Nb-Hf合金表面Si-Ti-Cr硅化物涂层在恒温氧化和热震中的高温抗氧化性能（英文）

为了提高Nb-Hf合金的高温抗氧化性能,采用浆料烧结和高温渗透制备了Si-Ti-Cr硅化物涂层。分析了Si-Ti-Cr硅化物包覆的Nb-Hf合金样品在恒温氧化和高温热震条件下的抗氧化性能,揭示了Si-Ti-Cr涂层高温恒温氧化和高温热震条件下的失效机理。结果表明,在1800℃恒温氧化5 h条件下,涂层的增重为7 mg/cm²;在1700℃热震循环50周次和恒温氧化5 h条件下,涂层的最大增重为1.8mg/cm²。硅化物涂层在1800℃恒温氧化环境下和1700℃热震/恒温氧化环境下具有优异的抗氧化性能。     

超音速大气等离子喷涂TiB2-SiC涂层的抗氧化性及耐熔盐腐蚀性能

采用超音速大气等离子喷涂制备全包覆TiB₂-SiC涂层,研究了TiB₂-SiC涂层在400和800 ℃的氧化性能,并探究其氧化机理。对TiB₂-SiC涂层在900 ℃下的抗铝熔盐腐蚀性能进行研究,并探讨其耐熔盐腐蚀机理。结果表明,超音速大气等离子喷涂制备的TiB₂-SiC涂层具有良好的抗氧化性,在400 ℃的氧化速率常数为1.92×10^-5 mg²·cm^-4·s^-1,在800 ℃的氧化速率常数为1.82×10^-4 mg²·cm^-4·s^-1。超音速大气等离子喷涂制备的TiB₂-SiC涂层在900 ℃下具有良好的抗熔盐腐蚀性能,熔盐腐蚀后TiB₂-SiC涂层都保持致密结构,未发生涂层的开裂及剥落。     

植酸修饰改性对TC4钛合金微弧氧化膜层性能的影响

通过向电解液中添加有机酸植酸,提升了TC4钛合金微弧氧化涂层的耐腐蚀性能和热稳定性。通过扫描电子显微镜、X射线衍射仪、X射线光电子能谱仪和热冲击实验等技术手段,分析了植酸对涂层形成、形貌和性能的影响。结果显示,植酸的添加使放电微孔更加细小,提高了涂层的形成效率并优化了相结构。通过动电位极化测试,发现添加植酸显著提高了微弧氧化涂层的耐腐蚀性能。将电解液中的植酸浓度调整为12 mL/L（最佳植酸浓度）后,腐蚀电流密度由8.406×10^-5 A·cm^-2降低至2.580×10^-6 A·cm^-2。循环高温氧化试验结果表明,TC4钛合金的耐热冲击性能和高温抗氧化性能得到了改善。     

MoSi2/Mo涂层热震过程中界面应力分布和裂纹扩展的有限元模拟

在氢气保护下将MoSi₂/Mo涂层加热至1000 ℃,再迅速冷却至室温进行热震循环,表征了材料在热震循环过程中裂纹的演变过程并评估了MoSi₂/Mo涂层的热冲击行为。采用Abaqus软件计算了MoSi₂/Mo涂层在热冲击过程中的应力分布,讨论了热震循环中裂纹的发展过程。结果表明：Mo基体与MoSi₂涂层之间存在较高的热冲击应力,这将导致裂纹的萌生和扩展。计算结果显示：在最初的10次热震循环中,涂层产生了垂直于界面的裂纹,在界面上没有出现裂纹,涂层与基体仍结合良好;在随后的热震循环中开始出现界面裂纹,界面裂纹开始于垂直裂纹的末端区域,当垂直裂纹与界面裂纹汇聚,会导致涂层剥离和涂层失效。     

