29 resultados para CATHODIC PROTECTION

em Chinese Academy of Sciences Institutional Repositories Grid Portal


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铜管一直是电厂凝汽器的主要应用管材,但由于其抗冲刷和抵御污染物腐蚀的能力差,特别不耐氨蚀,美国和欧洲大量使用不锈钢管替代铜管作为冷凝管,然而不锈钢管在我国的运用仅处于初步阶段。 常使用锌、铝阳极对铜管进行牺牲阳极保护,然而存在着电位差过大、阳极溶解过快的问题。铁基牺牲阳极与铜电位差适当、来源广泛、价格便宜,在一些工程上有所应用,但是目前针对铁基牺牲阳极的理论研究报道很少。 本文选用紫铜管、304不锈钢管作为实验用管材,首先运用实验室全浸实验、极化曲线和电化学阻抗研究了二者在海水和淡水中的腐蚀性能以及CO2、溶解氧对其腐蚀的影响。结果表明:CO2会加速二者的腐蚀,溶解氧却对它们的腐蚀影响不同,促进铜管的腐蚀却抑制不锈钢管的腐蚀;随浸泡时间的延长,紫铜管由于表面产物膜的生成耐蚀性提高,304不锈钢管的耐蚀性却降低;淡水中,304不锈钢管和紫铜管都具有很好的耐蚀性能。随后,运用失重法和极化曲线对比研究了紫铜管、304不锈钢管的氨蚀性能,运用SEM分析和电化学阻抗研究了紫铜在不同浓度氨溶液中的腐蚀机理。发现,304不锈钢管的耐氨蚀能力远远好于铜管;溶解氧是影响氨蚀的关键因素,其对二者氨蚀的影响也不同;紫铜管在低氨浓度和高氨浓度溶液中腐蚀机理和产物不同,低氨浓度时形成保护性的产物膜(CuO 和Cu(OH)2),高氨浓度时由活化溶解控制,生成可溶的[Cu (NH3)4]2+。 选用工业纯铁、35钢为牺牲阳极材料。恒电流实验结果表明它们具有良好的牺牲阳极性能;通过极化曲线和自腐蚀电位测试分析,认为将二者用于铜管牺牲阳极保护是可行的;实验室阴极保护效果测试表明,工业纯铁和35钢对紫铜管具有良好的保护效果,保护度达90%以上。

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随着人们对能源需求的不断增加,深海海洋油气开发已引起了人们越来越大的兴趣,随之而来的是对海洋构筑物的设计和防护提出了更高的要求。由于在传统的阴极保护工程设计中,大多采用实际测量或经验估计的方法来掌握电位分布规律,很难真实的反映构筑物的实际状态,为了确保安全,往往采用较大的安全系数,不但会造成金属材料的浪费,而且还会在构筑物的局部造成保护不足或过保护。 本文研究了边界元方法(BEM)利用数值仿真技术对阴极保护状态下的海洋构筑物的保护状态进行模拟,从而获得阴极保护状态下的金属材料的电位分布。采用常数单元对于二维问题进行了研究,推导出了边界积分方程的离散化形式,并结合阴极保护环境下的阳极和阴极的极化曲线作为边界条件,建立了线性方程组。采用Newton-Raphson 迭代法和分段拟线性化的方法对边界条件做了线性化处理,应用FORTRAN语言开发出阴极保护的边界元仿真求解程序CPBEM,并利用该程序选择合适的算例进行了验证,结果表明该程序是有效和可行的。 通过管线钢在不同温度海泥埋片的腐蚀失重实验,证明了如果有充足的氧的供给的情况下,温度每增加10oC,腐蚀速度便增加一倍。阴极保护系统数值仿真的精确度最主要的影响因素就是阴极和阳极的极化曲线。而金属材料的极化曲线往往受到多种环境因素的影响,本文系统的讨论了在海泥介质中两种管线钢的腐蚀行为,对管线钢极化行为产生影响的各种环境因素,以及这些因素与金属的腐蚀速度之间的关系。首次将灰关联分析的手段运用到海泥介质的腐蚀,研究了环境因素对于ERW,SML两种管线钢在海泥中的腐蚀速率的影响。

