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X.Y. Xu W.J. Liu M.L. Zhong H.Q.Sun X.Y. Xu R. Z. Ba 《航空制造技术》2004,(Z1):79-81
采用同轴送粉方法,激光熔覆制备了WC增强Ni3Al金属间化合物基复合涂层,通过试验,优化了工艺参数,对激光熔覆涂层的成分、组织和硬度进行了测试和分析.结果表明,激光熔覆涂层无裂纹和气孔,与基体形成良好的冶金结合,WC颗粒的添加显著提高了涂层硬度. 相似文献
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Crack monitoring method based on Cu coating sensor and electrical potential technique for metal structure 总被引:1,自引:0,他引:1
Advanced crack monitoring technique is the cornerstone of aircraft structural health monitoring.To achieve real-time crack monitoring of aircraft metal structures in the course of service,a new crack monitoring method is proposed based on Cu coating sensor and electrical potential difference principle.Firstly,insulation treatment process was used to prepare a dielectric layer on structural substrate,such as an anodizing layer on 2A12-T4 aluminum alloy substrate,and then a Cu coating crack monitoring sensor was deposited on the structure fatigue critical parts by pulsed bias arc ion plating technology.Secondly,the damage consistency of the Cu coating sensor and2A12-T4 aluminum alloy substrate was investigated by static tensile experiment and fatigue test.The results show that strain values of the coating sensor and the 2A12-T4 aluminum alloy substrate measured by strain gauges are highly coincident in static tensile experiment and the sensor has excellent fatigue damage consistency with the substrate.Thirdly,the fatigue performance discrepancy between samples with the coating sensor and original samples was investigated.The result shows that there is no obvious negative influence on the fatigue performance of the 2A12-T4 aluminum alloy after preparing the Cu coating sensor on its surface.Finally,crack monitoring experiment was carried out with the Cu coating sensor.The experimental results indicate that the sensor is sensitive to crack,and crack origination and propagation can be monitored effectively through analyzing the change of electrical potential values of the coating sensor. 相似文献
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热致变色涂层技术是航天器热控分系统的一项重要技术,对于未来航天器执行多任务、适应空间复杂多变的热环境具有重要意义。文中分析了航天器热控对热致变色涂层技术的需求,介绍了热致变色涂层的技术原理和国内外研究情况。在此基础上,总结了热致变色涂层技术的发展规律及趋势,并对我国热致变色涂层技术的后续发展提出了建议。 相似文献
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周雅 《南昌航空工业学院学报》2000,14(1):55-59
如果对粉末涂装系统技术或合作缺乏足够认识,生产不出高质量的产品,势必有被淘汰的一天。本文叙述了粉末涂料、喷粉设备、施工环境及设备使用维护等有关问题,以帮助使用者作出正确地选择。 相似文献
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分析了引起复合材料舱体软木粘贴质量问题的原因。按GD414和717胶的技术条件要求,对HYJ-51、J-48胶与GD414、717胶进行对比,选用HYJ-51胶并进行工艺适用性改进,如延长胶粘剂适用期等。探索了口框局部缺陷修补方法、基材表面处理、加压方式。通过软木粘贴工艺的改进,提高了口盖与口框的装配质量、软木粘贴质量、软木外表面涂层附着质量。 相似文献
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《中国航空学报》2021,34(10):103-114
An efficient method was proposed to prepare high-performance conductive Aramid-Carbon Blend Fabrics (ACBF) with cobalt–nickel (Co-Ni) alloy coatings, which is conducive to industrial production. The grid-like substrate composed of aramid and carbon fibers was innovatively used in flexible Electromagnetic Interference (EMI) shielding materials. The natural network structure is advantageous to the uniform deposition of metal particles to the establishment of conductive pathways subsequently in order to improve conductivity. The induction of a synergistic effect from Electromagnetic (EM) wave-reflection and EM wave-absorption through the whole carbon-Co-Ni-ternary system notably enhanced the EMI Shielding Effectiveness (SE) value to an average of 42.57 dB in the range of 30–6000 MHz. On the other hand, together with the inherent toughness of the alloy coatings, the tensile strength of the aramid fibers used for bulletproof made a significant contribution to the desired mechanical properties. The light weight of the resultant composite made it applicable to aerospace vehicles simultaneously. X-ray Photoelectron Spectroscopy (XPS) was conducted to investigate the variations of elements and groups on the sample surface in pre-treating process. The elemental components and surface morphologies of fabric samples during different stages of the process were investigated by Scanning Electron Microscope (SEM) and Energy Dispersive spectrometer (EDX) measurements. X-Ray Diffraction (XRD) results indicated that the obtained Co-Ni alloy coating had a combined Hexagonal Closed-Packed (HCP) and Faced-Centered Cubic (FCC) crystalline phase. The relatively high corrosion resistance demonstrated in different acid and alkaline conditions was instrumental in more complex environments as well. 相似文献
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SRB、G86涂层和铝阳极化着(黑)色是卫星表面热控用的材料。在轨道上,它们将直接与空间等离子体环境相接触,因此它们表面积累电荷的性质对是否会由它们引发放电、起弧、击穿等物理效应是至关重要的。为此在综合模拟空间环境下对它们的充电性能进行评价是十分必要的。通过实验评价可以正确了解它们的表面积累电荷的情况及其变化规律,为在工作中恰当的使用或改进提供科学依据。 相似文献