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1.
The aim of this study was to determine the influence of severe plastic deformation processing and the changes in microstructure resulting therefrom on the corrosion resistance of an Al–Mg–Si alloy. The alloy was processed using incremental equal channel angular pressing, which caused a reduction in grain size from 15 to 0.9 µm. The grain refinement was accompanied by an increase in the number of grain boundaries and dislocations, and by changes in grain orientation. However, there was no change in the size and number of intermetallic particles, which presumably resulted in a constant number of galvanic couplings. Electrochemical experiments revealed only slight differences between the samples before and after processing. Higher potential transients/oscillations upon immersion and increased corrosion currents in the vicinity of corrosion potential point to slightly higher reactivity of the most refined material. This indicates that intermetallic particles are the most crucial microstructural elements in terms of corrosion resistance. Their impact exceeds that of grain boundaries, in particular, at the stage of corrosion initiation. The development of corrosion attack is controlled more by the microstructure of the matrix as the grain refinement resulted in a less pronounced corrosion attack in comparison with the coarse-grained sample.  相似文献   
2.
将冷轧Ti/Al层状复合材料在675~750 ℃下进行不同时间的退火处理,退火过程中钛和铝都保持过剩,研究了Ti/Al层状复合材料的界面微观组织演变。结果表明:Ti和Al的界面层由2个亚层组成,其中一个为紧密的TiAl3亚层,其微观结构为紧密的TiAl3层,其中分布着随机取向的充满Al的裂纹,另一个为颗粒状的TiAl3亚层,其微观组织结构是颗粒状的TiAl3分布在Al基体中。在不同的退火温度和时间条件下,紧密TiAl3亚层的厚度几乎没有变化,但是颗粒状亚层的厚度随着退火温度及时间的增加而增加;另外,界面层中的TiAl3颗粒的体积分数在不同的温度下均随着退火时间的延长而下降。因此提出了反应扩散模型来描述界面层的形成机理,在此模型中,TiAl3相是化学反应和扩散的结果,并且也考虑了TiAl3相的溶解。计算结果表明TiAl3相的形成与生长由化学反应控制,其等效厚度与退火时间之间遵循线性规律,这主要是因为Ti和Al原子能够快速地通过紧密的薄TiAl3亚层。  相似文献   
3.
In order to determine the effect of heat treatment on the mechanical and wear properties of Zn–40Al– 2Cu–2Si alloy, different heat treatments including homogenization followed by air-cooling (H1), homogenization followed by furnace-cooling (H2), stabilization (T5) and quench–aging (T6 and T7) were applied. The effects of these heat treatments on the mechanical and tribological properties of the alloy were studied by metallography and, mechanical and wear tests in comparison with SAE 65 bronze. The wear tests were performed using a block on cylinder type test apparatus. The hardness, tensile strength and compressive strength of the alloy increase by the application of H1 and T6 heat treatments, and all the heat treatments except T6, increase its elongation to fracture. H1, T5 and T6 heat treatments cause a reduction in friction coefficient and wear volume of the alloy. However, this alloy exhibits the lowest friction coefficient and wear volume after T6 heat treatment. Therefore, T6 heat treatment appears to be the best process for the lubricated tribological applications of this alloy at a pressure of 14 MPa. However, Zn–40Al–2Cu–2Si alloy in the as-cast and heat-treated conditions shows lower wear loss or higher wear resistance than the bronze.  相似文献   
4.
The correlations among the corrosion behaviour, grain-boundary microchemistry, and Zn content in Al–Zn–Mg–Cu alloys were studied using stress corrosion cracking (SCC) and intergranular corrosion (IGC) tests, combined with scanning electron microscopy (SEM) and high-angle angular dark field scanning transmission electron microscopy (HAADF-STEM) microstructural examinations. The results showed that the tensile strength enhancement of high Zn-containing Al–Zn–Mg–Cu alloys was mainly attributed to the high density nano-scale matrix precipitates. The SCC plateau velocity for the alloy with 11.0 wt.% Zn was about an order of magnitude greater than that of the alloy with 7.9 wt.% Zn, which was mainly associated with Zn enrichment in grain boundary precipitates and wide precipitates-free zones. The SCC mechanisms of different Zn-containing alloys were discussed based on fracture features, grain-boundary microchemistry, and electrochemical properties.  相似文献   
5.
To further improve the mechanical performance and reduce the percolation threshold by controlling microstructures, Al2O3-TiC composites containing 0-20 vol% TiC were fabricated via in situ reaction synthesis. Graphite (ATC) and carbon nanotubes (ATCT) were used as carbon sources. The composites were also fabricated via a conventional process using a TiC starting powder (AT). X-ray diffraction analysis and scanning electron microscopy observation results indicated successful fabrication of the composites with various microstructures. TiC particles in ATCT were completely dispersed at grain boundaries, whereas in ATC and AT, these particles were either intragranular or intergranular dispersed. The composites could be listed as follows, ATCT > ATC > AT, that is, in descending order of the reinforcing flexural strength and fracture toughness. The nanoindentation measurement indicated the optimum hardening effect of ATCT. The ATCT composite also exhibited the highest fracture toughness, which was 49% higher than that of the monolithic Al2O3. Crack deflection was considered as the main toughening mechanism while crack bridging behavior also occurred in ATCT. For a given TiC content, ATCT exhibited the lowest electrical resistivity, owing mainly to the complete grain-boundary dispersion of the relatively large TiC particles. The similarity of the Al2O3 grain size and TiC particle size of ATCT contributed to the lowest percolation threshold achieved (11.2%), which (to date) is the lowest value that has been reported for the Al2O3-TiC system.  相似文献   
6.
