IMR纳米复合涂层与现役飞机典型涂层抗紫外线老化性能对比研究

采用紫外线照射加速老化实验方法对喷涂IMR纳米复合涂层与现役飞机结构典型涂层的试件进行了对比实验，定量地描述了涂层色差随着老化时间的变化.与现役飞机涂层相比，纳米复合涂层的抗紫外线老化性能有明显改进.研究结果为纳米复合涂层在典型军用飞机结构中的应用提供了实验依据.      

飞机外部 IMR21 纳米复合涂层在典型加速腐蚀环境中的腐蚀失效行为

目的研究IMR纳米复合涂层对飞机外部结构件的防护性能。方法对比考察典型加速腐蚀环境条件下,飞机外部结构模拟件表面聚氨酯面漆涂层和IMR21纳米复合涂层的腐蚀失效行为。结果在经过2个阶段各8个周期的加速腐蚀后,模拟件涂层表面均出现了鼓包、开裂、剥落等现象,而且涂层在第二阶段的腐蚀程度略重于第一阶段。与聚氨酯面漆涂层相比,IMR21纳米复合涂层的腐蚀失效程度要低很多,说明该纳米复合涂层具有优良的抗环境腐蚀性能。结论可考虑在飞机结构制造、大修以及外场维护中采用IMR21纳米复合涂层进行表面防腐涂装处理。     

SEBF/SLF重腐蚀防护涂层应用于典型飞机结构中防腐性能综合评定

针对典型飞机结构的局部腐蚀环境开展了加速腐蚀环境谱及加速腐蚀试验方法研究,为了综合评定SEBF/SLF重腐蚀防护涂层涂装在典型飞机结构中的防腐性能,对该涂层与现役飞机典型涂层进行了对比试验.结果表明,与现役飞机典型涂层相比,SEBF/SLF重腐蚀防护涂层的抗环境腐蚀性有明显改进.     

铝合金用的两种有机防护涂层评价

    选用LD5、LY11、ZL402为基材,分别施涂IMR11纳米浓缩浆复合涂层(纳米涂层)和SEBF-2型改性熔融结合环氧粉末复合涂层(环氧涂层),利用拉伸试验、抗弯试验以及铜加速乙酸盐雾腐蚀试验,研究涂层在应力应变条件下和酸性盐雾条件下与基材铝合金的适配性.结果表明：纳米涂层比环氧涂层与铝合金基材有更好的适配性;适合用于工作在海洋环境中的飞机、船舶、车辆等非磨损条件下动力设备铝合金结构件的防护涂层.     

等离子喷涂常规和纳米ZrO2-7％Y2O3热障涂层隔热性能

采用等离子喷涂工艺在TiAl合金表面制备常规和纳米ZrO2-7％Y2O3(质量分数)热障涂层,分析了两种涂层的组织结构,并对其隔热性能进行了比较.结果表明,等离子喷涂常规热障涂层呈典型的层状堆积特征,而纳米涂层为特殊的两相结构.相对于常规涂层,纳米涂层有较好的隔热性能;在1100℃时,等离子喷涂常规及纳米涂层的隔热温度分别为83、127℃.     

纳米ZrO2-Y2O3-La2O3热障涂层的结构与性能研究

采用喷雾造粒工艺在纳米ZrO2-8wt％Y2O3(8YSZ)基体中添加了纳米La2O3,并进行团聚、热处理,作为喷涂喂料.NiCrAlY(Ni-25Cr-5Al-0.5Y,wt％)作为粘结层材料,采用等离子喷涂技术制备热障涂层.对涂层的组织结构和性能进行了表征与分析.结果表明:喷涂后涂层相组成只有稳定的t相;涂层具有典型的等离子喷涂结构;添加纳米LaO3能够降低涂层的热导率,且涂层的结合强度随掺杂量的增多而提高.     

