Structure of Micro-nano WC-10Co4Cr Coating and Cavitation Erosion Resistance in NaCl Solution

Cavitation erosion （CE） is the predominant cause for the failure of overflow components in fluid machinery. Advanced coatings have provided an effective solution to cavitation erosion due to the rapid development of surface engineering techniques. However, the influence of coating structures on CE resistance has not been sys- tematically studied. To better understand their relationship, micro-nano and conventional WC-10Co4Cr cermet coat- ings are deposited by high velocity oxygen fuel spray- ing（HVOF）, and their microstructures are analyzed by OM, SEM and XRD. Meanwhile, characterizations of mechan- ical and electrochemical properties of the coatings are carried out, as well as the coatings＇ resistance to CE in 3.5 wt % NaC1 solution, and the cavitation mechanisms are explored. Results show that micro-nano WC-10Co4Cr coating possesses dense microstructure, excellent mechanical and electrochemical properties, with very low porosity of 0.26 4-0.07% and extraordinary fracture toughness of 5.58 4-0.51 MPa.m1/2. Moreover, the CE resistance of micro-nano coating is enhanced above 50% than conventional coating at the steady CE period in 3.5 wt % NaC1 solution. The superior CE resistance of micro- nano WC-10Co4Cr coating may originate from the unique micro-nano structure and properties, which can effectively obstruct the formation and propagation of CE crack. Thus,a new method is proposed to enhance the CE resistance of WC-10Co4Cr coating by manipulating the microstructure.

Protection Performance of Plasma Sprayed Al_(2)O_(3)-13 wt%TiO_(2) Coating Sealed with an Organic-inorganic Hybrid Agent

An organic-inorganic hybrid sealing agent was fabricated and used in the plasma sprayed Al_(2)O_(3)-13 wt%TiO_(2)coating,and conventional silicone agent was also used for comparison.Protection performance of the coatings was comprehensively evaluated based on both anti-corrosion and anti-biofouling properties.The results reveal that the sealing treatment is remarkably useful to decrease the porosity of the coating,and the porosity of the coating sealed with the hybrid agent is only 0.035%.Immersion corrosion test and Tafel polarization test reveal that the sealed coating with the hybrid agent exhibits a better corrosion resistance by compared with the coating sealed with silicone agent.The corrosion current density i_(corr) of the hybrid agent sealed coating is only 0.7×10^(-6)A·cm^(-2).Moreover,anti-biofouling tests both in the outdoor analogue hydraulic environment and in the natural marine environment prove that the mentioned novel coating presents a better combination of corrosion resistance and anti-biofouling property by compared with the other coatings,and it could be used as a protection of metal components in the marine environment.

Self - Crosslinking Behavior of Self - Emulsion Water - Based Polyure-thane Coating Agents

The relation between structures and properties of polyurethane are investigated by modern physical and chemical methods.The results obtained are as follows:the effects of the content of self-crosslinking agent on the properties of polyurethane,i.e.,dispersion stability,dynamical viscoelasticity and mechanical properties are discussed.It is found that the optimum molar ratio of epichlorohydrin and diethylenetriamine is 1:2.A mois-

Comparison of electrochemical properties of atmospheric pressure plasma coatings for Al_2O_3-3TiO_2 and CoNiCrAlY in sea water

To improve the durability of underwater rotating products,the corrosion characteristics in harsh marine environment were evaluated through various electrochemical experiments on the Al2O3-3TiO2 and CoNiCrAlY coating layers by atmospheric pressure plasma spray coating process.By evaluating the corrosion resistance of these materials,their applicability to environmentally friendly power generation equipment such as blades of tidal current turbines was examined.According to the Tafel analysis for micro-areas including the coating layer,the coating/metal interlayer and the base metal,the Al2O3-3TiO2 coating layer and the CoNiCrAlY coating layer show markedly lower corrosion current density than the base metal.The corrosion current density of the CoNiCrAlY coating layer (9.75316×10-8A/cm2) is about 1.6 times more than that of the Al2O3-3TiO2 coating layer (6.13139×10-8A/cm2).

