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71.
Finite element analysis of the hip implant is conducted in this paper for representative femoral cross-section geometries and development of stress in the presence of bone cement is elucidated. Differences in cement stresses generated by varying implant cross-sections were compared with conventional features derived from representative implants. The analysis was performed under idealized implant assemblies by constraining the implant movement in the assembly. The cross-sections and implant geometries used are generic and intended to be representative of available geometries. This paper is a part of student research projects, prepared from a series of activities in biomedical implant research currently underway at Ohio Northern and Arkansas Tech Universities. 相似文献
72.
Examination of the wreckage of a light aircraft revealed that approximately 20 cm was missing from one tip of the aluminum
alloy propeller. Fractographic and metallographic examination of the remaining portion of the propeller revealed extensive
grain-boundary separation in the vicinity of the fracture, and grain edges and corners rounded by corrosion on the fracture
surface. Energy dispersive X-ray analysis (EDXA) revealed fluorine on, and in the vicinity of, the fracture surface. In the
ensuing litigation, it was asserted that the crash occurred because the propeller fractured in flight as the result of intergranular
attack caused by the use of a fluorine-bearing cleaner. 相似文献
73.
74.
对铜在酸性CuCl_2溶液中蚀刻反应机理论述,利用氧化-还原电动势原理,详细论述了Ni80Cr20合金在酸性CuCl_2溶液中化学蚀刻反应机理,以及影响蚀刻速度的因素,并对溶液中金属离子的存在形式作了验证。 相似文献
75.
76.
P. J. C. Skitt M. A. Javed S. A. Sanders A. M. Higginson 《Journal of Intelligent Manufacturing》1993,4(1):79-94
The potential of using artificially simulated neural networks as intelligent, adaptive process-monitoring devices is discussed. The investigation is considered as a method for automatic, intelligent exception reporting for quality control applications. The technique is also compared with the conventional statistical approaches of principal component analysis and Kohonen's feature map. The applications of the technique in aerospace and manufacturing environments are presented and a possible extension of the method to incorporate a diagnostic function is discussed.Seconded from Cheltenham and Gloucester College of Higher Education as a Royal Society/SERC Research Fellow at Smith's Industries Aerospace and Defence Systems, Bishop's Cleeve, Cheltenham, UK. 相似文献
77.
基于甲基异丁基甲酮于稀盐酸介质中定量地萃取Zn ̄(2+)与CNS ̄-形成的络阴离子。从而达到与共存的锰、镍、铝、铬的完全分离。在有氟化物、硫脲存在时Fe ̄(3+)、Cn ̄(2+)和Ag ̄+也不被萃取。有机相中的锌于PH5.5“六胺”缓冲介质中返萃取回水相,用EDTA滴定。在文中给定的条件下锌的一次被萃取率可达99%以上,成功地解决了锰铜基高阻尼合金中共存离子对锌量测定的干扰问题。 相似文献
78.
盐浓度对交联聚合物线团形态的影响 总被引:16,自引:1,他引:15
用核孔膜过滤法 (过滤体积对过滤时间作图 )、动态光散射法 (DLS)和扫描电镜法 (SEM )研究了交联反应前后盐 (NaCl)浓度变化对低浓度HPAM与AlCit形成的交联聚合物溶液 (LPS)中交联聚合物线团 (LPC)形态的影响。所用HPAM相对分子质量 1.1× 10 7~ 1.4× 10 7,LPS中HPAM与Al的质量比 2 0∶1,HPAM浓度 0 .1或 0 .2 g/L ,交联反应温度 40℃ ,时间 7天。实验结果表明 :①LPC的平均水力半径Rh(DLS测定值 )随交联反应时盐浓度的增大先减小后增大 ,盐浓度由 0 .5 g/L增加到 2 g/L时Rh 由 45 0nm迅速减小到 2 5 0nm ,盐浓度增加到 2 0 g/L时Rh达到最小值 16 0nm ,此后随盐浓度的继续增加Rh 有所增大 ;盐浓度 0 .5和 2 .0 g/L时Rh 的SEM测定值分别为45 0和 2 5 0nm ,与DLS结果一致。②交联反应完成后改变LPS的盐浓度 ,也可改变LPC的Rh 值 ,但改变幅度较小 ;盐浓度 0 .5 g/L时形成的LPS ,当盐浓度增加至 2 g/L时 ,Rh 值由 45 0nm减小至 35 9nm ,大于盐浓度 2 g/L时形成的LPS的Rh 值 (2 46nm) ;盐浓度 2 g/L时形成的LPS ,当盐浓度减少至 0 .5 g/L时 ,Rh 值由 2 46nm增大至32 6nm ,小于盐浓度 0 .5g/L时形成的LPS的Rh 值 (4 5 0nm)。用盐浓度改变引起LPC水化层厚度改变 ,线团收缩或舒张解释盐浓度改变时Rh 测定值的 相似文献
79.
In the present study, attempts are made to extend the application of the mechanical model for the fatigue crack initiation (FCI) and the FCI life formula of metallic notched elements in laboratory air to those in the corrosive environment. The test results and analysis of the corrosion FCI (CFCI) life of aluminum alloys and Ti---6A1---4V show that the expression of the CFCI life obtained by modifying the FCI life formula in laboratory air can give a good fit to the test results of the CFCI life. The salt water (3.5% NaCl) environment has no effects on the CFCI resistant coefficient compared with the FCI resistant coefficient in laboratory air. However, 3.5% NaCl environment greatly decreases the CFCI threshold of aluminum alloy, but has little effect on the CFCI threshold of Ti---6A1---4V. The loading frequency ranging from 1 Hz to 10 Hz has no appreciable effect on the CFCI life, and thus, the CFCI threshold of aluminum alloys investigated. Hence, the expression for the CFCI life of metallic notched elements proposed in this study is a better one, which reveals a correlation between the CFCI life and the governing parameters, such as, the geometry of the notched elements, the nominal stress range, the stress ratio, the tensile properties and the CFCI threshold. However, this new expression of the CFCI life needs to be verified by more test results. 相似文献
80.
Y. N. Lenets 《Fatigue & Fracture of Engineering Materials & Structures》1997,20(2):249-256
Abstract— The behaviour of fatigue cracks in an Al-alloy under cyclic compression, either with or without overloads, was studied. For constant-amplitude compressive cycling, a non-catastrophic (saturation) character of the fatigue crack behaviour was confirmed, with the final depth of a crack depending on the applied load level. Single (tensile or compressive) intermittent overloads were shown to re-activate a previously arrested crack while reversed (tensile—compressive or compressive—tensile) ones were also shown to maintain continual fatigue crack extension under otherwise fully compressive cycling. 相似文献