钼合金MoSi2涂层高温热震行为与裂纹扩展

采用料浆烧结法在钼合金表面制备了MoSi₂涂层,利用内热法测试了涂层室温～1600℃抗热震性能,通过扫描电镜(SEM)、电子探针(EPMA)、波谱分析(WDS)和X射线衍射(XRD)等测试手段分析了不同热震次数的涂层微观形貌、组织结构以及裂纹萌生扩展。结果表明：涂层可承受室温～1600℃热震400次,热震过程中涂层由原始的MoSi₂-Mo₅Si₃双层结构演变为SiO₂-MoSi₂-Mo₅Si₃多层结构,涂层热震初期形成纵向裂纹并不断向基体扩展,热震后期裂纹贯穿涂层到达基体,MoO₃挥发使涂层/基体界面应力增大产生横向裂纹,导致涂层剥落失效。     

LaAl添加对放电等离子烧结LaFeSi磁体微观结构和磁热效应的影响

使用LaFe_11.3Si_1.7薄带合金为前驱体粉末,研究了低熔点La_0.77Al_0.23合金添加对放电等离子烧结磁体微观结构和磁热性能的影响。研究发现,适量低熔点LaAl合金的添加能够促进包晶反应,制得了具有较高1:13相含量的LaFeSi磁体。磁体中观察到有微弱的巡游电子变磁转变现象的存在。热处理工艺研究显示,退火时间的增加会使得磁体的磁性转变由一级向二级变化,这主要归因于Al向1:13相内部的扩散。1000 ℃/6 h热处理工艺条件下,其在0~5 T磁场变化下的磁熵变最大,达12.40 J?kg^-1?K^-1,而1000 ℃/10 h条件下所获得磁体的制冷能力最强,为318.40 J?kg^-1。     

石墨抗氧化SiC涂层的制备与性能研究

本文以SiC、Si和酚醛树脂为主要原料,通过浸涂和气相渗硅两步法在石墨表面制备了SiC抗氧化涂层。利用XRD、SEM研究了涂层的相组成与形貌。结果表明,气相渗硅后涂层的主相为α-SiC,β-SiC和Si,其中Si是气相渗硅过程中残留的。涂层与基体之间具有过渡结构,致密度良好。抗氧化和抗热震实验表明：由气相渗硅工艺制备的SiC涂层结构致密,具有良好的抗氧化性能,1200℃空气条件下氧化16 h后试样每小时增重量约为2.18 mg/cm₂。涂层具有良好的抗热震性能,经1000 ℃—室温循环热震15次后试样质量变化百分率仅为-0.17%。     

CeO_2粉体对激光熔覆Ni基合金层抗高温热震性能的影响

为了研究激光熔覆中添加纳米CeO2粉体对涂层抗高温热震性能的影响,采用压片预置式激光熔覆工艺,添加适量纳米CeO2粉体,利用NiCoCrAlY合金粉末在GH4037合金表面激光熔覆制备了Ni基合金涂层,对熔覆层进行了1070℃高温抗热震性能试验。结果表明,添加适量纳米CeO2粉体的Ni基合金激光熔覆涂层经1070℃10次高温热震循环后,其表面氧化膜由大面积的扩展剥落转变为小的单元剥落;经100次热震循环后,其涂层内氧化得到有效抑制,横切面上裂纹数量及尺寸均小于未加纳米粉体的涂层,且均未出现内部裂纹,其抗高温热震性能得到显著提高。     

电流密度对ZK60镁合金表面超疏水涂层的制备及耐腐蚀性的影响

为了提高镁合金的耐腐蚀性能,基于层状双氢氧化物（LDHs）膜在ZK60镁合金表面制备了超疏水（SH）涂层。涂层制备过程中引入电场辅助,研究了工作电流密度对涂层性能的影响。结果表明,工作电流密度显著影响LDHs膜的微观结构,这对SH涂层的疏水性具有重要影响。当工作电流密度为25 mA/cm²时,SH涂层表面呈现均匀的微纳米结构,并表现出超疏水性。超疏水涂层的腐蚀电流密度（I_corr=9×10^-7 A·cm^-2）比ZK60基体的腐蚀电流密度（I_corr=3×10^-5 A·cm^-2）低了2个数量级,表现出优异的耐腐蚀性。     

