超音速微粒沉积-激光同步强化Inconel718涂层高温氧化行为

针对镍基高温合金 Inconel 718 表面损伤问题,利用超音速微粒沉积-激光同步强化技术在基体表面制备了相同成分的 Inconel 718 修复涂层。 采用场发射扫描电子显微镜( SEM) 及其自带的能谱分析仪 EDS、X-射线衍射仪 (XRD)、显微拉曼光谱仪、场发射高分辨透射电子显微镜(TEM)分析了激光功率为 1300 W 时涂层的微观组织结构和 750 ℃高温氧化后表/ 截面形貌。 结果表明:涂层表面光洁,内部组织致密,孔隙率仅为 0. 2%,涂层与基体结合良好且无明显裂纹等缺陷。 在氧化初期,镍基高温合金涂层表面快速氧化并形成富 Ni、Fe、Cr 的 NiO、Fe₂O₃ 、Cr₂O₃ 以及含 Ni 的尖晶石 Cr₂O₃·NiO 结构。随着氧化时间的延长,NiO 与 Fe₂O₃ 结合生成复合相 NiFe₂O₄ ,而覆盖在 NiO 表面的 Cr₂O₃ 不断生长扩张,与 NiO 发生固相反应生成 NiCr₂O₄ 。     

Si对625合金激光熔覆层高温氧化特性的影响

利用循环氧化法,研究了不同Si含量（0%,1%,3%,质量分数）的625合金熔覆层在700、800、900 ℃下氧化144 h后的高温氧化行为。用XRD分析了氧化物相。通过SEM/EDS研究了氧化物表面和截面的形貌、元素组成和氧化膜的厚度。结果表明,不同温度下试样的氧化动力学都保持抛物线规律,随着温度的升高,氧化增重逐渐增加。通过观察,在900 ℃时,0% Si含量的625合金熔覆层出现了氧化膜大面积剥落的情况,3% Si含量的合金熔覆层氧化膜保持完整。在700 ℃时,随着Si含量增加,氧化膜表面的氧化颗粒尺寸减小且更加致密,同时促进了Cr₂O₃氧化物的生成。在700 ℃下,0 % Si含量的试样出现了大片的内氧化区域;1% Si含量的试样基体部分出现了2处条状的含Ni,Cr,Mo的氧化物相区;而3% Si含量的试样氧化后由于生成了富Si的内氧化层,这阻止了内氧化的发生。外层Cr₂O₃氧化膜和内层SiO₂的联合作用既阻止了O阴离子的渗入也抑制了Fe等金属离子的扩散,提高了合金熔覆层的抗氧化性。     

CoCrNiAlY涂层制备工艺对组织形态及高温氧化行为的影响

为了研究CoCrNiAlY涂层微观组织结构对高温氧化行为和剥落行为的影响规律,采用激光熔覆技术和等离子喷涂工艺在718高温合金表面制备CoCrNiAlY涂层,观察其微观组织形态。利用XRD和SEM对1150 ℃高温氧化试验样品进行氧化层物相分析和形貌观察。结果表明,激光熔覆制备的CoCrNiAlY涂层中形成了胞状亚结构的等轴晶凝固组织,相对于等离子喷涂制备的CoCrNiAlY涂层结构更致密,具有更优异的抗高温氧化性能。在高温氧化过程中,等离子喷涂CoCrNiAlY涂层生成了以Cr₂O₃结构为主的复合氧化膜。激光熔覆CoCrNiAlY涂层生成Al₂O₃结构的单一氧化膜,而且熔覆层中原位形成的Y₂O₃钉扎作用能有效提高氧化膜的抗剥落性。文中系统分析讨论了两种不同工艺制备的组织形态对高温氧化膜形成机制的影响,激光熔覆涂层在高温下主要是以界面扩散方式形成致密的Al₂O₃膜,等离子喷涂涂层在高温下以界面反应的方式快速形成Cr₂O₃复合氧化膜。     

