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真空感应熔炼法制备了多晶Ni52Mn24.4Ga23.6合金,对多晶合金进行了DSC分析和显微组织观察;采用粉末压缩压制的方法制备了粘结Ni52Mn24.4Ga23.6磁体;通过X射线衍射分析,讨论了外应力场和磁场对粘结Ni52Mn24.4Ga23.6磁体马氏体相变的影响;测量了粘结Ni52Mn24.4Ga23.6磁体在磁场下的磁诱发应变.结果表明:室温时粘结磁体在1.2T的磁场下能产生150ppm的饱和伸长应变. 相似文献
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研究了铸态及快淬Ni50Mn26Ga19Fe5掺杂合金的磁致应变性能.结果表明,掺Fe的Ni-Mn-Ga合金也具有典型的热弹性马氏体相变过程和磁转变过程,但铸态合金的结构为7层调制型马氏体(7M),而快淬合金的结构为14层调制型马氏体(14M).铸态合金最大磁致应变可达0.1%,快淬薄带合金最大磁致应变只能达到0.0095%.Ni50Mn26Ga19Fe5铸态合金比快淬合金有更大的磁致应变,说明掺杂元素Fe在Ni-Mn-Ga合金中的作用较为复杂. 相似文献
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Abstract: We present the results of investigations into the strain distributions in the adhesive layers of epoxy‐bonded aluminium–aluminium and aluminium–carbon fibre reinforced polymer (Al/CFRP) double‐lap shear joints. The area of the adhesive at the end of the overlap region, where high stresses are predicted and failure generally initiates, has been studied at high magnification. 2‐D maps of the longitudinal and engineering shear strains in this region have been obtained experimentally by using high magnification moiré interferometry (HMMI). These results have been compared with the strain maps predicted by 3D elastic and elasto‐plastic finite element (FE) modelling. Excellent agreement is seen between the experimentally measured and FE‐predicted strain distributions, thus validating both methods. In some cases, quantitative comparison of the strains along certain profiles is compromised by noise in the measurements, especially for the Al/CFRP joints, which experienced lower overall strains. The source of such errors is discussed in the paper. 相似文献
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锂离子电池用正极材料LixCo0.8N0.2O2 总被引:7,自引:0,他引:7
在控制结晶工艺合成LixCo0.8Ni0.2O2的基础上制备了锂离子电池正极材料LixCo0.8Ni0.2O2。能量散射谱分析结果表明活性材料中Co、Ni元素分布均匀。由于在控制结晶合成的前驱体Co0.8Ni0.2(OH)2中,Co、Ni均匀分布在M(OH)2中的M层,因此可以避免形成一般固溶体发生扩散性重组所需长时间的煅烧过程。扫描电子显微镜分析了表微观形貌的变化。X米衍射分析表明LixCo0.8Ni0.2O2为单一相的α-NaFeO2层状结构,不存在其它杂相;晶胞参数a和c随x变化经历了由小到大再变小的;c/a则经历了一个由大到小再变大的过程。 相似文献