萌生与扩展,直至断裂,是合金在蠕变期间的断裂机制。  相似文献   

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