High-temperature oxidation behavior of CeO_2-SiO_2/Ni-W-P composites

Ni-W-P matrix composites containing CeO2 and SiO2 nano-particles were prepared on common carbon steel surface by means of pulse electrodeposition,and the high-temperature oxidation behavior was investigated.The results show that when the oxidation time is controlled in 1 h,oxidation kinetics curve between oxidation mass gain rate and oxidation temperature of CeO2-SiO2/Ni-W-P composites accords with the index increasing law.When the oxidation temperature is controlled at 300℃,the kinetics curve between oxidation mass gain rate and oxidation time accords with the linear increasing law.The composites as-deposited are in the amorphous state and turn into the crystal state at 400℃.The microstructures of oxidation film on the composites will change from the compact state to the loose state with increasing oxidation temperature to 800℃.They are still continuous and compact,and there are no crackle,strip and falling-out.CeO2 and SiO2 nano-particles co-deposited into Ni-W-P alloy can improve the high-temperature oxidation resistance.

High-temperature oxidation behavior of a cast Ti-47.5Al-2.5V-1.0Cr-0.2Zr alloy

The oxidation behavior of the Ti-47.5Al-2.5V-1.0Cr-0.2Zr alloy at 900℃ was investigated at different oxidation times(5,20,60 and 100 h).The results show that the total weight gain of the alloy after 100 h at 900℃ oxidation is 9.1 g·m^(-2),and the oxidation rate decreases with oxidation time.The oxides on the alloy surface are mainly TiO_(2) and Al_(2)O_(3).At the beginning of oxidation(5 h),the oxide film is relatively complete,thin,and the interface between the oxide layer and the matrix is virtually flat.At the end of oxidation(100 h),the thickness of the oxide film is expanded,cracking and spalling occur,and the spalling form is intra-film spalling.At the same time,oxygen is mainly distributed in the oxide film and the oxygen content in the alloy substrate is reduced,confirming that the TiAl alloy has a certain oxidation stability at 900℃.From the outer surface of the oxide layer to the matrix,the TiO_(2) content increases and the Al_(2)O_(3) content decreases.Oxidation proceeds to completion in this system via the dissolution and diffusion of O atom.

Interfacial Behavior of Sulfur and Yttrium in Yttrium Modified Ni _3Al Based Alloy IC6 during High Temperature Oxidation Process

The interfacial behavior of sulfur and yttrium in the yttrium modified Ni 3Al based alloy IC6 during oxidation at 1100 ℃ was analyzed by X ray line scan of electron probe microstructural analysis(EPMA). The results show that the migration and segregation of sulfur to the interface between oxide scale and the substrate at high temperature is retarded owing to the presence of yttrium. This is attributed to the desulfurization by yttrium in the melt and the trapping of sulfur by yttrium rich phases during oxidation, which leads to improving the coherence between oxide scale and substrate. Another reason of increasing the high temperature oxidation resistance of alloy IC6 by the addition of yttrium is that yttrium migrates to the grain boundaries of oxides during oxidation and hence improve their strength. This results in the transformation of the oxide scale spallation cracks from intergranular cracks for alloy without yttrium to transgranular ones for yttrium modified alloy.

Microstructure and Oxidation Behavior of ZrB_(2)-SiC Ceramics Fabricated by Tape Casting and Reactive Melt Infiltration

ZrB_(2)-based ceramics typically necessitate high temperature and pressure for sintering,whereas ZrB_(2)-SiC ceramics can be fabricated at 1500℃using the process of reactive melt infiltration with Si.In comparison to the conventional preparation method,reactive synthesis allows for the more facile production of ultra-high temperature ceramics with fine particle size and homogeneous composition.In this work,ZrSi_(2),B4C,and C were used as raw materials to prepare ZrB_(2)-SiC via combination of tape casting and reactive melt infiltration herein referred to as ZBC ceramics.Control sample of ZrB_(2)-SiC was also prepared using ZrB_(2) and SiC as raw materials through an identical process designated as ZS ceramics.Microscopic analysis of both ceramic groups revealed smaller and more uniformly distributed particles of the ZrB_(2) phase in ZBC ceramics compared to the larger particles in ZS ceramics.Both sets of ceramics underwent cyclic oxidation testing in the air at 1600℃for a cumulative duration of 5 cycles,each cycle lasting 2 h.Analysis of the oxidation behavior showed that both ZBC ceramics and ZS ceramics developed a glassy SiO_(2)-ZrO_(2) oxide layer on their surfaces during the oxidation.This layer severed as a barrier against oxygen.In ZBC ceramics,ZrO_(2) is finely distributed in SiO_(2),whereas in ZS ceramics,larger ZrO_(2) particles coexist with glassy SiO_(2).The surface oxide layer of ZBC ceramics maintains a dense structure because the well-dispersed ZrO_(2) increases the viscosity of glassy SiO_(2),preventing its crystallization during the cooling.Conversely,some SiO_(2) in the oxide layer of ZS ceramics may crystallize and form a eutectic with ZrO_(2),leading to the formation of ZrSiO_(4).This leads to cracking of the oxide layer due to differences in thermal expansion coefficients,weakening its barrier effect.An analysis of the oxidation resistance shows that ZBC ceramics exhibit less increase in oxide layer thickness and mass compared to ZS ceramics,suggesting superior oxidation resistance of ZBC ceramics.