X-ray diffraction study of effect of deposition conditions on α-β phase transition and stress evolution in sputter-deposited W coatings

Pure W and W-Cu-W trilayer coatings were deposited on an Fe substrate by d.c. magnetron sputtering. The α-β phase evolution, intragranular stress evolution in sputter-deposited W layer were investigated by x-ray diffraction. They are directly related to the film microstructure, density and adhesion. Therefore, control of the film stress and phase component transition is essential for its applications. The phase component transition from β-W to α-W and intragranular stress evolution from tensile to compressive strongly depend on the deposition parameters and can be induced by lowering Ar pressure and rising target power. The compressively stressed films with α-W phase have a dense microstructure and high adhesion to Fe substrate.

Influence of Microstructures on Thermal Shock and Sintering Behavior of YSZ-based Thermal Barrier Coatings

In this study, two thermal barrier coatings based on YSZ were produced by using a commercially available agglomerated and sintered powder and a special spray powder prepared by high energy ball milling. Both thermal barrier coatings exhibited similar overall porosities, but significantly different microstructures. Application of the special spray powder prepared by high energy ball milling led to a microstructure with numerous inclusions of semi-molten agglomerates, which introduced a plethora of clusters of fine pores into the coating and several more microstructural defects. This microstructure resulted in a significantly better thermal shock behavior compared to the conventional thermal barrier coating. The heat treatment of both thermal barrier coatings atθ=1150℃for t=100 h led to a sintering of both coatings. The results were reduced overall porosity and significantly increased fracture toughness. A correlation between the fracture toughness of both coatings after the heat treatment and the thermal shock life time could not be identified.

Coating Resistant Refractory Castables YB/T 4193-20091

1 Scope This standard specifies the term, definition, classification, technical requirements, test methods, quality appraisal procedures, packing, marking, transportation, storage, and quality certificate of coating resistant refractory eastables.

The Influence of Ceramic Coating on Fatigue Crack Growth Behaviour of X17CrNi15-2 Stainless Steel

Fatigue crack growth tests were carried out on the SEN B3 precracked specimens, with dimensions in accordance with ISO 12108 requirements. The specimens were made of martensitic stainless steel, X17CrNi15-2, and some of them were modified by the ceramic coating deposition surface treatment. The effects of ceramic coating, on the fatigue crack growth behaviour of hollow shaft specimens, were experimentally investigated. Fatigue crack growth rates, da/dN, were characterised, using the power law relationship between da/dN (in mm/cycle) and the stress intensity factor range, ΔK (in MPa∙m0.5). The two constants of the correlation are 7.9768 × 10−9 and 2.8107 for the parent material, and those for the coated material are 2.4391 × 10−9 and 3.1990, respectively. Microstructural analyses were carried out on the tested specimens, which shows that the maximum hardness of the ceramic coating is higher than that of substrate by a factor of ~3.2. The dimple fracture dominates the final fracture mechanism for the parent material, and the combination of fatigue, ductile fracture and cleavage dominates the final fracture mechanism for the coated material, based on the SEM analyses. EDS tests’ results reveal that the parent material specimen shows higher levels of C at matrix regions along with Fe- and O-rich regions, compared with the coated material specimen.

Microstructural Characteristics and Wear Performance of Plasma Sprayed Al_2O_3-13 wt. % TiO_2 Coating on the Surface of Extrusion Wheel

The conventional Al2O3-13 wt. % TiO2 composite ceramic coatings are fabricated by plasma spraying on the surface of extrusion wheel. The microstrueture, morphology and phase compositions of the substrate and coat- ing are investigated by using X-ray diffractometry （XRD） , scanning electron microsopy （SEM） and energy dis- persive spectroscopy （EDS）. Moreover, the microhardness of the substrate and the coating are investigated using Vickers mierohardness tester, the friction and wear behaviors of the substrate and the coating are investigated by using a block-on-ring tribometer under dry sliding conditions with the load of 245 N. The results show that both γ-Al2O3 and α-Al2O3 phases are observed in the as-sprayed coatings, the mian phase is γ-Al2O3. There are white particulates Al2O3 on its surface. The Al2O3-13 wt. % TiO2 coating possesses higher mierohardness which is about 1018HV and 1.6 times that of the substrate. The wear performance of coating is better than that of the substrate. In a practical application, the life of the extrusion wheel which is plasma sprayed Al2O3-13 wt. % TiO2 coating on the surface is 1.2 times that of the conventional extrusion wheel, and the life is about 330 h.