介质对GH3625合金高温腐蚀中氧化膜的影响机制

本文采用XRD、SEM、EDS、增重法测量和热力学计算等手段研究了铸态GH3625合金在900 ℃下不同腐蚀介质中(Air、75 wt.% Na₂SO₄+25 wt.% NaCl和2% SO₂+H₂O+Air)腐蚀120 h后的高温腐蚀行为,探讨了不同腐蚀介质下氧化膜的形成及破坏机制。研究表明,GH3625合金在不同介质中腐蚀后,从合金最表层到合金内部结构均分为疏松氧化层、致密氧化层、贫Cr区和合金基体,其氧化层主要由NiO、Cr₂O₃和NiCr₂O₄组成。同时,合金在熔盐和高温酸性气氛中腐蚀后的贫Cr区深度(约14 μm和11μm)均大于在空气中氧化后贫Cr区深度(约8 μm),腐蚀介质对合金表层氧化膜的破坏程度从大到小依次为熔盐介质、高温酸性气氛介质、空气介质。合金的腐蚀主要是不同介质下合金表层氧化膜的形成与溶解的相互竞争,当GH3625合金在熔盐介质中腐蚀时,腐蚀机制主要是氧化膜与Cl^_-反应生成气相Cl₂和与Na₂O反应生成铬酸盐Na₂CrO₄;而当GH3625合金在酸性气氛介质中腐蚀时,腐蚀机制主要是Cr、Ni元素与SO₂、O₂的连续硫化和氧化反应。     

激光熔覆纳米 Al2O3颗粒增强 Ni 基合金涂层界面组织和高温热腐蚀性能

目的 研究纳米颗粒对 Ni 基合金涂层抗热腐蚀性能的影响。 方法 采用压片预置式激光熔覆工艺,制备了纳米 Al₂O₃ 颗粒增强的 NiCoCrAlY 合金涂层,对熔覆层界面区组织及裂纹进行了显微分析,进行了 1000 益 高温熔盐热腐蚀性能试验。 结果 加入纳米 Al₂O₃ 颗粒的激光熔覆涂层界面区未出现明显缺陷,其热腐蚀失重速率远远低于未加纳米颗粒的涂层,腐蚀表面未出现严重的隆起和剥落,腐蚀层深度小。 结论 添加适量纳米 Al₂O₃ 颗粒对 NiCoCrAlY 合金激光熔覆层界面区裂纹的形成有一定的抑制作用,可使熔覆层的抗高温热腐蚀性能明显提高。     

磁控溅射Cr/CrN和Cr/CrN/CrAlN涂层的抗高温氧化性能

为了提高航空紧固件涂层的高温工况防护能力,采用磁控溅射技术在钛合金表面分别制备 Cr/ CrN 交替涂层和 Cr/ CrN / CrAlN 涂层,研究氧化时间和氧化温度对涂层高温氧化性能影响。 利用 SEM、EDS 和 XRD 进行微观形貌和物相成分分析,采用热重法分析氧化增重量( w) 和氧化速率常数( k) ,使用显微硬度计测试涂层高温氧化后硬度。 结果表明:随着氧化时间和氧化温度的增加,涂层硬度均降低,但 Cr/ CrN / CrAlN 涂层下降趋势更缓; 两种涂层的 w 和 k 均上升,其中 Cr/ CrN / CrAlN 涂层 w 和 k 增幅均低于 Cr/ CrN 交替涂层,950 ℃ 氧化 96 h 后 Cr/ CrN / CrAlN 涂层和 Cr/ CrN 交替涂层的 w 值分别为 40 mg / cm ² 和 135. 7 mg / cm ² ,其对应的 k 分别为 0. 1996 和 0. 4092,说明 Cr/ CrN / CrAlN 涂层抗高温氧化性更好。 Cr/ CrN / CrAlN 涂层活化能 E_a 值比 Cr/ CrN 交替涂层高 48. 5%,Cr/ CrN / CrAlN 涂层在高温下产生 Cr₂O₃ 和 Al ₂O₃ 的混合氧化物,结构更致密,Cr/ CrN / CrAlN 涂层抗高温氧化性能高于 Cr/ CrN 交替涂层。     

