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从包括阴阳极、电位、偶对间距在内的材料自身因素,以及包括含氧量、温度、流动状态在内的环境因素两个方面,综述了异种结构材料电偶腐蚀的主要影响因素。探讨了目前国内外针对异种结构材料电偶腐蚀预防措施的研究现状,对比了国内外针对设计制造阶段和服役使用阶段的不同电偶腐蚀预防措施,最后指出我国在电偶腐蚀预防方面,规范、标准和措施匮乏以及存在的其他问题,并为接下来电偶腐蚀及防护技术的发展方向提出了建议,指出需要进一步研究实际结构因素对异种材料电偶腐蚀的影响机理和规律,并提出典型耦接件的腐蚀防护技术途径。 相似文献
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根据2214铝合金的材料特性,大型航空锻件的外形尺寸构造,锻件的精度等级、冶金质量和等温成形工艺的特点,设计了应用等温成形工艺加工锻件的模具结构。通过模具型腔、飞边槽、导向、锁扣装置、测温、控温、保温、装夹方式、锻模选材、加热装置的设计与计算等,阐明了模具结构的特点。 应用该缎模,采用等温成形工艺,在液压机上成功的加工出等级高、冶金质量好的航空大型2214材料锻件。代表着该锻模的设计合理和计算精确。 相似文献
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自行车D型中轴棍结构复杂,制造精度要求高。此文从材料选择、坯料制造、设备选型等方面阐述了D型中轴棍冷挤压成形工艺;对冷挤压模具结构及工作原理、凹模芯的设计及加工也做了详细介绍。 相似文献
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研究了黄铜 /紫铜 ,黄铜 /白铜复合板带室温轧制成形工艺 ,借助金相显微镜、扫描电镜、电子探针分析了复合工艺参数对轧制复合后的复合板结构强度的影响 ,确定了最佳复合工艺 ,并对结合机制进行了探讨 相似文献
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分析了摩托车油箱外壳体采用聚氨酯凸模整体冲压成形的工艺过程和特点,介绍了聚氨酯凸模的变形特点,给出了相应的模具结构及设计要点,提出了该方案今后的发展思路。采用这种结构和设计方法,能简化模具制造工艺,优化产品工艺,提高材料利用率,降低模具成本。 相似文献
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Jayanthi Parthasarathy Binil Starly Shivakumar Raman 《Journal of Manufacturing Processes》2011,13(2):160-170
CAD/CAM-based layered manufacturing and additive manufacturing techniques of metals have found applications in near-net-shape fabrication of complex shaped parts with tailored mechanical properties for several applications. Especially with the onset of newer processes such as electron beam melting (EBM) and direct metal laser sintering (DMLS), revolutionary advances may be achieved in material substitution in the medical implant industry. These processes must be suitably developed and tested for the production of medical grade substitutions. In this article, we discuss a design process for creating periodic cellular structures specifically targeted for biomedical applications. Electron beam melting is used to fabricate the parts. Evaluation of the mechanical properties is performed and compared with design parameters. Compression tests of the samples show effective stiffness values ranging from 0.57 (±0.05) to 2.92 (±0.17) GPa and compressive strength values of 7.28 (±0.93) to 163.02 (±11.98) MPa. Substituting these values for simulation of biomechanical performance of patient-specific implants illustrates the compatibility and matched functional performance characteristics of highly porous parts at a safety factor of 5 and an effective reduction in weight. These developments are unique for the construction of maxillofacial and craniofacial implants. The novel design strategy also lends itself very well to metal additive manufacturing technologies. Implants designed and fabricated with this design strategy and manufacturing process would have mechanical properties equivalent to the part they replace and restore better function and esthetics as against the currently used methods of reconstruction. Suitable examples of a titanium porous cranioplasty plate and a sandwich structure are illustrated. 相似文献
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Sandwich panels are commonly used in various applications to improve the stiffness-to-weight ratio of structure components. While producing flat sandwich panel is relatively straightforward, manufacturing of shaped sandwich components can be a challenging task. This paper presents the use of hydroforming technique in forming bi-layered and sandwich materials with an open-cell foam core. Hydraulic bulge experiments were conducted to form bi-layered and sandwich blanks into a dome shape. Various failure modes were observed from the experiments. Finite element simulations were conducted to understand the different failure mechanisms that could occur during the deformation process. The investigation can facilitate the selection of geometry and property of the constituents of the sandwich material for successful hydroforming. 相似文献