应用化疗泵持续滴注5-Fu联合CF和HCPT治疗消化系肿瘤的疗效观察

目的 :观察应用化疗泵持续滴注 5 Fu联合CF HCPT治疗消化系肿瘤的疗效和安全性。方法 :治疗组 5 0例消化道肿瘤应用化疗泵持续滴注 5 Fu联合CF HCPT与对照组 47例消化道肿瘤常规点滴 5 Fu联合CF及其它化疗药物进行对比观察。结果 :治疗组应用化疗泵持续滴注 5 Fu联合CF HCPT治疗消化道肿瘤的总有效率为 46 %,而对照组为 34 0 4%。结论 :应用化疗泵持续滴注 5 Fu联合CF HCPT治疗消化道肿瘤的有效率高 ,毒性反应小 ,化疗泵体积小 ,重量轻 ,携带方便 ,值得临床进一步推广。

cf-可膨胀类的逆极限运算的保持性

主要证明如下结果:设X=lim←{Xα,πβα,Λ},λ=|Λ|并且每个投射πα是开满映射,如果X是(遗传)λ-仿紧的且每个Xα是性质■(遗传性质■)的,则X是性质■(遗传性质■)的.■表示cf-可膨胀、θ-cf可膨胀、序列cf-可膨胀、离散cf-可膨胀、离散θ-cf可膨胀,离散序列cf-可膨胀6种性质之一.

先驱体浸渍-裂解法制备Cf/SiC复合材料

采用先驱体浸渍-裂解法制备了Cf/SiC复合材料.重点研究碳纤维类型对复合材料力学性能和断裂行为的影响.研究表明,采用先驱体浸渍-裂解法可制备出致密度较高的Cf/SiC复合材料.由于M40JB纤维的制备温度明显高于T300纤维的制备温度,因此与T300纤维相比,M40JB纤维具有较高的结晶度和较低的表面活性.结果,在复合材料制备过程中,M40JB纤维与基体的界面反应较弱,从而使复合材料呈现韧性断裂,具有较好的力学性能,其抗弯强度和断裂韧性分别为614.4 MPa和18.8 MPa·m1/2.而T300纤维则与基体发生较强的界面反应,导致纤维与基体间的界面结合过强,复合材料表现为脆性断裂.

升温速率对PIP工艺制备的3D-Cf/SiC复合材料性能及结构的影响

研究了不同升温裂解速率对PIP工艺制备的3D-Cf/SiC复合材料性能的影响。采用了3种升温制度,每次裂解时间分别为3 900 min、1 500 min和1 000 min。实验发现3种升温制度下制备的材料的力学性能差别比较小,1 000 min裂解制备的试样的弯曲强度高达762.5 MPa,其弯曲强度和断裂韧性常数还略高于另外2种。不同升温速率下试样断口的SEM照片均显示很长的纤维拔出,增韧效果显著。研究表明,适当提高升温速率并没有降低Cf/SiC复合材料的力学性能。

奥沙利铂联合5-FU和CF术前治疗直肠癌28例疗效观察

目的观察奥沙利铂联合5-氟尿嘧啶(5-FU)、亚叶酸钙(CF)术前治疗直肠癌患者的疗效。方法直肠癌患者60例分为联合化疗组(28例)和单纯化疗组(32例)。联合化疗组治疗方案采用奥沙利铂、5-氟尿嘧啶及亚叶酸钙术前联合化疗;单纯化疗组治疗方案采用5-氟尿嘧啶、亚叶酸钙术前化疗。两组患者均接受3周期化疗,依据WHO推荐的实体瘤疗效评价标准比较两组肿瘤近期疗效;手术后标本按Wheeler的直肠癌消退分级判定比较两组直肠癌肿瘤消退情况。结果实体瘤疗效联合化疗组总有效率64%(18例),单纯化疗组总有效率19%(6例),两组比较差异有显著性(P<0.05)。直肠癌肿瘤消退联合化疗组总有效率79%(22例),单纯化疗组总有效率34%(11例),两组比较差异有显著性(P<0.05)。结论奥沙利铂联合5-FU、CF治疗直肠癌比单纯5-FU、CF术前化疗能明显缩小肿瘤体积,显著消退肿瘤细胞。

