SiCp/2024铝基复合材料的超塑性变形行为研究

对经过热处理和冷轧后的体积分数为17％，尺寸为3．5μm的SiC颗粒增强2024铝合金薄板在753－853K范围内进行了超塑性实验研究. 结果在813K时以10^-1/S的变形速率下获得了259％的最大延伸率，最大应力敏感系数为0．25复合材料的变形激活能值在753－793K范围内为144kJ/mol，在813－853K内为202kJ/mol，接近纯铝的晶格扩散激活能值142kJ/mol。复合材料的变形机制主要为基体晶粒滑动机制。     

LC9铝合金热扭转晶粒细化

ＬＣ９铝合金在７７３Ｋ热扭转中显微组织由粗大的柱状晶转变为细等轴晶。研究表明：其晶粒细化的过程为：位错的聚集；亚晶网络的形成；亚晶界面两侧晶体位向差的增加；亚晶界转变为晶界。从而细晶网络形成。     

定向凝固NiAl-15Cr合金的微观组织与超塑性变形行为

研究了定向凝固NiAl-15Cr合金的显微组织和高温拉伸变形行为。结果表明:定向凝固Ni-25Al-15Cr合金由β-NiAl枝晶干、γ/γ＇枝晶间相和γ＇过渡层组成。合金在1123—1373 K、初始应变速率为1.67×10~(-4)—1.67×10~(-2) S~(-1)的条件下表现出超塑性变形行为。在1323 K和初始应变速率为8.35×10~(-3)s(-1)条件下获得的最大延伸率为280％,应变敏感指数m为0.22。通过变形过程中显微组织观察,对其超塑性变形行为的机理进行了初步的讨论。     

金属相变超塑性的研究进展

综述了国内外金属相变超塑性的研究现状,包括金属相变超塑性的实现条件、影响因素和太合金变形机制,提出了相变超塑性的研究方向.     

Temperature and grain size dependence of superplasticity in a Zn−0.3wt.%Al alloy

The superplastic deformation behavior of quasi-single phase Zn-0.3 wt. %Al was investigated. A series of load relaxation and tensile tests was conducted at various temperatures ranging from RT (20 °C) to 200 °C. The recently proposed internal variable theory of structural superplasticity was applied. The flow curves obtained from load relaxation tests were shown to consist of contributions from interface sliding (IS) and accommodating plastic deformation. In the case of quasi-single phase Zn-0.3 wt.% Al alloy with an average agrain size of 1 μm, the IS behavior could be described as a viscous flow process characterized by a power index of M_g=0.5. A large elongation of about 1400% was obtained at room temperature and the strain rate sensitivity parameter was about 0.4. Although relatively large-grained (10 μm) single phase alloy showed a high value of strain rate sensitivity comparable to that of fine-grained alloy at very low strain rate range, IS was not expected from the analysis based on the internal variable theory of structural superplasticity at room temperature. As the temperature increased above 100 °C, however, the contribution from IS was observed at a very low strain rate range. A high elongation of ∼400% was obtained in a specimen of 10-μm-grain-size at 200 °C under a strain rate of 2×10⁻⁴/sec. Jointly appointed at Center for Advanced Aerospace Materials (CAAM)     

Processing,deformation, and failure in superplastic aluminum alloys: Applications of orientation-imaging microscopy

The importance of grain size refinement in enabling superplasticity is reviewed, and the current understanding of grain boundary characteristics is summarized. The application of orientation-imaging microscopy (OIM) methods to the processing response and the deformation and failure modes in superplastic aluminum alloys are illustrated through microtexture analysis and determination of grain boundary characteristics in selected commercial materials. Continuous and discontinuous recrystallization reactions exhibit distinct microtextures and grain boundary characteristics. The application of OIM and microtexture analysis to the evaluation of both deformation and failure mechanisms during superplastic forming is illustrated. This paper was presented at the International Symposium on Superplasticity and Superplastic Forming, sponsored by the Manufacturing Critical Sector at the ASM International AeroMat 2004 Conference and Exposition, June 8–9, 2004, in Seattle, WA. The symposium was organized by Daniel G. Sanders, The Boeing Company.     

65Mn钢的组织超细化与超塑性

利用盐浴加热循环淬火对６５Ｍｎ钢进行奥氏体晶粒的超细化，并对晶粒细化后的６５Ｍｎ钢进行超塑拉伸试验。结果表明，热轧或正火态的６５Ｍｎ钢经８１０℃循环淬火３次，奥氏体晶粒即可细化至１３级，在温度６６０～７２０℃、变形速率０．５～３．７×１０（－２）ｍｉｎ（－１）范围内呈现超塑性，δ≥２００％，最高达２９４％，σ最低仅３８ＭＰａ，ｍ值为０．３８左右。     

Deformation of metallic glasses with special emphasis in supercooled liquid region

1　ＩＮＴＲＯＤＵＣＴＩＯＮＩｎｔｅｎｓｉｖｅｅｆｆｏｒｔｓｈａｖｅｂｅｅｎｃａｒｒｉｅｄｏｕｔｏｖｅｒｔｈｅｐａｓｔｄｅｃａｄｅｔｏｄｅｖｅｌｏｐｍｅａｎｓｔｏｓｌｏｗｄｏｗｎｔｈｅｐｈａｓｅｔｒａｎｓｆｏｒｍａｔｉｏｎｋｉｎｅｔｉｃｓｄｕｒｉｎｇｔｈｅ     

Superplastic behavior of Al-Cu-Li based alloy

The superplastic behavior was studied in an Al-4Cu-ILi-0.4Mg-0.4Ag-0.1Zr alloy. The alloys were manufactured both by＂ a conventional rolling route and a thermo-mechanical treatment route. The superplastic properties were evaluated as a function of temperature, strain rate, and processing history. Prior to thermo-mechanical processing, the alloys have elevated-temperature ductilities of 94% to 130%, strain rate sensitivities of about 0.25, and activation energies corresponding to lattice diffusion. After thermo-mechanical processing, the alloys have ductilities of 200% to 630%, strain rate sensitivity of about 0.42, and activation energies corresponding to grain boundary diffusion or a mixture of grain boundary diffusion and lattice diffusion. Skipping rapid recrystallization annealing can supply a higher value of elongation-to-failure.