Ni76Cr19AlTi合金的高温氧化行为

采用静态恒温氧化增质法研究Ni76Cr19AlTi合金在600~800℃范围内的高温氧化动力学规律,采用场发射扫描电镜对氧化产物进行表面和横断面形貌观察,用X射线衍射仪分析氧化膜层的物相组成。结果表明,合金在600~800℃范围内氧化增质与氧化时间的关系遵从抛物线规律,氧化速率常数Kp随温度的升高而增大;在800℃下氧化200 h,平均氧化速率为0.002 15 mg.cm-2.h-1,合金属于完全抗氧化级;氧化过程中,氧化膜主要受控于Cr2O3的生长,经过长时间氧化后,表层为比较疏松的TiO2和Cr2O3,内层为起保护作用的Cr2O3和Al2O3,氧化膜的组成以Cr2O3为主。     

Isothermal oxidation behavior of cast Ni-base superalloy K44

The oxidation behavior of a cast Ni-base superalloy K44 in air at 850-1 000℃ for 100 h was studied. The scales on the surface were determined by SEM and EPMA equipped with an EDXS. The results show that oxidation kinetics obey the parabolic law fi＇om which the values of activation energy Qp1=221.1 kJ/mol and Qp2=247.6 kJ/mol are estimated. The oxidation scales are composed of loose outer layer of TiO2/TiO-Cr2O3 and a small amount of NiCr204 and NiAl2O4, compact intermediate layer Cr2O3, and precipitate of internal oxides Al2O3.     

含纳米ZrO2颗粒复合电铸层高温氧化行为研究

通过间歇式高温氧化实验,建立了纯镍电铸层和Ni—ZrO2纳米复合电铸层高温氧化动力学模型,分析了电铸层表面和横截面的形貌,测定了脉冲复合电铸层横截面中各组织成分的分布状态。结果表明,Ni—ZrO2纳米复合电铸层高温氧化性能明显优于纯镍铸层,复合电铸层表面生成的氧化膜晶粒细小且致密。复合电铸层表面的氧化膜与复合电铸层的黏附性较好,这是由于其较薄,并且所产生的内应力较小所致。     

2507双相不锈钢高温氧化行为

通过高温氧化试验(1200℃,保温5 min,氧化气氛A和B)模拟了2507双相不锈钢热轧初期的氧化过程,并应用扫描电子显微镜( SEM)、辉光放电光谱仪(GDS)、X射线衍射仪(XRD)和X射线光电子能谱仪(XPS)等手段,分析了不同气氛下氧化膜的组成和结构以及初期氧化特性.结果表明:氧化膜主要由Fe3O4、Cr2O3和尖晶石型(FeCr2O4、MnCr2O4等)等复合氧化物组成;气氛中氧含量的变化可改变氧化膜中氧化物结构、组成,铁素体优先于奥氏体氧化.     

High-temperature oxidation of pure titanium in CO2 and Ar-10%CO2 atmospheres

The oxidation behavior of pure titanium has been investigated in the temperature range of 1000 K to 1300 K in CO₂ or Ar-10%CO₂. Optical microscopy, electron probe microanalyses, and X-ray measurements on the oxide scales formed during oxidation indicate that their structures are nearly independent of temperature and the corrosion atmosphere. The scales consisted of two layers, an external one and an internal one, having a rutile (TiO₂) structure. The parabolic rate law was confirmed for growth of the external scale and the permeation depth of oxygen in titanium with apparent activation energies of 266 and 226 kJ/mol, respectively. The rate-determining diffusion species in the oxidation processes are discussed.     

Comparisons of high temperature oxidation behavior between reactive-sintered and melted Ti-45at.%Al-1.6at.%Mn intermetallics

In order to investigate high temperature oxidation behavior, isothermal oxidation experiments for Ti-45at.%Al-1.6at.%Mn intermetallics prepared by both reactive sintering and melting were carried out in both oxygen and air environments at temperatures of 900, 1000 and 1100°C. In the oxygen environment, reactive sintered Ti-45at.%Al-1.6at.%Mn was found to have excellent oxidation resistance due to the formation of a continuous A1₂O₃ layer at temperatures up to 1100°C; however, when melted it showed very poor oxidation resistance at and above 1000°C. Weight gains of the melted specimen after 12 hours, especially at the temperature of 1000°C and 1100°C, were nearly 12 times that of the reactive sintered one. In air, the reactive-sintered intermetallics showed a poorer oxidation resistance man did that in the oxygen environment. Especially, the weight gains in air were 6 times larger than the weight gains in oxygen when oxidized at 1100°C for 12 hours.     

Oxidation behavior of TiAl coated with a fine-grain Co-30Cr-4Al film

The oxidation behavior of TiAl coupons coated with a fine-grain Co-30Cr-4Al (mass %) film of about 30-m thickness has been studied at 1100–1400 K in a flow of purified oxygen at atmospheric pressure for up to 500 ks. Three oxidation stages were recognized: initial transient, parabolic, and accelerated stages. However, at 1100 K a parabolic stage continues for more than 800 ks. The activation energy for parabolic oxidation agrees with reported values for the oxidation of alumina-former alloys, although the mass gains during the parabolic stages are relatively small at 1200 and 1300 K. Micropores developed mainly at the scale/coating and coating/substrate interfaces as oxidation proceeded. This is attributable to recrystallization of the coating during oxidation and a Kirkendall effect due to preferential diffusion of Co into the substrate. The accelerated oxidation can be explained in terms of the formation of rutile mounds on the scale.     

