共查询到18条相似文献,搜索用时 140 毫秒
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本文对供应状态LY12CZ硬铝合金在未经任何超细预处理的情况下进行了超塑性变形的力学特性、显微组织方面的研究。确认LY12CZ硬铝合金在等温压缩变形中发生了动态再结晶,动态再结晶会诱发超塑性,使用新研制的D润滑剂,使其能在快速成形时有较好的超塑性能,在实际生产中有推广应用价值。 相似文献
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碳化硅增强LY12铝基复合材料的超塑性 总被引:2,自引:0,他引:2
本文研究了以搅拌铸造法生产的碳化硅颗粒增强LY12铝基复合材料(SiCp/LY12)的超塑性预处理工艺及超塑性变形条件。经均匀化退火—热反挤压—温轧—再结晶预处理后,SiCp/LY12复合材料具有较好的超塑性。在T=793K、ε0=6.4×10-4S-1的变形条件下,其最高延伸率达293%。并探讨了碳化硅颗粒在超塑性预处理及超塑性变形中的作用。 相似文献
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为了研究晶界形态及动态再结晶在超塑性形变中的作用,采用光学显微镜、扫描电镜,透射电镜,对硬铝LY12的超塑性形过程进行了观察,分析,提出金属材料的超塑性主要依靠晶界流态化区的粘性变形来实现,动态再结晶不是超塑性的一种机制。 相似文献
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本研究运用动态再结晶诱发超塑性的原理,对未经细化晶粒预处理的常规生产热轧态2091Al-Li合金直接进行高温拉伸,试验结果表明合金在470~530℃温度范围和2×10~(-4)~1×10~(-3)应变速率范围内具有超塑性,最大断裂延伸率达405%。根据光镜和电镜组织观察和真应力—真应变曲线的单一峰值和变形激活能随应变量增大而下降等特征,讨论了动态再结晶诱发超塑性的机制。 相似文献
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对热挤压FGH96合金棒材超塑性进行了研究,结果表明:挤压FGH96合金在1050℃和1100℃的变形温度下具有良好的超塑性,在变形温度为1100℃初始应变速率为3.33×10-4s-1进行超塑拉伸时,伸长率可以达到405%,流变应力降低到32MPa。显微组织分析表明,FGH96合金经控制冷却速度的预热处理后,合金中γ′相尺寸及间距较大,能够促进合金在后续变形过程动态再结晶的发生,并阻碍晶粒快速长大。FGH96合金在挤压变形后发生了明显的动态再结晶,但由于再结晶进行的不充分,晶粒内部仍存在大量变形亚结构,这种亚稳态组织在超塑变形过程中通过进一步回复和再结晶,可以获得平均晶粒尺寸为10μm左右的等轴、均匀、稳定的细晶组织,使合金具有良好的超塑性。 相似文献
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强电场对摩擦焊接头组织与性能的影响 总被引:1,自引:1,他引:0
为提高摩擦焊缝金属的变形能力,采用外加电场考察了摩擦焊缝金属的电塑性效应,利用金属组织观察、显微硬度测试及抗拉试验,定量分析了外加强电场对LY12铝合金摩擦焊缝组织与力学性能的影响,结果表明:外加强电场使焊缝金属组织轴向分布梯度减小,等轴性提高;不同焊接压力时,强电场使焊接接头的动态再结晶区宽度有不同程度的增大;在中等摩擦压力作用下,使近轴心线处的动态再结晶区宽度趋干均匀;此外,外加电场使接头焊合区硬度增加,并使焊接接头的硬度分布趋干均匀;采用强规范施焊时,外加电场提高了焊接接头的抗拉强度。 相似文献
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利用Gleeble-3500热模拟试验机对Mg-9Al-3Si-0.375Sr-0.78Y合金试样进行等温恒应变速率压缩实验,研究其在温度250~400℃、应变速率0.001~10s~(-1)条件下的热变形行为。结果表明:在热变形过程中,峰值应力随着应变速率的降低和温度的升高而减小,且峰值应力对应变速率的敏感性随着变形温度的下降而增强。建立了考虑应变的热变形Arrhenius本构模型,模型精度良好,在300,350℃及0.001~10s~(-1)范围内,模型的平均绝对误差分别为1.57%和1.76%;合金的平均变形激活能为183.58k J/mol,平均应变速率敏感指数为0.1616。热变形过程中,α-Mg相呈现明显的动态再结晶特征,β-Mg17Al12相尺寸减小且分布均匀,初生Mg_2Si相较小。在低温(250~300℃)变形时,动态再结晶仅发生在晶界处。在高温(350~400℃)变形时,初生α-Mg晶粒发生了明显的动态再结晶。随着温度的增加和应变速率的降低,再结晶程度提高,再结晶晶粒逐渐长大。 相似文献
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The dynamic recrystallization (DRX) behavior of a typical nickel-based superalloy is investigated by the hot compression tests. Based on the conventional DRX kinetics model, the volume fractions of DRX are firstly estimated. Results show that there is an obvious deviation between the experimental and predicted volume fractions of DRX when the forming temperature is below 980 °C, which is induced by the slow dynamic recrystallization rate under low forming temperatures. Therefore, the segmented models are proposed to describe the kinetics of DRX for the studied superalloy. Comparisons between the experimental and predicted results indicate that the proposed segmented models can give an accurate and precise estimation of the volume fractions of DRX for the studied superalloy. In addition, the optical observation of the deformed microstructure confirms that the dynamically recrystallized grain size can be well characterized by a power function of Zener–Hollumon parameter. 相似文献