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先简要介绍新型智能材料、即磁粘弹性体的制备;再介绍磁粘弹性材料的力学性能实验,给出其拉伸、压缩及动力学试验结果,说明大小变形时的特性;最后介绍磁粘弹性材料在微振动控制方面的应用,通过可控复合结构的分析与计算,得到夹层梁与夹层板微振动的均方根速度谱指标,说明磁粘弹性复合结构的微振动控制效果。 相似文献
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Sladjan Lazarevic Scott F. Miller Jingjing Li Blair E. Carlson 《Journal of Manufacturing Processes》2013,15(4):616-624
Mass reduction of automotive body structures is a critical part of achieving reduced CO2 emissions in the automotive industry. There has been significant work on the application of ultra high strength steels and aluminum alloys. However, the next paradigm is the integrated use of both materials, which poses a challenge of how to join the dissimilar materials. Friction stir forming is a new manufacturing process for joining dissimilar materials. The concept of this process is stir heating one material and forming it into a mechanical interlocking joint with the second material. In this research the process was experimentally analyzed in a position controlled robotic friction stir welding machine between aluminum and steel workpieces. New tool geometries were evaluated toward the goal of optimizing joint strength. The significant process parameters were identified and their optimized settings for the current experimental conditions defined using a design of experiments methodology. A scanning electron microscope was used to characterize the bonding and joint structure for single and multi-pin configurations. Two failure modes, aluminum sheet peeling and bonding delamination, i.e. braze fracture, were identified. It was found that the presence of zinc coating on the steel and overall joint geometry greatly affected the joint strength. The aluminum–zinc braze joint appears to be the largest contributor to joint strength for the single-pin joint configuration. The multi-pin geometry enabled a distribution of load to the four pins following fracture of the braze for increased joint toughness and ductility. Thus, the FSF method has been shown to exhibit potential for joining of aluminum to steel. 相似文献
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目的研究一种低成本轻质复合蒙布设计,为中小型飞艇尾翼提供蒙皮材料。方法通过材料选型、连接设计、典型的复合蒙布性能测试。结果实现了该型蒙布在某大型飞艇尾翼中的应用,表现出了良好的力学性能、可靠性与维修性。结论结构质量与同等强度的气囊材料相比约轻30%。同时,该型复合蒙布还可用于飞艇框架结构的装饰,具有较高的使用价值。 相似文献
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介绍了传统蜂窝夹层结构,它是由蜂窝芯材耦合面板/薄膜组合而成,具有优异的降噪特性。为进一步提升蜂窝夹层结构的降噪性能,结合多孔吸声原理及“吸/隔声结构功能一体化”概念,将多孔吸声材料填充至蜂窝芯中,形成了基于多孔吸声的蜂窝夹层结构,但中、低频降噪性能较差。结合微穿孔板、亥姆霍兹共振理论,开发了基于共振吸声的单自由度蜂窝夹层结构,由蜂窝芯材耦合穿孔面板/薄膜组合而成,提升了中、低频降噪特性,但是依旧存在降噪频带过窄的问题,只能在某段特定频率范围内表现出良好的降噪特性。为此,研发了基于共振吸声的多自由度蜂窝夹层结构,利用各层穿孔面板/薄膜和蜂窝结构特性,实现了不同频率噪声控制。最后总结了蜂窝夹层结构在国内外直升机被动噪声控制上的应用情况,展望了新型蜂窝夹层结构的发展趋势。 相似文献
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目的 分析某型飞机在使用中其方向舵第4悬挂点连接螺栓出现不同程度断裂损伤的原因,并进行设计改进。方法 从宏观和微观2个方面研究螺栓的断口形貌和特征,对螺栓材料进行金相组织分析和力学性能测试,与同类型飞机相同位置螺栓的结构和功能进行对比分析。结果 螺栓断口边缘无明显的腐蚀和氧化特征,无有害的夹杂物和磷化物,硬度及拉伸强度符合材料力学性能要求。该型飞机方向舵第4悬挂点连接螺栓的结构较同类型飞机相同位置的螺栓结构应力集中更加明显,材料强度更低,存在设计缺陷。结论 连接螺栓断裂性质为疲劳断裂,螺栓受到异常的拉伸和弯曲循环载荷作用是导致其疲劳断裂的主要原因。基于裂纹原因及性能对比分析提出的设计改进方案,在螺栓选材、强度、刚度和耐久性等方面符合飞机结构设计规范,经验证,满足飞机装配技术要求,实践表明,能够确保飞机寿命期的安全使用。 相似文献
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