成分设计优化TiC/Hastelloy复合材料的抗氧化性能

TiC/Hastelloy复合材料是极具应用前景的中温固体氧化物燃料电池连接体材料,而抗氧化性能是影响其应用的关键性能之一。通过无压反应渗透工艺分别制备出含有50vol%和58vol%金属基体的TiC/Hastelloy复合材料。高金属含量使复合材料中的Cr含量增加,促进连续Cr₂O₃氧化层的形成,抑制Ni和Ti原子的外扩散,进而优化复合材料的抗氧化性能。氧化膜中Ti和Ni的氧化物含量降低,复合材料的氧化增重由2.03 mg·cm^-2降低到0.55 mg·cm^-2。同时,为了抑制Cr挥发,在含有58vol%金属基体的TiC/Hastelloy复合材料中引入Co。在氧化过程中,Co和金属基体中的Fe在Cr₂O₃氧化层中具有较快的扩散速率,可以在Cr₂O₃氧化层外侧原位形成CoFe₂O₄层。     

包埋法制备NiAl涂层NiCrW基高温合金的抗氧化性能

以CaCl₂为活化剂,采用包埋法在NiCrW基高温合金表面制备了NiAl涂层。采用X射线衍射、扫描电子显微镜和能谱仪对涂层表面和横截面进行了分析。结果表明,CaCl₂可以替代NH₄Cl,是一种有效的活化剂。在950 ℃下,通过4 h的包埋渗铝,制备出几乎为单相、厚度为30 μm的NiAl涂层,涂层与基体之间为富铬中间层。当包埋渗剂填充率小于100%时,NiAl层表面生成针状θ-Al₂O₃。在1000 ℃恒温空气氧化试验中,NiAl涂层开始时被高速氧化,然后逐渐变为缓慢氧化,完成了亚稳态针状θ-Al₂O₃向稳态不规则颗粒状α-Al₂O₃的转变,最终稳定的α-Al₂O₃为基体提供了良好的抗氧化保护。     

γ-TiAl合金表面Al2O3/Al复合涂层的抗高温熔盐腐蚀性能研究

采用磁控溅射技术于γ-TiAl合金表面制备Al₂O₃/Al复合涂层。在850 °C下、 100 wt.% Na₂SO₄熔盐中观测Al₂O₃/Al复合涂层的高温腐蚀行为。结果表明,Al₂O₃/Al复合涂层具备由Al₂O₃表层、富Al中间层以及互扩散层组成的梯度结构,因而有效地提高了基体γ-TiAl合金的抗高温腐蚀性能。在腐蚀实验后,涂层试样表面相结构为Al₂O₃,TiO₂和TiAl₃。致密的Al₂O₃/Al复合涂层有效地抑制了O_2-,S_-和Na₊对基体γ-TiAl合金的侵蚀。并且,Al₂O₃/Al复合涂层的梯度结构亦使其表现出了优异的抗开裂和抗剥落性能。     

Ti-6Al-4V合金表面NiCrAlY/Al复合涂层的抗高温腐蚀性能

采用多弧离子镀技术在Ti-6Al-4V合金基底表面依次沉积Al层和NiCrAlY涂层,对比研究Ti-6Al-4V合金和NiCrAlY/Al复合涂层在高温腐蚀 (500 ℃, 30 h) 过程中微观组织结构变化及其抗高温腐蚀性能。经测定,NiCrAlY/Al复合涂层中Al层的厚度约为270 nm,NiCrAlY涂层的厚度约为3.8 μm。高温腐蚀测试结果显示,Ti-6Al-4V合金表面出现点蚀,腐蚀区域出现大量裂纹,表明合金发生严重的高温腐蚀。表面沉积NiCrAlY/Al复合涂层的Ti-6Al-4V合金经高温腐蚀后表面依然完整,未产生明显裂纹和涂层脱落。经分析,NiCrAlY/Al复合涂层在高温腐蚀过程中表面可自形成厚度约为43 nm的Al₂O₃和Cr₂O₃,连续且致密的薄氧化膜可在高温下阻隔氧气向钛合金内部的侵蚀,从而显著提高基底合金的抗高温腐蚀性能。     