研究辊速差对连铸连轧7075铝板显微组织、织构及力学性能的影响。采用3种不同上辊/下辊转速比(ω/ω0,ω为上辊转速,ω0为下辊转速)1:1、1:1.2及1:1.4进行多次试验。结果显示,在最大辊速差条件下(ω/ω0=1:1.4),7075铝板在轧制方向的屈服强度和极限抗拉强度分别提高41.5%和21.9%。此外,当辊速比ω/ω0为1:1.4时,成品轧制板的平均晶粒尺寸减小36%,横剖面平均硬度增加约9.2%。织构研究结果显示,辊速差越大,成品各向同性及硬度越大。然而,采用不同辊速度的连铸连轧会导致变形板伸长率降低约6%。  相似文献   
7.
Titanium carbide (TiC) nanoparticles with well-designed exposed crystal planes perform intriguing prospects for functional and engineering applications. In this study, a simple and controllable in situ synthesis strategy was proposed for the synthesis of TiC nanoparticles with specific morphology. Reaction behaviors suggested that most of TiC nanoparticles were formed by an instantaneous reaction between Al3Ti and Al4C3 in the Al-rich melt and the resultant morphology was controlled by the discrepant growing rates of (100) and (111) crystal planes. In addition, a growth morphology control model was presented for the prediction and manipulation of the morphology of TiC nanoparticles by the doping of different alloying elements Me (Me = Cu, Mg, Mn, Zn, and Si). According to the morphological observations and density functional theory analyses including the interface energy, charge density differences, and orbital hybridization: Cu, Mg, and Zn atoms could stabilize the Al/TiC(111) interface, whereas Mn and Si atoms promoted the rapid growing and disappearance of the TiC(111) planes in the Al melt. This work provides a feasible way to intelligently design and manipulate TiC nanoparticles with desirable exposed crystal planes, and exhibits a promising prospect for personalized applications.  相似文献   
8.
The uniaxial tensile test of the 5A06-O aluminium–magnesium (Al–Mg) alloy sheet was performed in the temperature range of 20–300 °C to obtain the true stress–true strain curves at different temperatures and strain rates. The constitutive model of 5A06-O Al–Mg alloy sheet with the temperature range from 150 to 300°C was established. Based on the test results, a unique finite element simulation platform for warm hydroforming of 5A06-O Al–Mg alloy was set up using the general finite element software MSC.Marc to simulate warm hydroforming of classic specimen, and a coupled thermo-mechanical finite element model for warm hydroforming of cylindrical cup was built up. Combined with the experiment, the influence of the temperature field distribution and loading conditions on the sheet formability was studied. The results show that the non-isothermal temperature distribution conditions can significantly improve the forming performance of the material. As the temperature increases, the impact of the punching speed on the forming becomes particularly obvious; the optimal values of the fluid pressure and blank holder force required for forming are reduced.  相似文献   
9.
范祥娟  李文生  崔帅  李建军 《表面技术》2021,50(5):152-159, 191
目的 合理选用摩擦偶件材料,以减缓Ni3Al基涂层宽温域内的摩擦磨损.方法 分别以WC-Co和316L为摩擦偶件,研究25~800℃内其对Ni3Al基涂层润滑和磨损机理的影响.采用高温硬度仪测试摩擦偶件在不同温度时的硬度,采用附带能谱仪的扫描电子显微镜观察磨损表面、磨斑和磨屑的形貌并测试成分,采用拉曼散射仪测试磨损表面和磨斑的成分.结果 在25~800℃,随温度的升高,两种摩擦副的摩擦系数具有一致的变化规律.与WC-Co对摩时,涂层在各温度下均具有低磨损率,且随温度升高,磨损率呈下降趋势.在25~200℃,与316L对摩时,涂层主要表现为粘着磨损和磨粒磨损,而与WC-Co对摩时,涂层在高接触应力下发生塑性变形,抑制Ag润滑相析出和涂层剥落,使其较前者具有高摩擦系数和低磨损率.在400℃,与WC-Co对摩时,高接触应力下产生的摩擦热促使涂层发生轻微的氧化,形成NiO和NiCr2O4,使其减摩性能优于Ni3Al/316L摩擦副.在600~800℃,与316L对摩时,涂层由严重的粘着磨损转变为氧化磨损;而与WC-Co对摩时,涂层由氧化磨损和剥层磨损转变为氧化磨损.此外,800℃时,Ni3Al/316L摩擦副的摩擦磨损发生在光滑润滑膜与粗糙转移膜之间,而Ni3Al/WC-Co摩擦副发生在光滑的润滑膜与转移膜之间.结论 在25~800℃,涂层与316L和WC-Co对摩时均具有良好的减摩性能,且与WC-Co对摩时具有更优的耐磨性能.  相似文献   
10.
摘要:铝碳耐火材料是冶金连铸、铁水包、中间包等部位常用的耐火材料,因其使用环境恶劣,对强度、抗热震性、抗渣侵蚀性等各项性能的要求都较高。优化铝碳耐火材料的力学性能能降低因机械应力引发的物理损毁和热应力引发的热震损毁,直接影响使用寿命。优化耐火材料的原料是易实现且高效的研究方向。从制备铝碳耐火材料的3种原料出发,分别从催化改性结合剂、添加纳米碳源和使用高效添加剂3个角度介绍了铝碳耐火材料力学性能优化的研究进展。最后对利于铝碳耐火材料工业化生产的研究方向进行了建议和展望。  相似文献   
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