纳米掺杂Al2O3＋13wt% TiO2等离子喷涂涂层的抗磨损性能

采用纳米掺杂(5%～30%)方法制备出纳米包覆微米级粒子的AT13等离子喷涂粉末,并利用大气等离子喷涂技术制备出了含有纳米复相结构的陶瓷涂层.在MM-200型磨损试验机上进行了常温干摩擦试验,比较了纳米复相结构涂层和传统陶瓷涂层的耐磨性能,利用扫描电镜观察了磨损后的磨痕形貌.结果表明,纳米复相涂层的耐磨性能明显好于传统陶瓷涂层,且随着磨损载荷的增大,纳米复相涂层和传统涂层的磨损机制的变化是不同的,传统涂层的磨损机理主要是微裂纹和颗粒的剥落,而相同条件下纳米复相涂层则由于涂层韧性的提高,主要表现为涂层的粘着磨损与局部剥落,并对纳米掺杂等离子喷涂涂层对AT13涂层磨损机制的影响进行了探讨.     

激光重熔纳米Al2O3-13%TiO2陶瓷涂层组织及性能

为了进一步提高等离子喷涂纳米Al2O3-13%TiO2(质量分数, 下同)复合陶瓷涂层的性能,在γ-TiAl基体材料表面采用激光重熔工艺对涂层进行处理,研究了激光重熔对涂层微观组织和性能的影响.用扫描电镜(SEM)和显微硬度计分析了涂层形貌、微观结构和显微硬度,同时对涂层的磨损特性进行了考察.结果表明,等离子喷涂纳米陶瓷涂层由纳米颗粒完全熔化区和部分熔化区两部分组成,仍然具有等离子喷涂态的典型层状结构.经过激光重熔后,形成了致密细小的等轴晶重熔区、烧结区和残余等离子喷涂区,由于激光快速加热和快速冷却加工特点,在重熔区仍保留了部分来源于原等离子喷涂部分熔化区的残留纳米粒子.与常规等离子喷涂陶瓷涂层相比,纳米结构涂层可在一定程度上提高其硬度和耐磨性,经过激光重熔后其硬度和耐磨性进一步提高.     

2A12与30CrMnSiA在相同海洋大气环境中的加速环境谱差异

实验室加速试验是飞机结构日历寿命评定的重要方法,编制加速环境谱则是开展加速试验的前提。现有的海军飞机加速环境谱主要有金属、涂层、复合材料三类,但是金属种类并未进一步细分。不同的金属腐蚀机理存在差异,应在试验的基础上针对飞机典型金属材料分别编制加速环境谱。以某海域海洋大气环境谱为基础,选取2A12、30CrMnSiA两种飞机常用材料为研究对象,给出了两种材料加速环境试验模块参数的确定方法及加速环境谱与服役环境的当量关系,编制了分别适合2A12、30CrMnSiA的典型海洋大气环境加速环境谱,并通过试验对环境谱的当量关系进行了验证。     

纳米WC与CeO2对陶瓷涂层组织和性能的影响

以水轮机叶片的工作条件为背景,将纳米CeO2与纳米WC添加到Fe-WC金属陶瓷喷涂材料中,采用等离子喷涂方法制备涂层.对涂层进行显微组织分析及耐磨性和结合强度等试验,探讨纳米CeO2和纳米WC对喷涂层组织、耐磨性及结合强度的影响,以便制备性能优良的喷涂层用于水轮机叶片的保护,结果表明:将适量的纳米CeO2与纳米WC粉末添加到Fe-WC涂层中,可以改善喷涂层的组织,提高喷涂层的结合强度、耐磨性.     