Effect of temperature on leaching behavior of copper minerals with different occurrence states in complex copper oxide ores

The effect of temperature on leaching behavior of copper minerals with different occurrence states in complex copper oxide ores was carried out by phase analysis means of XRD, optical microscopy and SEM-EDS. The results indicated that at ambient temperature, the easily leached copper oxide minerals were completely dissolved, while the bonded copper minerals were insoluble. At lukewarm temperature of 40℃, it was mainly the dissolution of copper in isomorphism state. With increasing temperature to 60℃, the copper leaching rate in the adsorbed state was significantly accelerated. In addition, when the temperature increased to 80℃, the isomorphic copper was completely leached, leaving 11.2% adsorbed copper un-leached. However, the copper in feldspar-quartz-copper-iron colloid state was not dissolved throughout the leaching process. Overall, the leaching rates of copper in different copper minerals decreased in the order: malachite, pseudo-malachite > chrysocolla > copper-bearing chlorite > copper-bearing muscovite > copper-bearing biotite > copper-bearing limonite > feldspar-quartz-copper-iron colloid.

Exploring the Low-Temperature Oxidation Chemistry of Cyclohexane in a Jet-Stirred Reactor:an Experimental and Kinetic Modeling Study

We report the investigation on the low-temperature oxidation of cyclohexane in a jet-stirred reactor over 500-742 K. Synchrotron vacuum ultraviolet photoionization mass spectrometry （SVUV-PIMS） was used for identifying and quantifying the oxidation species. Major products, cyclic olefins, and oxygenated products including reactive hydroperoxides and high oxygen compounds were detected. Compared with n-alkanes, a narrow low-temperature window （-80 K） was observed in the low-temperature oxidation of cyclohexane. Besides, a kinetic model for cyclohexane oxidation was developed based on the CNRS model [Combust. Flame 160, 2319 （2013）], which can better capture the experimental results than previous models. Based on the modeling analysis, the 1,5-H shift dominates the crucial isomerization steps of the first and second O2 addition products in the low-temperature chain branching process of cyclohexane. The negative temperature coefficient behavior of cyclohexane oxidation results from the reduced chain branching due to the competition from chain inhibition and propagation reactions, i.e. the reaction between cyclohexyl radical and O2 and the de- composition of cyclohexylperoxy radical, both producing cyclohexene and HO2 radical, as well as the decomposition of cyclohexylhydroperoxy radical producing hex-5-en-l-al and OH radical.

Microwave absorbing characteristics and temperature increasing behavior of basic cobalt carbonate in microwave field

The microwave absorbing characteristics of basic cobalt carbonate,cobalt oxide(Co3O4),and the mixture of basic cobalt carbonate and cobalt oxide were investigated by means of microwave cavity perturbation,their temperature increasing curves were measured,and their ability to absorb microwave energy was also assessed based on the temperature increasing behavior of the material exposed to microwave field.Analyses of spectrum attenuation and relative frequency shift show that basic cobalt carbonate has weak capability to absorb microwave energy,while cobalt oxide has very strong capability to absorb microwave energy.It is feasible to thermally decompose basic cobalt carbonate though addition of small amount of cobalt oxide in microwave fields.The capability to absorb microwave energy of sample increases with an increase in mixing ratio of Co3O4.