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A comparative investigation of hot dip Zn-25Al alloy, Zn-55Al-Si and Zn coatings on steel was performed with attention to their corrosion performance in seawater. The results of 2-year exposure testing of these at Zhoushan test site are reported here. In tidal and immersion environments, Zn-25Al alloy coating is several times more durable than zinc coating of double thickness. At long exposure times, corrosion rate for the Zn-25Al alloy coating remains indistinguishable from that for the Zn-55Al-Si coating of similar thickness in tidal zone, and is two to three times lower than the latter in immersion zone. The decrease in tensile strength suggested that galvanized and Zn-55Al-Si coated steel suffer intense pitting corrosion in immersion zone. The electrochemical tests showed that all these coatings provide cathodic protection to the substrate metal; the galvanic potentials are equal to - 1,050, - 1,025 and - 880 mV (SCE) for zinc, Zn-25Al alloy and Zn-55Al-Si coating, respectively, which are adequate to keep the steel inside the immunity region. It is believed that the superior performance of the Zn-25Al alloy coating is due to its optimal combination of the uniform corrosion resistance and pitting corrosion resistance. The inferior corrosion performance by comparison of the Zn coating mainly results from its larger dissolution rate, while the failure of the Zn-55Al-Si coating is probably related to its higher susceptibility to pitting corrosion in seawater.

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The method for the measurement of the pure mechanical wear loss for 321 stainless steel, 1045 steel and pure iron in the study of the synergy between corrosion and wear was studied, The methods studied included the measurement in distilled water, by cathodic protection and by adding inhibitor KI, and all were compared with the wear loss in air. The experiment showed that the pure mechanical wear losses and friction coefficients obtained by the three methods were close to each other and can be used to calculate the various wear components in the study of the interaction of corrosion and wear, but the measurements in distilled water for pure iron and 1045 steel are not recommended due to their corrosion.

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Experiments on the corrosion fatigue behaviour of welded joints of the steel for marine platform in air and seawater, and of the joints in seawater with cathodic protection, yielded data for linear regression to obtain fatigue life curves (Delta S-N-f). The laws of corrosion fatigue in welded joints of test steel are discussed with reference to those of A(587) and A(131) steel. In these experiments, the fatigue damage occurring at all welded joints around the weld interface resulted in the cracks and fractures. The fatigue life of the specimens in seawater with cathodic protection is longer than that in seawater Without protection.

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In this paper, it is reported for the first time that a carbon-supported Au (Au/C) catalyst for the cathodic catalyst in a direct formic acid fuel cell (DFAFC) was prepared using a polyvinyl alcohol (PVA) protection method. The results indicated that for oxygen reduction, the electrocatalytic activity of the Au/C catalyst prepared with the PVA protection method is much better than that of a Au/C catalyst prepared with the pre-precipitation method. This is due to the small average size and low relative crystallinity of the An particles in the Au/C catalyst prepared by the PVA protection method, compared to that of the Au/C catalyst prepared by the pre-precipitation method, illustrating that the average size and the relative crystallinity of the ALL particles has an effect on the electrocatalytic activity of the Au/C catalyst for oxygen reduction. In addition, because An has no electrocatalytic activity for the oxidation of formic acid, the Au/C catalyst possesses a high formic acid tolerance. After the electrocatalytic activity of the Au/C catalyst for the oxygen reduction is improved, it is suitable to be used as the cathodic catalyst in DFAFC.

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Orthogonal designs are used to investigate the main factors when doing experiments in which pulse bias is superimposed on d.c. bias during cathodic are deposition of TiN. Pulse peak, duty cycle, frequency, direct voltage, are current and pressure all are investigated when coating TiN on HSS substrates. Roughness, surface micrograph, microhardness and thickness are tested. By analysis of variance, it is shown that pressure and frequency are the main factors. R-a and droplet density of the film with (d.c. + pulse) bias decrease. A simple explanation for the result is suggested.

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Hypersonic vehicles represent future trends of military equipments and play an important role in future war. Thermal protection materials and structures, which relate to the safety of hypersonic vehicles, are one of the most key techniques in design and manufacture of hypersonic vehicles. Among these materials and structures, such as metallic temperature protection structure, the temperature ceramics and carbon/carbon composites are usually adopted in design. The recent progresses of research and application of ultra-high temperature materials in preparation, oxidation resistance, mechanical and physical characterization are summarized.

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A new idea of drag reduction and thermal protection for hypersonic vehicles is proposed based on the combination of a physical spike and lateral jets for shock-reconstruction. The spike recasts the bow shock in front of a blunt body into a conical shock, and the lateral jets work to protect the spike tip from overheating and to push the conical shock away from the blunt body when a pitching angle exists during flight. Experiments are conducted in a hypersonic wind tunnel at a nominal Mach number of 6. It is demonstrated that the shock/shock interaction on the blunt body is avoided due to injection and the peak pressure at the reattachment point is reduced by 70% under a 4A degrees attack angle.

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Experimental research on a 150 kW arc-heated plasma testing facility was conducted. Stable plasma jets with different gas compositions, temperatures and velocities were obtained at chamber pressure between 400 Pa – 100 kPa. Stagnation ablation experiments were conducted on samples of typical super alloys used for thermal protection systems. The microstructure and hardness of alloys before and after ablation were compared.