掺杂镍对镁合金表面冷喷涂锌基涂层性能的影响

目的研究镍添加对冷喷涂锌基涂层耐蚀性的影响,为镁合金提供有效的防护涂层。方法采用低压冷喷涂技术在镁合金基体表面分别制备锌基和锌/镍基复合涂层,通过微观观察、摩擦磨损实验、电化学极化法和电化学阻抗谱测试及全浸泡腐蚀试验,研究镁合金表面冷喷涂涂层的结构、摩擦磨损行为和耐蚀性。结果镁合金表面冷喷涂锌基涂层后,其硬度和耐磨性得到显著提高,掺镍后的锌/镍基涂层具有更高的硬度和耐磨性。锌基和锌/镍基涂层均能为镁合金提供腐蚀防护,锌/镍基涂层比锌基涂层具有更好的耐蚀性。相对镁合金来说,锌基涂层和锌/镍基涂层的自腐蚀电位分别正移了260 mV和560 mV;长期腐蚀后锌/镍基涂层形成了更致密的腐蚀产物膜,腐蚀电阻显著高于锌基涂层。结论冷喷涂锌基和锌/镍复合涂层均能对镁合金提供防护作用,掺杂镍后的锌/镍基复合涂层具有更高的硬度、耐磨性和耐蚀性。     

热喷涂Fe基非晶涂层耐腐蚀性与孔隙率研究进展

热喷涂Fe基非晶合金涂层的综合性能优异,特别是在耐磨、耐腐蚀方面具有传统晶体材料无可比拟的优势,因而广泛应用于材料表面的防护领域。然而热喷涂涂层为典型的层状结构,涂层内部会存在一定量的孔隙,致使涂层耐腐蚀性能下降。首先介绍了热喷涂Fe基非晶涂层的腐蚀机理及其影响因素,总结了热喷涂涂层孔隙产生的机制、分类和影响因素。接着重点介绍了孔隙与热喷涂Fe基非晶涂层耐腐蚀性之间关系的研究进展。最后,通过对热喷涂涂层的形成过程与孔隙形成机理进行分析,粒子铺展变形能力差是显著影响涂层形成时粒子相互嵌套叠加和变形能力的主要原因。所以,Fe基非晶涂层可以从改变喷涂粉末成分和粒度、第二项粒子加入及喷涂工艺参数优化等措施,来改善粒子铺展变形能力,提高致密度。采用激光快速表面重熔技术对涂层微表层进行快速重熔处理,同样可以达到降低涂层孔隙率、提高涂层耐腐蚀性的目的。     

Improving corrosion properties of high-velocity oxy-fuel sprayed inconel 625 by using a high-power continuous wave neodymium-doped yttrium aluminum garnet laser

Thermal spray processes are widely used to protect materials and components against wear, corrosion and oxidation. Despite the use of the latest developments of thermal spraying, such as high-velocity oxy-fuel (HVOF) and plasma spraying, these coatings may in certain service conditions show inadequate performance,e.g., due to insufficient bond strength and/or mechanical properties and corrosion resistance inferior to those of corresponding bulk materials. The main cause for a low bond strength in thermalsprayed coatings is the low process temperature, which results only in mechanical bonding. Mechanical and corrosion properties typically inferior to wrought materials are caused by the chemical and structural inhomogeneity of the thermal-sprayed coating material. To overcome the drawbacks of sprayed structures and to markedly improve the coating properties, laser remelting of sprayed coatings was studied in the present work. The coating material was nickel-based superalloy Inconel 625, which contains chromium and molybdenum as the main alloying agents. The coating was prepared by HVOF spraying onto mild steel substrates. High-power continuous wave Nd:YAG laser equipped with large beam optics was used to remelt the HVOF sprayed coating using different levels of power and scanning speed. The coatings as-sprayed and after laser remelting were characterized by optical microscopy and scanning electron microscopy (SEM). Laser remelting resulted in homogenization of the sprayed structure. This strongly improved the performance of the laser-remelted coatings in adhesion, wet corrosion, and high-temperature oxidation testing. The properties of the laser-remelted coatings were compared directly with the properties of as-sprayed HVOF coatings and with plasma-transferred arc (PTA) overlay coatings and wrought Inconel 625 alloy.     