Effect of doping aluminum and yttrium on high-temperature oxidation behavior of Ni-11Fe-10Cu alloy

Aiming to develop materials for construction of the set-up and electrode of high-temperature molten salt reactors, the effect of Al and Y on the high-temperature oxidation behavior of Ni-11Fe-10Cu at 750 and 950 °C in air were investigated. The oxidation kinetics of Ni-11Fe-10Cu alloy followed parabolic law at 750 °C without spallation and linear law at 950 °C with severe spallation, while that of Ni-11Fe-10Cu-6Al-3Y alloy followed parabolic law at 750 and 950 °C without spallation. The parabolic rate constant （kp） of Ni-11Fe-10Cu was smaller than that of Ni-11Fe-10Cu-6Al-3Y at 750 °C. The oxide scale formed on Ni-11Fe-10Cu at 750 °C was composed of a CuO outer layer, a NiFe2O4 middle layer and a NiO inner layer. The oxide scale formed on Ni-11Fe-10Cu-6Al-3Y at 750 °C was also composed of the similar triplex layers in addition to an internal oxidation zone containing Al, Ni and Cu oxide and the microstructure of the scale changed with increasing temperature. Although the doping Al and Y could improve the adherence of oxide scale, it could aggravate the extent of internal oxidation. Based on the combination of X-ray diffraction （XRD）, scanning electron mi-croscopy/energy dispersive spectroscopy （SEM/EDX） analysis, the microstructure and growth mechanism of the multi-layer oxide scale was studied and the effect of doping Al and Y on the oxidation behavior of Ni-11Fe-10Cu alloy was also discussed.

Improvement in oxidation resistance of Cantor alloy through microstructure tailoring

A method of improving the oxidation resistance of Cantor alloy through microstructure tailoring was revealed.Samples with distinctive microstructures were achieved by different annealing treatments on the cold-rolled Cantor alloy.Oxidation test was then carried out on the various annealed samples at 800°C for 24 h in air.The oxidation behavior was evaluated in terms of oxidation rate,surface and cross-section microstructure characterization.Although stratified oxide layers including outer Mn_(2)O_(3) and inner Cr_(2)O_(3) were observed in all the annealed samples,the thickness of Mn_(2)O_(3) and Cr_(2)O_(3) layers was different.Also,the samples exhibited different oxidation rates.The results indicate that the oxidation resistance of various annealed samples is closely related with grain size as well as twin density.

Insight into the effect of Ti substitutions on the static oxidation behavior of (Hf,Ti)C at 2500℃

Hf-based carbides are highly desirable candidate materials for oxidizing environments above 2000℃.However,the static oxidation behavior at their potential service temperatures remains unclear.To fill this gap,the static oxidation behavior of(Hf,Ti)C and the effect of Ti substitutions were investigated in air at 2500℃ under an oxygen partial pressure of 4.2 kPa.After oxidation for 2000 s,the thickness of the oxide layer on the surface of(Hf,Ti)C bulk ceramic is reduced by 62.29%compared with that on the HfC monocarbide surface.The dramatic improvement in oxidation resistance is attributed to the unique oxide layer structure consisting of various crystalline oxycarbides,HfO_(2),and carbon.The Ti-rich oxycarbide((Ti,Hf)C_(x)O_(y))dispersed within HfO_(2) formed the major structure of the oxide layer.A coherent boundary with lattice distortion existed at the HfO2/(Ti,Hf)C_(x)O_(y) interface along the(111)crystal plane direction,which served as an effective oxygen diffusion barrier.The Hfrich oxycarbide((Hf,Ti)CxOy)together with(Ti,Hf)C_(x)O_(y),HfO_(2),and precipitated carbon constituted a dense transition layer,ensuring favorable bonding between the oxide layer and the matrix.The Ti content affects the oxidation resistance of(Hf,Ti)C by determining the oxide layer's phase distribution and integrity.

High temperature mechanical retention characteristics and oxidation behaviors of the MoSi2（Cr5Si3）–RSiC composites prepared via a PIP-AAMI combined process