Inconel 617合金高温热变形行为与组织演变

为解决Inconel 617合金的高温加工问题，对锻造Inconel 617合金的高温热变形行为进行了研究。利用Gleeble-3500热模拟试验机研究了Inconel 617合金在900~1200 ℃、应变速率为0.001~10 s^-1范围内的热塑性行为。推导了该温度和应变速率下的本构方程，得到了该温度范围内的热加工图。用电子背散射衍射研究了合金压缩后的动态再结晶。确定了失稳区的位置，并表明在热变形条件下，确实发生了动态再结晶，获得了细小的晶粒。Inconel 617热处理的最佳温度范围为1075~1175 ℃，该温度范围处于材料的安全区。     

High temperature performance of arc-sprayed aluminum bronze coatings for steel

1 Introduction The aluminum bronze coatings on steel substrate which are sprayed by electric arc process have been developed as possible new candidates for the use to high temperature applications, while their corrosion properties at high temperature in …     

Preparation of three-dimensional braided carbon fiber reinforced mullite composites from a sol with high solid content

To prepare the three-dimensional braided carbon fiber reinforced mullite (3D C/mullite) composites, an Al₂O₃-SiO₂ sol with a solid content of 20% (mass fraction) and an Al₂O₃/SiO₂ mass ratio of 2:1 was selected as the raw material. Characteristics and mullitization of the sol were analyzed throughly. It is found that the formation of mullite is basically completed at 1300 °C and the gel powders exhibit favorable sintering shrinkage. The 3D C/mullite composites without interfacial coating were fabricated through the route of vacuum impregnation-drying-heat treatment. Satisfied mechanical properties with a flexural strength of 241.2 MPa and a fracture toughness of 10.9 MPa·m^1/2 are obtained although the total porosity reaches 26.0%. Oxidation resistances of the composites at 1200, 1400 and 1600 °C were investigated. Due to the further densification of matrix, the 3D C/mullite composites show tiny mass loss and their mechanical properties are well retained after oxidation at 1600 °C for 30 min.     

Thermal properties and microstructure of a plasma sprayed wollastonite coating

Wollastonite coatings were deposited using an atmospheric plasma spraying technique. The microstructure and phase compositions of the coating before and after heat treatment were investigated using scanning electron microscopy (SEM), x-ray diffraction (XRD), and differential thermal analysis (DTA) technologies, respectively. In addition, the coefficient of thermal expansion and thermal diffusivity of the coating were also investigated. Crystalline wollastonite, glassy phase, and tridymite (SiO₂) were observed in the coating. Tridymite (SiO₂) likely reacted with other composites such as CaO and glassy phase to form crystalline wollastonite when the coating was heated at about 882 °C. During the first thermal cycle, the coefficient of thermal expansion of the coating decreased dramatically between 700 and 850 °C and the thermal diffusivity of the coating was 2.7–3.1 × 10⁻³cm²/s between 20 and 1000 °C. During the second thermal cycle, the coefficient of thermal expansion of the coating increased slightly between room temperature and 1000 °C and the thermal diffusivity of the coating increased by about 20% compared with that of the first thermal cycle. The atmospheric plasma sprayed Wollastonite coating may be used as thermal barrier coating.     

Formation of high-density TiN/Ti<Subscript>5</Subscript>Si<Subscript>3</Subscript> ceramic composites using preceramic polymer

The formation, microstructure and properties of high-density TiN/Ti₅Si₃ ceramic composites created by the pyrolysis of preceramic polymer with filler were investigated. Methylpolysiloxane was mixed with TiH₂ as filler and ceramic composites prepared by pyrolysis at 1200°C to 1600°C under N₂, Ar and vacuum were studied. When a specimen with 70 vol.% TiH₂ was pyrolyzed up to 1600°C in a vacuum after a preheat treatment at 850°C in a N₂ atmosphere and subsequently heat-treated at 1600°C for 1 h under Ar at a pressure of 2 MPa, a ceramic composite with full density was obtained. The microstructure of the ceramic composite was composed of TiN and Ti₅Si₃ phases. Under specific pyrolysis conditions, a ceramic composite with a density of 99.2 TD%, a Vickers hardness of 18 GPa, a fracture toughness of 3.5 MPam^1/2, a flexural strength of 270 MPa and a electrical conductivity of 6200 ohm⁻¹·cm⁻¹ was obtained.     