盐雾环境下X70管线钢等离子喷涂铝涂层的腐蚀行为

目的研究X70管线钢的防腐工艺,以延长其使用寿命。方法采用等离子喷涂方法在X70管线钢基体表面制备铝涂层,通过扫描电镜(SEM)和能谱仪(EDS)对涂层表面、界面质量和微观形貌进行分析。利用盐雾腐蚀试验,对比分析涂层对基体的保护作用机制。结果涂层为富铝层,主要以富铝脆性物相存在,并受环境空气的影响,涂层出现孔洞、裂纹和未熔颗粒等缺陷。涂层表面因铝粉颗粒尺寸差异,颗粒间熔融状态不同,导致表面铝元素呈波浪式分布。涂层界面结合处,铁、铝元素相互渗透,形成Fe-Al冶金结合,增加了涂层结合强度。热处理后,未熔颗粒及部分金属氧化物熔化并填充涂层缺陷,减小了表面粗糙度和孔洞率,提高了涂层质量。盐雾腐蚀16h后,未喷涂涂层试样表面出现了严重的点蚀现象,影响了管线钢的使用寿命。喷涂铝涂层试样在盐雾腐蚀试验120h后,表面出现了轻微腐蚀现象。结论涂层表面形成了致密氧化膜,避免了腐蚀介质和基体直接接触,提高了X70管线钢的耐腐蚀性。     

Corrosion fatigue behavior of a steel with sprayed coatings

This paper describes the corrosion fatigue behavior and fracture mechanisms of a steel with different sprayed coatings. Rotating bending fatigue tests were conducted in 3% NaCl solution using specimens of a medium carbon steel with sprayed coatings of a ceramic (Cr₂O₃), a cermet (WC-12%Co) and two metals (Ni-11 % P and Al-2% Zn). The corrosion fatigue process was basically the same for ceramic, cermet, and Ni-11 % P sprayed specimens. That is, the corrosive media could be supplied from the specimen surface to the substrate through cracks initiated during fatigue cycling and/or pores in the coatings, and thus corrosion pits were generated followed by subsequent crack initiation and growth in the substrate. The corrosion fatigue strength of ceramic sprayed specimens was slightly improved compared to that of the substrate steel because the under-coating (Ni-5%A1) could impede the penetration of the corrosive media although the ceramic coating had a poor resistance to cracking under cyclic loading. Cermet sprayed specimens also exhibited improved corrosion fatigue strength because of the high resistance to cracking and the low volume fraction of pores of the coating. In Ni-11 % Psprayed specimens, cracks were initiated in the coating even at low stress levels; thus the corrosion fatigue strength was the same as that of the substrate. Anodic dissolution took place in Al-2 % Zn coating because the coating was electrochemically poor, and thus the substrate was cathodically protected. Therefore, the corrosion fatigue strength of Al-2 % Zn sprayed specimens was enhanced to as high as the fatigue strength of the substrate in room air. Based on the experimental results, a dual-layer coating consisting of WC-12%Co and Al-2%Zn was fatigue tested. The coating was effective at low stress levels and exhibited long life under conditions where corrosion fatigue strength was critical.     

Adhesion improvements of Thermal Barrier Coatings with HVOF thermally sprayed bond coats

Thermal barrier coatings (TBC) are an effective engineering solution for the improvement of in service performance of gas turbines and diesel engine components. The quality and further performance of TBC, likewise all thermally sprayed coatings or any other kind of coating, is strongly dependent on the adhesion between the coating and the substrate as well as the adhesion (or cohesion) between the metallic bond coat and the ceramic top coat layer. The debonding of the ceramic layer or of the bond coat layer will lead to the collapse of the overall thermal barrier system. Though several possible problems can occur in coating application as residual stresses, local or net defects (like pores and cracks), one could say that a satisfactory adhesion is the first and intrinsic need for a good coating. The coating adhesion is also dependent on the pair substrate-coating materials, substrate cleaning and blasting, coating application process, coating application parameters and environmental conditions. In this work, the general characteristics and adhesion properties of thermal barrier coatings (TBCs) having bond coats applied using High Velocity Oxygen Fuel (HVOF) thermal spraying and plasma sprayed ceramic top coats are studied. By using HVOF technique to apply the bond coats, high adherence and high corrosion resistance are expected. Furthermore, due to the characteristics of the spraying process, compressive stresses should be induced to the substrate. The compressive stresses are opposed to the tensile stresses that are typical of coatings applied by plasma spraying and eventually cause delamination of the coating in operational conditions. The evaluation of properties includes the studies of morphology, microstructure, microhardness and adhesive/cohesive resistance. From the obtained results it can be said that the main failure location is in the bond coat/ceramic interface corresponding to the lowest adhesion values.     