In the present paper,MoSi2(Cr5Si3)–RSiC composites were prepared via a combination of precursor impregnation pyrolysis(PIP) and MoSi2-Si-Cr alloy active melt infiltration(AAMI) process. Composition, microstructure, mechanical retention characteristics, and oxidation behaviors of the composites at elevated temperature were studied. X-ray diffraction(XRD) pattern confirms that the composites mainly compose of 6 H–SiC, hexagonal MoSi2, and tetragonal Cr5Si3. Scanning electron microscopy(SEM) image reveals that nearly denseMoSi2(Cr5Si3)–RSiC composites exhibiting three-dimensionally(3D) interpenetrated network structure are obtained when infiltrated at 2173 K, and the interface combination of the composites mainly depends on the composition ratio of infiltrated phases. Oxidation weight gain rate of the composites is much lower than that of RSiC matrix, where MoSiCr2 possesses the lowest value of 0.1630 mg×cm-2, about 78% lower than that of RSiC after oxidation at 1773 K for 100 h. Also, it possesses the highest mechanical values of 139.54 MPa(flexural strength σf and RT) and 276.77 GPa(elastic modulus Ef and RT), improvement of 73.73% and 29.77% as compared with that of RSiC, respectively. Mechanical properties of the composites increase first and then decrease with the extension of oxidation time at 1773 K, due to the cooperation effect of surface defect reduction via oxidation reaction and thermal stress relaxation in the composites, crystal growth, and thickness increase of the oxide film. Fracture toughness of MoSiCr2 reaches 2.24 MPa·m1/2(1673 K), showing the highest improvement of 31.70% as compared to the RT value.

Simultaneously improving mechanical properties and oxidation resistance of Ti-bearing high-entropy superalloys at intermediate temperature via silicon addition

Ti-bearing high-entropy superalloys(HESAs)often suffer from severe intergranular embrittlement and terrible oxidation degradation at intermediate temperatures.Here we showcase that minor Si addition can effectively mitigate the intergranular embrittlement and improve the oxidation resistance of the a(Ni_(2)Co_(2)FeCr)_(92) Ti_(4)Al_(4) HESA at 700℃ simultaneously.Experimental analysis revealed that the intergranu-lar G phase induced by 2 at%Si addition can effectively suppress the inward diffusion of oxygen along grain boundaries at 700℃,thus enhancing the tensile ductility of the alloy from∼8.3%to∼13.4%.Be-sides,the 2 at%Si addition facilitated the formation of a continuous Al_(2)O_(3) layer during oxidation,con-tributing to a remarkable reduction in the growth rate of the oxide scale to a quarter of the Si-free HESA.Our results demonstrate that Si can be a favorable alloying element to design advanced HESAs with syn-ergistically improved thermal-mechanical performance.

Design and preparation of an ultra-high temperature ceramic by in-situ introduction of Zr_(2)[Al(Si)]_(4)C_(5) into ZrB_(2)-SiC:Investigation on the mechanical properties and oxidation behavior

Novel ZrB_(2)-matrix composites were designed and prepared by in-situ introducing SiC and Zr_(2)[Al(Si)]_(4)C_(5) simultaneously for the first time.The obtained composites were dense and showed good mechanical properties,especially the strength and toughness,706 MPa and 7.33 MPa·m^(1/2),respectively,coupled with high hardness of 21.3 GPa,and stiffness of 452 GPa.SiC and Zr_(2)[Al(Si)]_(4)C_(5) constituted a reinforcing system with synergistic effects including grain refinement,grain pull-out as well as crack branching,bridging,and deflection.Besides,the oxidation results of the composites showed that the oxidation kinetics followed the parabolic law at 1600℃,and the oxidation rate constants increased with the increase of Zr_(2)[Al(Si)]_(4)C_(5) content.The formation and evolution model of the oxidation structure was also investigated,and the oxide scale of the composite exhibited a three-layer structure.

Elucidating the role of preferential oxidation during ablation:Insights on the design and optimization of multicomponent ultra-high temperature ceramics

Multicomponent ultra-high temperature ceramics(UHTCs)are promising candidates for thermal protection materials(TPMs)used in aerospace field.However,finding out desirable compositions from an enormous number of possible compositions remains challenging.Here,through elucidating the role of preferential oxidation in ablation behavior of multicomponent UHTCs via the thermodynamic analysis and experimental verification,the correlation between the composition and ablation performance of multicomponent UHTCs was revealed from the aspect of thermodynamics.We found that the metal components in UHTCs can be thermodynamically divided into preferentially oxidized component(denoted as MP),which builds up a skeleton in oxide layer,and laggingly oxidized component(denoted as ML),which fills the oxide skeleton.Meanwhile,a thermodynamically driven gradient in the concentration of MP and ML forms in the oxide layer.Based on these findings,a strategy for pre-evaluating the ablation performance of multicomponent UHTCs was developed,which provides a preliminary basis for the composition design of multicomponent UHTCs.