Si对Ni-Cr-Mo合金熔覆层高温耐腐蚀性能的影响

为研究Si含量对Ni-Cr-Mo系合金熔覆层耐高温腐蚀性能的影响，利用激光熔覆技术制备了4种不同Si含量的熔覆层。采用失重法测试了4种熔覆层在模拟垃圾发电腐蚀环境中多种温度下的耐腐蚀性能。通过对4种熔覆层在600及650℃下腐蚀产物的特性分析，发现Si的加入有助于腐蚀产物中富Cr氧化皮的稳定性。还可以通过“钉扎”作用提升富Cr氧化皮与基体的粘结性，从而有效提高熔覆层的耐腐蚀性能。但Si含量并非越多越好。当温度提升到600℃以上，含3%(质量分数，下同)Si的合金展现了最佳的耐腐蚀性能。这是由于含3%Si的合金腐蚀层中形成了一层保护性的SiO₂，有助于耐腐蚀性能的提升。而含1%Si的合金由于Si含量较低，含5%Si的合金由于Si的偏析严重，均未能形成有效的SiO₂保护层。     

Effect of Mo on corrosion behavior of Ni20Cr–xMo alloys in air with NaCl–KCl–CaCl2 vapor at 570°C

The effect of Mo on the corrosion behavior of Ni20Cr–xMo alloys in an oxidizing chlorine-containing atmosphere using air mixed with the salt-vapor mixture of NaCl–KCl–CaCl₂ at 570°C was investigated. The results revealed that the corrosion performance of the Ni20Cr alloys in the oxidizing chlorine atmosphere was improved by Mo addition of up to 3 wt%. The Mo-free alloy formed a potassium chromate during corrosion as a result of the reaction between the Cr₂O₃ scale and KCl vapor. The chromate formation increased the chlorine potential at the scale surface and induced the breakdown of the protective Cr₂O₃ scale, resulting in internal chromium chloride precipitates and a Cr-depleted zone. In contrast, the presence of Mo resulted in the formation of a NiO scale, which did not react with the salt vapors and, therefore, prevented the formation of chromates. The beneficial effect of Mo on the high-temperature chlorination of Ni–Cr alloys in salt-vapor-containing atmospheres was ascribed to the suppression of chlorine generation due to NiO scale formation.     

Roles of Nb on the oxidation characteristics and oxide scale evolution of Fe-25Cr-35Ni-2.5Al-XNb alloys at 1000°C and 1100°C

The oxidation characteristics of Fe-25Cr-35Ni-2.5Al-_XNb (0, 0.6, and 1.2 wt%) alumina-forming austenitic alloys at 1000°C and 1100°C in air were investigated. Results show that Nb has an important effect on the high-temperature oxidation resistance. A bilayer oxide scale with a Cr₂O₃-rich outer layer and Al₂O₃-rich internal layer forms on the surface of the Nb-free alloy and exhibits a poor oxidation resistance at 1000°C and 1100°C. With Nb addition, both the 0.6Nb-addition and 1.2Nb-addition alloys exhibit better oxidation resistance at 1000°C. Because of the third element effect, Nb addition reduces the critical Al content and forms a single external protective Al₂O₃ scale, which greatly improves the oxidation resistance. After oxidation at 1100°C, niobium oxides (mainly Nb₂O₅) are formed on the surface of the 1.2Nb-addition alloy and destroy the integrity of the Al₂O₃ scale, which causes the formation of Cr-rich oxide nodules and eventually develops to be a loose bilayer oxide scale with NiCr₂O₄, Cr₂O₃, and Fe₂O₃ outer layers and Al₂O₃ inner layer.     