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Double-pass hot compression tests were carried out over a wide range of holding time (0–180?s) and Zener-Hollomon parameter (1.6E15–1.3E20) to study the deformation behavior of cast Mg-8Gd-3Y alloy. The flow curves show obvious work hardening and strain softening stages, leading to the peak stress of double-pass hot compression. Holding time and Zener-Hollomon parameter can significantly affect the second pass peak stress. It is found that increasing the holding time can cause a higher peak stress in the second pass deformation. The second pass stress reaches the peak stress of 71?MPa at Zener-Hollomom parameter of 1.6E15. When the parameter rises to 1.3E20, the second pass peak goes up to 237?MPa. In addition, the second pass peak stress is significantly higher than the unloading stress, which is opposite to the flow behavior of aluminum alloys. Residual stored deformation energy caused by the first pass deformation could be consumed by metadynamic recrystallization. Therefore, more strain energy is required for subsequent dynamic recrystallization, resulting in hardening behavior. A hardening fraction is defined to describe the deformation behavior quantitatively, which shows a positive correlation with the metadynamic recrystallization fraction. The metadynamic recrystallization leads to grain growth at the inter pass holding stage, diminishing dynamic recrystallization nucleation positions in the second pass deformation. 相似文献
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Stefanie Hanke Ian Sena Rodrigo S. Coelho Jorge F. dos Santos 《Materials and Manufacturing Processes》2018,33(3):270-276
In friction surfacing (FS), material is deposited onto a substrate in the plasticized state, using frictional heat and shear stresses. The coating material remains in the solid state and undergoes severe plastic deformation (SPD) at high process temperatures (≈0.8 Tmelt), followed by high cooling rates in the range of 30?K/s. Dynamic recrystallization and the thermal cycle determine the resulting microstructure. In this study, Ni-based alloy 625 was deposited onto 42CrMo4 substrate, suitable, for instance, for repair welding of corrosion protection layers. Alloy 625 is known to undergo discontinuous dynamic recrystallization under SPD, and the resulting grain size depends on the strain rate. The coating microstructure was studied by microscopy and electron backscatter diffraction (EBSD). The coatings exhibit a fully recrystallized microstructure with equiaxed grains (0.5–12?µm) and a low degree of grain average misorientation. Flow lines caused by a localized decrease in grain size and linear alignment of grain boundaries are visible. Grain nucleation and growth were found to be strongly affected by localized shear and nonuniform material flow, resulting in varying amounts of residual strain, twins and low-angle grain boundaries in different regions within a single coating layer’s cross section.FS can be used to study dynamic recrystallization at high temperatures, strains and strain rates, while at the same time materials with a recrystallization grain size sensitive to the strain rate can be used to study the material flow during the process. 相似文献
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在变形温度为350~510℃、应变速率为0.001~10s-1条件下,在Gleeble-3500热模拟实验机上对AlMg-Si-Ti合金进行等温热压缩实验,以实验所得数据为基础,结合变形微观组织,确定了Al-Mg-Si-Ti合金热变形时发生动态再结晶的条件,建立了Al-Mg-Si-Ti合金动态再结晶峰值应变模型。采用加工硬化率的方法,利用lnθ-ε曲线的拐点特征和-(lnθ)/ε-ε曲线的极小值判据对再结晶峰值应变与临界应变关系进行了研究。结果表明:AlMg-Si-Ti合金热变形时在变形温度430~510℃、应变速率0.001~0.1s-1发生动态再结晶。Al-Mg-Si-Ti合金发生动态再结晶时的临界应变随应变速率的增大而增加,随变形温度的升高而降低。临界应变与峰值应变满足关系:εc=0.88εp。 相似文献