An investigation of the effect of thermal cycling on plasma‐sprayed zirconia/NiCoCrAlY thermal barrier coating

The microstructural change, crack initiation and spallation of a vacuum plasma sprayed (VPS) thermal barrier coating on an INCONEL‐738 superalloy substrate were investigated after successive 300 h thermal cycles at 1050°C. The coating was characterised using Raman spectroscopy, scanning electron microscopy (SEM) energy dispersive X‐ray analysis (EDX) and Auger electron spectroscopy (AES). Localised micro‐cracks at the yttrium (III) oxide stabilised zirconium (IV) oxide (YSZ) ceramic coating/thermally grown oxide (TGO) interface were observed after 8 cycles. Spallation of the YSZ coating occurred after approximately 21 cycles. Significant amounts of the elements titanium, tantalum and chromium were found within the TGO together with the formation of nickel, cobalt and chromium‐rich oxides at this TGO/YSZ interface.     

The superior thermal stability and tensile properties of hot rolled W-HfC alloys

Herein, a W-0.5wt%HfC (WHC05) alloy is fabricated by conventional sintering and multi-step hot-rolling. The high-temperature stability and tensile properties at different temperatures, ranging from room temperature to 600 °C, are studied to demonstrate the influence of HfC addition. The results reveal that the WHC05 alloy has a higher recrystallization temperature (1400 °C–1500 °C) than the previously reported as-rolled pure W (1200 °C) and as-rolled W-0.5wt%ZrC (WZC05 ~ 1300 °C) alloy. Moreover, after recovery and recrystallization (annealing at 1600 °C), the WHC05 alloy maintained a high ultimate tensile strength of ~300 MPa and exhibited a desirable increase in total elongation (>35%), which is ~1.6 times higher than the recrystallized WZC05 at 500 °C. The superior thermal stability and excellent high-temperature mechanical properties can be ascribed to the unique microstructure and uniform dispersion of nano-sized HfC particles in W matrix. The influence of annealing temperature on grain structure, grain orientation and distribution of nano-sized HfC particles has been studied to unveil the possible mechanism of enhanced thermal stability and superior mechanical properties.     

Formation and oxidation resistance of Hf and Al modified silicide coating on Nb–Si based alloy

Codeposition of Si, Al and Hf were prepared by pack cementation at 1300 °C for 10 h. The results show that the coating is composed of a thick (Nb, X)Si₂ outer layer, a (Ti, Nb)₅Si₄ middle layer and a thin discontinuous (Cr, Al)₂(Nb, Ti) inner layer. The mass gain of the coating is only 4.12 mg/cm² after isothermal oxidation at 1250 °C for 100 h. Some “oxide pegs” form at the interface of the oxide scale and coating. The coating exhibits good cyclic oxidation resistance due to the improved adhesion between the oxide scale and coating.     

Oxidation behavior of C/C composites with SiC/ZrSiO4–SiO2 coating

A SiC/ZrSiO₄–SiO₂ (SZS) coating was successfully fabricated on the carbon/carbon (C/C) composites by pack cementation, slurry painting and sintering to improve the anti-oxidation property and thermal shock resistance. The anti-oxidation properties under different oxygen partial pressures (OPP) and thermal shock resistance of the SZS coating were investigated. The results show that the SZS coated sample under low OPP, corresponding to the ambient air, during isothermal oxidation was 0.54% in mass gain after 111 h oxidation at 1500 °C and less than 0.03% in mass loss after 50 h oxidation in high OPP, corresponding to the air flow rate of 36 L/h. Additionally, the residual compressive strengths (RCS) of the SZS coated samples after oxidation for 50 h in high OPP and 80 h in low OPP remain about 70% and 72.5% of those of original C/C samples, respectively. Moreover, the mass loss of SZS coated samples subjected to the thermal cycle from 1500 °C in high OPP to boiling water for 30 times was merely 1.61%.