Cyclic Corrosion Behavior of Ni-Based Superalloys in Hot Lithium Molten Salt

In this study, the cyclic corrosion behavior of N06230, N07263, and N06625 in a LiCl–Li₂O molten salt was investigated at 650?°C in argon atmosphere. The cyclic corrosion behavior was observed through measurements of the oxide morphology and thickness, the extent of internal corrosion, and compositional changes in the oxide scale and the substrate. The corrosion products in the surface corrosion layers of N07263 were (Ni,Co)O, (Ni,Co)Cr₂O₄, Cr₂O₃, and TiO₂ and those in the surface corrosion layers of N06230 were NiO, NiCr₂O₄, and Cr₂O₃, while NiO, NiCr₂O₄, CrNbO₄, and Cr₂O₃ were identified as the corrosion products of N06625. The internal corrosion behavior of N07263 was localized, while N06230 and N06625 showed uniform corrosion. N07263 exhibited superior corrosion resistance as its corrosion layer was more continuous, dense, and adherent as compared to those of N06230 and N06625.     

Microstructure and corrosion resistance of Cr/Cr2N multilayer film deposited on the surface of depleted uranium

Depleted uranium is widely used in national defence and nuclear energy fields. However, the inferior corrosion resistance limits its application. A Cr/Cr₂N film was prepared by magnetron sputtering on the uranium to improve its corrosion resistance. The Cr/Cr₂N film exhibits modulation structure. The introduction of the Cr/Cr₂N increases the corrosion potential; the corresponding current density decreases about three orders of magnitude. After polarization corrosion, the surface morphology of the Cr/Cr₂N-coated on uranium keeps integrated. Only a thin layer of film (∼40 nm) is oxidized. The Cr/Cr₂N film shows great potential in improving oxidation and corrosion resistance of depleted uranium.     

Corrosion properties of materials coated with Cr2O3/NiCr and with Cr2O3+NiCr functionally gradient materials

This paper studied the corrosion properties of five kinds of Cr₂O₃ coated materials: the SUS316L austenitic stainless steels respectively coated with the Cr₂O₃ layer (Cr₂O₃/316), Cr₂O₃ and 80Ni‐ 20Cr layers (Cr₂O₃/80NiCr/316), Cr₂O₃ and 50Ni‐ 50Cr layers (Cr₂O₃/50NiCr/316), Cr₂O₃ + 80Ni‐ 20Cr functionally gradient materials (Cr₂O₃ + 80NiCr FGM), and Cr₂O₃ + 50Ni‐ 50Cr FGM (Cr₂O₃ + 50NiCr FGM). All the coatings were made by atmospheric pressure plasma spraying method (APPS). The corrosion resistance of the coated materials was analyzed by immersion tests and electrochemical evaluations. A mechanism of the corrosion failures for these kinds of coated structures was proposed. The different coating structures for improving the adhesion between ceramics and substrates were assessed, and the effect of Cr content in the NiCr coatings on the corrosion property was discussed. The ceramic coatings with the 50Ni‐ 50Cr intermediate layer possessed a better corrosion resistance than that with 80Ni‐ 20Cr. The FGM structures appeared to offer weaker resistance to corrosion attack than that with the intermediate layer in general. Under corrosion test conditions, the corrosion‐proof abilities of the coated structures were, respectively: the Cr₂O₃/50NiCr/316 in the best rank; the Cr₂O₃/316, Cr₂O₃/80NiCr/316, and Cr₂O₃ + 50NiCr FGM in the second rank; and the Cr₂O₃ + 80NiCr FGM in the last rank. This means that applying the 50NiCr intermediate layer under the Cr₂O₃ ceramic coating can further improve the corrosion resistance of Cr₂O₃/316. Porosity analysis was used to explain the difference of corrosion resistance between the Cr₂O₃/50NiCr coated material and the Cr₂O₃ + 50NiCr FGM. The porosity in each layer of the Cr₂O₃ + 50NiCr FGM was higher than that in the Cr₂O₃/50NiCr coating, and as a result the corrosion resistance of Cr₂O₃/50Ni Cr/316 is better than Cr₂O₃ + 50NiCr FGM.     

