High-temperature compressive properties of 20vol% volume fraction nano-Al2O3 particles reinforced aluminum matrix composite
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摘要: 为提高铝基材料的高温力学性能以满足其在573 K以上用于航空航天装备结构件的性能需求,采用高能球磨结合真空热压烧结工艺制备了体积分数高达20vol%的纳米Al2O3颗粒(146 nm)增强铝基复合材料,对其微观结构和高温压缩性能进行了研究。结果表明:纳米Al2O3颗粒均匀分散于超细晶铝基体中,且复合材料完全致密;该复合材料具有优异的高温压缩性能:应变速率为0.001/s时,473 K时压缩强度高达380 MPa,即使673 K时依然高达250 MPa,比其他传统铝基材料提高至少1倍;通过对其流变应力进行基于热激活的本构模型拟合可以发现,该复合材料具有高的应力指数(30)和表观激活能(204.02 kJ/mol)。这是由于高体积分数纳米颗粒能够有效钉扎晶界,并与铝基体形成热稳定的界面结合,显著提高复合材料的组织热稳定性,而且在变形过程中与晶界有效阻碍位错运动,显著提高复合材料的热变形门槛应力(在473~673 K时为190.6~328.4 MPa),其热变形过程可以由亚结构不变模型进行解释。Abstract: To improve the high-temperature mechanical properties of aluminum-based materials with the aim of satisfying application requirements for the structural components in aerospace above 573 K, a novel aluminum matrix composite reinforced with 20vol% volume fraction nano-Al2O3 particles (146 nm) was prepared via high energy ball milling followed by vacuum hot pressing, and its microstructures and high-temperature compressive properties were investigated. The results show that, nano-Al2O3 particles are uniformly distributed in the ultrafine-grained Al matrix, and the resultant composite is fully densified. The composite exhibits superior high-temperature compressive properties: As the strain rate is fixed as 0.001/s, the high-temperature compressive strength reaches 380 MPa at temperature of 473 K, still maintains a high value of 250 MPa when the temperature increased to 673 K, which is at least onefold higher than that of traditional Al-based materials. By establishing constitutive model based on thermal activation, it is also found that the composite shows high stress exponent which is 30 and high apparent activation energy which is 204.02 kJ/mol. This may be attributed to the addition of high volume fraction nanoparticles into Al matrix which not only anchors Al grain boundaries and enables thermal stable interface between nanoparticles and the Al matrix and thus significantly enhance the thermal stability of the microstructure, but also can impede the dislocation motion effectively as well as Al grain boundary, thereby increasing the threshold stress for hot deformation which ranges from 190.6 MPa to 328.4 MPa as the temperature is in the range of 473 K to 673 K. The hot deformation process of this composite can be properly explained by substructure invariant model.
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图 4 20vol%纳米Al2O3/Al复合材料不同倍数的TEM图像和Al基体晶粒尺寸统计:(a)低倍TEM图像;(b) 铝基体晶粒尺寸统计;(c) 高倍TEM图像;(d) Al2O3颗粒/铝基体界面HRTEM图像
Figure 4. TEM images and Al grain size statistics of 20vol% nano-Al2O3/Al composites: (a) Low magnification TEM image; (b) Grain size statistics of the Al matrix; (c) High magnification TEM image; (d) High resolution TEM (HRTEM) image of Al2O3 particle/Al interface
图 5 20vol%纳米Al2O3/Al复合材料不同温度和应变速率下高温压缩性能:(a)应变速率为0.1/s;(b)应变速率为0.01/s;(c)应变速率为0.001/s;(d)峰值应力对比
Figure 5. High temperature compressive properties of 20vol% nano-Al2O3/Al composites under different temperatures and strain rates conditions: (a) Strain rate of 0.1/s; (b) Strain rate of 0.01/s; (c) Strain rate of 0.001/s; (d) Comparison of peak stress
图 11 20vol%纳米Al2O3/Al复合材料在673 K、0.001/s变形后的TEM图像和电子衍射分析结果:(a) TEM图像;(b)对应于图11(a)圆形区域的电子衍射图谱;((c)、(e)、(g))分别为对应于图11(a)圆形区域的Al2O3颗粒/铝基体界面、铝晶界和铝晶粒内部的高分辨TEM图像;((d)、(f)、(h))分别对应于图11(c)、图11(e)和图11(g)正方形区域的反傅里叶变换图
Figure 11. TEM images and analysis results based on electron diffraction of 20vol% nano-Al2O3/Al composites after deformation at 673 K and strain rate of 0.001/s: (a) TEM image; (b) Electron diffraction pattern corresponding to circular area in Fig.11(a); ((c), (e), (g)) HRTEM images of Al2O3/Al interface, Al grain boundary and Al grain interior, respectively, corresponding to square areas in Fig.11(a); ((d), (f), (h)) Inverse fourier transform images corresponding to square area in Fig.11(c), Fig.11(e) and Fig.11(g), respectively
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