NSE、CF21-1与CEA在治疗肺癌患者中的临床价值

目的对患有肺癌的患者在治疗过程中对其血清NSE、CF21-1和CEA水平进行评价的临床价值进行探讨。方法抽取在我院就诊的患有肺癌和肺部感染的临床确诊患者病例各35例,分别将其定义为A、B组,再取同期在我院进行健康检查的患者资料35例,将其定义为C组,对三组患者的血清NSE、CF21-1和CEA水平进行测定,并对结果进行比较分析。结果分析结果表明,A组患者的NSE、CF21-1和CEA水平明显高于B、C两组,有显著的统计学差异(P<0.05);B、C两组患者NSE、CF21-1和CEA的水平没有太大差别,没有显著的统计学差异(P>0.05);A组患者的CEA水平明显高于C两组,有显著的统计学差异(P>0.05);B、C两组患者的CEA水平没有太大差别,没有显著的统计学差异(P>0.05)。结论根据患者的血清NSE、CF21-1和CEA水平高低,可以为对肺癌患者进行诊断和治疗提供可靠的依据,在对肺癌患者进行治疗的过程,对上述通过对以上三项数据进行监测,可以对患者的治疗效果进行客观的反应,值得在今后的临床治疗工作中进一步使用和推广。

CF4-1B型车载火箭发射装置装卸架研制与应用

采用槽钢、方钢管和万向轮,对江西九三九四厂生产的CF4-1B型车载火箭发射装置研制、生产了装卸架。经过反复应用证明该装卸架结构简单、合理、造价低,能使火箭发射装置轻巧、方便地在皮卡车上装卸。也可在装卸架上直接进行火箭作业。

Cf/SiC复合材料表面抗氧化涂层研究进展

Cf/SiC复合材料因其低密度,高比强度,优异的抗热震、抗氧化和抗烧蚀性能以及高温强度保持率,被认为是高速飞行器的重要热防护材料之一。然而,由于碳纤维在500℃以上发生显著氧化导致材料逐渐失效,因此需对其进行有效的氧化防护。抗氧化涂层被认为是实现Cf/SiC复合材料长时氧化防护的有效手段。本文基于热防护系统对Cf/SiC复合材料抗氧化性能的苛刻要求,综述了现有Cf/SiC复合材料表面抗氧化涂层的研究进展,着重对抗氧化涂层制备技术及涂层体系进行了梳理。提升Cf/SiC复合材料抗氧化涂层使用温度(≥1800℃)及结合强度是当前需要重点解决的问题,制备更长服役时间、更高服役温度同时兼具抗氧化、抗水蒸气腐蚀乃至较好隔热性能的多功能涂层是未来发展的重要方向。

Improved wettability and mechanical properties of metal coated carbon fiber-reinforced aluminum matrix composites by squeeze melt infiltration technique

In order to improve the wettability and bonding performance of the interface between carbon fiber and aluminum matrix,nickel-and copper-coated carbon fiber-reinforced aluminum matrix composites were fabricated by the squeeze melt infiltration technique.The interface wettability,microstructure and mechanical properties of the composites were compared and investigated.Compared with the uncoated fiber-reinforced aluminum matrix composite,the microstructure analysis indicated that the coatings significantly improved the wettability and effectively inhibited the interface reaction between carbon fiber and aluminum matrix during the process.Under the same processing condition,aluminum melt was easy to infiltrate into the copper-coated fiber bundles.Furthermore,the inhibited interface reaction was more conducive to maintain the original strength of fiber and improve the fiber−matrix interface bonding performance.The mechanical properties were evaluated by uniaxial tensile test.The yield strength,ultimate tensile strength and elastic modulus of the copper-coated carbon fiber-reinforced aluminum matrix composite were about 124 MPa,140 MPa and 82 GPa,respectively.In the case of nickel-coated carbon fiber-reinforced aluminum matrix composite,the yield strength,ultimate tensile strength and elastic modulus were about 60 MPa,70 MPa and 79 GPa,respectively.The excellent mechanical properties for copper-coated fiber-reinforced composites are attributed to better compactness of the matrix and better fiber−matrix interface bonding,which favor the load transfer ability from aluminam matrix to carbon fiber under the loading state,giving full play to the bearing role of carbon fiber.