TNM钛铝合金高温抗氧化行为研究

TNM(Ti–43Al–4Nb–1Mo–0.1B)钛铝合金具有较低的密度、优异的高温力学性能和较好的高温变形能力,其长期服役温度可达750℃左右,是备受瞩目的新一代航空发动机低压涡轮叶片用材料.选取热暴露温度时间不同的两个热暴露条件对TNM合金在空气中进行氧化实验,采用扫描电子显微镜、能谱仪及X射线光电子能谱分析仪对试样的表面形貌、氧化物组成进行分析,系统研究了TNM合金在不同温度、不同时间热暴露条件下的氧化规律.结果表明,在700℃和760℃下,TNM合金抗氧化级别分别为完全抗氧化和抗氧化等级.700℃下,TNM合金在氧化初期先生成TiO_(2),随后Al_(2)O_(3)逐渐增加,直至覆盖整个样品,在氧化进行200 h时,表面生成的氧化物主要为Al_(2)O_(3),含有少量的MoO_(2)、MoO_(3),能保持较好的抗氧化性;760℃条件下,合金在氧化初期即形成不稳定的Al的氧化物与Ti的氧化物,表面生成的氧化物主要为TiO_(2)和少量的MoO_(2)、MoO_(3)与MoO_(x)的氧化物.

吉木萨尔页岩油注气相态物性变化特征实验研究

为探索不同注入气体对页岩油的相态行为及物性变化特征,综合利用高温高压PVT物理模拟实验系统及气相色谱,开展了减氧空气(含氧量10%)、空气、CO_(2)的注气膨胀实验研究,通过实时监测不同油气体系相态行为的变化情况,分析了不同注入气对地层油体系饱和压力、膨胀系数、黏度和密度等物性参数的影响。结果表明,不同注入气体对于地层油的相态行为及物性影响存在显著差异。向页岩储层注入空气,可与原油接触,发生低温氧化反应,空气含氧量越高低温氧化作用越强,越有助于气相溶解至油相中,体系饱和压力越低;注入CO_(2)时,易与原油产生较好的混相作用进而可增强气体的溶解性。受限于较高的溶解饱和压力,高含氧量空气与减氧空气的膨胀系数相差不大,但高含氧量空气的降黏效果较明显,CO_(2)可在压差和扩散作用下进入原油内部,抽提萃取强度更大,膨胀降黏效果最好。高含氧量空气与原油接触时,可产生质量交换,使得轻质组分萃取至气相中,加速重质组分占比升高,原油密度逐渐增大。CO_(2)对于低碳组分的强抽提作用可促使原油轻质组分向重质组分转化,进而导致原油密度上升的幅度更大,注CO_(2)开发有望成为页岩油提高采收率并兼顾埋存的有效途径。该研究成果可为页岩储层注气的高效开发提供借鉴。

CVD法制备Inconel 718高温合金表面铝化物涂层高温氧化行为研究

Inconel 718高温合金是燃气轮机和航空发动机热端部件的关键核心材料,其表面通常制备有铝化物涂层,起到提高抗氧化和热腐蚀性能的作用。理解铝化物涂层的高温氧化行为,是提高部件抗高温氧化能力的关键。采用化学气相沉积(CVD)技术,在Inconel 718高温合金表面制备了铝化物涂层,在大气环境、950℃条件下开展了恒温氧化测试,采用扫描电子显微镜、X射线衍射和X射线能谱等手段,研究了其高温氧化行为,并与Inconel 718高温合金进行对比。结果表明:Inconel 718高温合金表面制备的CVD铝化物涂层,其表面粗糙,具有双层结构。外层为富含Ni和Al元素的β-NiAl层,平均厚度为14.1μm,内层为富含Fe和Cr元素的σ相与富含Nb、Mo和Fe元素的Laves相共存的互扩散层,平均厚度为5.9μm。恒温氧化后,Inconel 718高温合金表面氧化生成了Cr_(2)O_(3)膜,而CVD铝化物涂层表面氧化生成了α-Al_(2)O_(3)膜。Cr_(2)O_(3)膜和α-Al_(2)O_(3)膜的生长都遵循抛物线型生长规律,Cr_(2)O_(3)膜的生长速率常数为0.86μm·h^(-1/2),α-Al_(2)O_(3)膜的生长速率常数为0.15μm·h^(-1/2)。此外,观察发现Inconel 718高温合金发生了内氧化,而CVD铝化物涂层未出现内氧化,两者氧化行为差异的原因在于CVD铝化物涂层中的β-NiAl相,其氧化生成均匀、连续、致密的α-Al_(2)O_(3)膜,阻止了内部金属发生进一步氧化。本研究揭示了Inconel 718高温合金和CVD铝化物涂层的抗高温氧化作用机理,为Inconel 718高温合金用高抗氧化性CVD铝化物涂层的制备及应用提供了技术支撑。