Y2O3 对DZ125合金表面Cr-Al-Y渗层的组织结构及抗氧化性能影响

为进一步提高DZ125合金高温服役性能,通过扩散渗方法在其表面制备了稀土元素Y改性的Cr-Al共渗层,研究了Y₂O₃含量对渗层组织结构及抗高温氧化性能的影响。结果表明：不同条件下制备的Cr-Al-Y渗层均具有三层结构,由外向内依次为：Cr+Ni₃Cr₂外层,Ni₃Cr₂+Al₁₃Co₄中间层,以及Ni₃Al内层。当渗剂中Y₂O₃含量为0%～2%(质量分数,下同)时,渗层的厚度与密度显著增加;当稀土Y₂O₃的添加量过高时(5%),渗层的密度及厚度反而下降。1100℃高温氧化实验表明,Cr-Al-Y渗层显著提高了DZ125合金的抗高温氧化性能。     

High-temperature corrosion behaviors of typical nickel alloy coatings in a simulated boiler coal ash/gas environment in the Zhundong region

The high-temperature corrosion behaviors of five nickel alloy coatings used in coal-fired boilers in the Zhundong region (Xinjiang province) were investigated in simulated coal ash and coal-combusted flue gas environment at 650°C for 250 and 500 hr. The samples were analyzed by weight gain experiment, X-ray diffraction test, and scanning electron microscopy technique with energy-dispersive spectroscopy. The results indicated that the corrosion level is in the order of NiCrMo13 ≈ Hastelloy C-276 (276) > NiCrBSi > Inconel 718 (718) > 45CT. The compositions of the corrosion scale in five nickel alloy coatings mainly consist of NiO, Ni₃S₂, and Cr₂O₃. The enrichment of Cr in the corrosion scale in 45CT, 718, and NiCrBSi coatings inhibits the formation of oxide and sulfide on the coating surface. The presence of W and Mo in nickel alloy coatings accelerates the formation of corrosion products, thus weakening the corrosion resistance of NiCrMo13 and 276 in simulated coal ash and coal-combusted flue gas environment.     

Kinetics and Microstructural Investigation of High-Temperature Oxidation of IN-738LC Super Alloy

The present study was carried out to investigate the kinetics and the surface chemistry of the oxide layers formed on the IN-738LC super alloy during high-temperature oxidation at 950 °C in air from 1 to 260 h. Oxidation kinetics were studied by mass gain measurement. The oxide layers were characterized by field emission scanning electron microscope, elemental distribution map, energy-dispersive spectroscopy as well as x-ray diffractometry (XRD). The oxidation kinetics followed the parabolic law. The XRD analysis revealed that the oxide scale contained mainly NiO, Ni (Cr, Al)₂O₄, Al₂O₃, TiO₂ and Cr₂O₃. The oxide structure, from the top surface down to the substrate, was clarified by elemental map distribution studies as Ni-Ti oxides, Cr-Ti oxides, Cr₂O₃ oxide band, Ni-Co-Cr-W oxide and finally a blocky Al₂O₃ region. The oxidation scales were composed of three distinct layers of the outer and mid layers enriched by TiO₂ and Cr₂O₃, NiCr₂O₄ oxide, respectively, and the innermost layer was composed of Al₂O₃ and matrix alloy. The depleted gamma prime layer was formed under the oxidation scales due to the impoverishment of Al and Ti which were induced by the formation of Al₂O₃ and TiO₂.