Thermal spray for commercial shipbuilding

Thermal spraying of steel with aluminum to protect it from corrosion is a technology that has been proven to work in the marine environment. The thermal spray coating system includes a paint sealer that is applied over the thermally sprayed aluminum. This extends the service life of the coating and provides color to the end product. The thermal spray system protects steel both through the principle of isolation (as in painting) and galvanizing. With this dual protection mechanism, steel is protected from corrosion even when the coating is damaged. The thermal- sprayed aluminum coating system has proved the most cost- effective corrosion protection system for the marine environment. Until recently, however, the initial cost of application has limited its use for general application. Arc spray technology has reduced the application cost of thermal spraying of aluminum to below that of painting. Commercial shipbuilders could use this technology to enhance their market position in the marine industry.     

Resistance of thermal-sprayed duplex coating composed of aluminum and 80Ni-20Cr alloy against aqueous corrosion

The development of corrosion-resistant sprayed coatings without sealing is required to increase the reliability of the thermal spray coating method and to expand the field of application for wet corrosion environments. The conventional wire flame-sprayed aluminum coating on steel without sealing has poor resistance against aqueous corrosion and has restricted practical use. A duplex coating composed of sprayed aluminum on an 80Ni-20Cr alloy undercoat exhibited sufficient resistance in a hot, near-neutral aqueous environment through a trial use in a vegetable oil process. In this paper, the mechanism of corrosion resistance of the duplex coating is investigated by electrochemical polarization measurements and electron probe microchemical analysis (EPMA) to examine the individual role of each layer and the change of the microstructure with time.     

氯离子浓度对Ni-P合金涂层失效过程影响的SECM实验和COMSOL模拟研究

目的发展具有空间分辨的腐蚀电化学研究方法。方法用电沉积方法在铜基体上制备Ni和Ni-P涂层,应用扫描电镜和XRD检测涂层表面形貌和晶体结构,采用扫描电化学显微镜(SECM)研究Ni和Ni-P涂层在不同浓度Na Cl溶液中的失效行为,并结合COMSOL多物理场软件建立二维和三维模型,模拟量化活性点大小和反馈机制。结果低浓度Cl-对于纯Ni涂层具有活化作用,增加Cl-浓度会促进腐蚀发生。Ni-P合金涂层在低浓度Na Cl溶液中,短时间内保持良好的稳定性,浸泡6 h后,低P合金涂层出现典型的活性点和腐蚀产物,而高P合金涂层在浸泡24 h后出现腐蚀产物和活性区域。0.1 mol/L的Na Cl溶液促进低P合金涂层局部腐蚀的发生,而涂层在0.3 mol/L Na Cl溶液中则以发生均匀腐蚀为主。逼近曲线及其模拟结果表明,腐蚀产物对于Fc Me OH的电化学过程完全失活,而新鲜Cu表面对Fc Me OH氧化还原过程受扩散控制。三维模拟结果显示,低P合金涂层失效过程中活性点大小接近10μm。结论 Ni和Ni-P合金涂层的失效过程中活性点的形成、腐蚀产物的生成和累积过程与SECM面扫描图谱中正负反馈效应相关,Cl-促进腐蚀发生,其浓度影响腐蚀类型。COMSOL多物理场模拟明确反馈效应与探针和基底的距离有关,Ni-P涂层失效活性点大小在微米级。