镍基高温合金U720Li在750℃不同氧化阶段的恒温氧化行为

航空发动机涡轮盘服役温度的不断升高,对材料的抗氧化性能提出了更严苛的要求。U720Li合金是一种具有较高承温能力的涡轮盘用镍基高温合金,其长期服役温度高达750℃。阐明该合金在服役温度下的氧化行为,对延长涡轮盘的服役寿命具有重要意义。本文采用静态增重法测定了锻态U720Li合金在750℃的氧化动力学曲线,用XRD、SEM-EDS等手段分析了不同氧化阶段的氧化膜形貌、结构及元素分布。结果表明,U720Li合金在其服役温度下具有优异的抗氧化性能,在750℃的恒温氧化动力学曲线大致遵循立方规律,达到了完全抗氧化级别。分析认为,U720Li合金在氧化初期生成了疏松的γ-Cr_(2)O_(3),随着氧化的进行,γ-Cr_(2)O_(3)层不断剥落,氧化膜变得更加连续致密并形成复杂多层结构,且在氧化膜附近基体内形成γ'贫化层。在稳定氧化阶段,氧化膜更加连续致密并形成规整的双层结构,包括致密的α-Cr_(2)O_(3)外氧化层和α-Al_(2)O_(3)内氧化层。连续致密的α-Cr_(2)O_(3)和α-Al_(2)O_(3)层的形成能够有效阻止氧的内扩散及合金元素的外扩散,保障了U720Li合金的优异抗氧化性能。

Molten salt synthesis, formation mechanism, and oxidation behavior of nanocrystalline HfB2 powders

Nanocrystalline Hf B2 powders were successfully synthesized by molten salt synthesis technique at 1373 K using B and Hf O2 as precursors within KCl/Na Cl molten salts.The results showed that the as-synthesized powders exhibited an irregular polyhedral morphology with the average particle size of 155 nm and possessed a single-crystalline structure.From a fundamental aspect,we demonstrated the molten-salt assisted formation mechanism that the molten salts could accelerate the diffusion rate of the reactants and improve the chemical reaction rate of the reactants in the system to induce the synthesis of the high-purity nanocrystalline powders.Thermogravimetric analysis showed that the oxidation of the as-synthesized Hf B2 powders at 773–1073 K in air was the weight gain process and the corresponding oxidation behavior followed parabolic kinetics governed by the diffusion of oxygen in the oxide layer.

Ni基高温合金在LiCl-KCl熔盐中的腐蚀行为研究

熔盐电解精炼是乏燃料干法后处理的核心工艺单元,其反应容器需在高温、LiCl-KCl熔盐环境下长期服役,活泼合金元素Cr的选择性溶解使得钝化Cr_(2)O_(3)保护膜难以生成,结构材料面临严重的腐蚀问题,严重阻碍了干法后处理技术的工程化应用。Ni基高温合金在高温氯化物熔盐中的热力学性质稳定,是电解精炼反应容器潜在的候选材料,然而目前Mo、W等关键合金元素对Ni基高温合金在LiCl-KCl熔盐中的耐腐蚀性能影响暂不明确。采用浸泡腐蚀的方法,研究了Haynes 230、Inconel 625、GH 3535、Inconel 690和GH 4169五种Ni基高温合金在550℃、氩气气氛下LiCl-KCl熔盐中的腐蚀行为,采用X射线衍射、扫描电子显微镜及能谱分析对腐蚀产物的组成和形貌进行了分析。研究结果表明,五种Ni基高温合金在与LiClKCl熔盐相互作用的过程中均发生腐蚀失重,失重情况为Inconel 625>GH 3535>Haynes 230>Inconel690>GH 4169。其中Inconel 625和GH 4169合金在基体近表层生成了富Mo氧化膜,导致外层(Cr,Fe)2O3与基体的热相容性变差,有明显的脱落趋势。相比高Cr含量的Inconel 690合金发生严重的电化学溶解,低Cr的GH 3535合金外层(Cr,Fe)_(2)O_(3)含量低,抗氧化能力也明显降低,使得氧向基体内部渗入。而Haynes230合金外表面生成了富W的氧化物,有效地阻挡了Cl^(-)的侵蚀,在以上五种Ni基高温合金中具有最好的耐腐蚀性能。