Oxidation and sulfidation behavior of Fe-20Cr-16Ni-4Al-1Y2O3 oxide-dispersion-strengthened alloy

High-temperature oxidation and sulfidation studies were conducted on an oxide-dispersion-strengthened alloy of composition Fe-20Cr-16Ni-4Al-1Y₂O₃. The oxidation studies were conducted in air and low-PO₂ environments over a temperature range of 650–1200°C. Results are also reported on the sulfidation resistance of preformed oxide scales and the influence of reoxidation of preformed sulfide scales. Detailed microstructural results and x-ray diffraction analysis data are presented to substantiate the corrosion behavior of the alloy over the wide range of conditions anticipated in fossil-energy systems. Data are also presented on the corrosion behavior of the alloy in oxygen/sulfur mixed gas atmospheres, and the results are used to compare the corrosion behavior of the present alloy with other chromia- and alumina-forming alloys.     

High-temperature oxidation of Fe-16.7% Mn-2.1% Ni-6.6% Si alloy in SO2

The oxidation of an austenitic Fe-16.7% Mn-2.1% Ni-6.6% Si (by weight) alloy in SO₂ in the temperature range 600–900°C is described. The corrosion products formed on this alloy in this environment below 800°C consist only of oxides, rather than a mixture of oxides and sulfides as is observed for unalloyed Fe or Mn. The kinetics of oxidation of the alloy in SO₂ in this temperature range are similar to those in O₂. It is proposed that these characteristics result from the presence of a thin silicate layer near the scale-metal interface that alters the gradient of oxygen potential within the scale.     

Oxidation of Ni-base alloys in atmospheres with widely varying oxygen partial pressures

The oxidation behavior of the Ni-base alloys IN 617, IN 713 LC, Ni20Cr, and Ni20Cr+Si has been investigated in the temperature range from 850°C to 1000°C in air and at low-oxygen partial pressure p(O₂) (10^–19 to 10^–16 bar). With the exception of alloy IN 713 LC, the materials show no influence of p(O₂) on the oxidation mechanisms and the kinetics. This result can be explained by the formation of a dense Cr₂O₃ layer, the growth rate of which is controlled by the Cr ion interstitial concentration in Cr₂O₃ at the phase boundary oxide/alloy and the mobility of Cr ions in Cr₂O₃. For the alloy IN 713 LC which develops a dense Al₂O₃ layer in air, a modified transition mechanism at low p(O₂) leads to the formation of Cr₂O₃ at the surface and a strong internal oxidation of Al.     

Corrosion behavior of Fe-20Cr and Ni-20Cr alloys in Ar-H2O-HBr gas mixtures at 1000 K

Discontinuous mass-change measurements and corrosion-product analyses were made for Fe-20Cr and Ni-20Cr alloys after exposing them to Ar-H ₂ O-HBr gas mixtures at 1000 K for 24 hours. Predominantly chromia scales formed on both alloys. Upon cooling, the scales remained adherent to the Fe-20Cr alloy but spalled extensively from Ni-20Cr samples. After tests in HBr-rich gas mixtures, bromine-rich corrosion products were found underneath chromia scales on both alloys while nickel evaporation was observed from Ni-20Cr samples. Preoxidation of the Ni-20Cr alloy prior to exposure to Ar-H ₂ O-HBr gas mixtures increased chromia scale adherence but did not prevent nickel loss from the alloy. Chromia scales formed on the Fe-20Cr alloy were more protective due to the absence of iron oxides in the scale. Large NiO crystals formed over the Ni-20Cr alloy decreased chromia-scale adherence and increased nickel loss from the alloy due to the low stability of NiO in HBr-containing gas mixtures.     

Sulfidation properties of an Fe-23.4Cr-18.6Al alloy at temperatures 1073 and 1173 K in H2S-H2 atmospheres of sulfur at pressures 104-10−5 Pa

An investigation is reported on the sulfidation properties of an Fe-23.4Cr-18.6Al(at.%) alloy at 1073 and 1173 K in H₂S-H₂ atmospheres, 10⁴ > P_{S 2} 10⁵Pa. The sulfidation kinetics exhibited an early transient period before onset of parabolic kinetics. Values of the parabolic sulfidation rate constants increased by as much as 10⁵ from their smallest values at low sulfur pressures, P_{S 2} 10^–4 Pa, to maximum values at sulfur pressures P_{S 2} 10² Pa. Multilayered scales were formed, the number and types of layers dependent on sulfur pressure. A fully developed scale at sulfur pressures P_{S 2} > 10^–3 Pa.     

Sulfidation behavior of Fe-25Cr-20Ni-1.5Al2O3 in simulated coal combustion/gasification environments

The effect of minor addition of -Al₂O₃ dispersoids on the sulfidation behavior of Fe-25Cr-20Ni was investigated over a range of pO₂, 1.13×10^–20 to 1.18×10 ****^–22 atm. at constant pS₂=1.22×10^–8 atm. Fe-25Cr-20Ni and Fe-25Cr-20Ni 1.5 Al₂O₃ with and without preformed oxide scales were exposed to bioxidant gas mixtures H₂/H₂O/H₂S/Ar at 700° C. Both isothermal and cyclic exposures were included. Scales were characterized by a combination of several surface analytical tools. A remarkable improvement in sulfidation resistance is observed in Fe-25Cr-20Ni-1.5Al₂O₃ under the conditions investigated here. This is attributed to the ability of the alloy to form and maintain a predominantly Cr₂O₃ scale with reduced Fe-diffusion and content. Possible scientific reasons for such improvement are discussed. The base alloy, Fe-25Cr-20Ni, fails to develop and retain such a Cr₂O₃ scale and undergoes sulfidation within a few minutes of exposure. The scale breakdown process by sulfidation is explained qualitatively. Experimental evidence suggests that sulfur in the environment enhances Fe-diffusion and content in the scale.     

Oxidation of an Fe—19 wt. % Ni alloy in CO2 at 700–1000°C

The oxidation of an Fe—19.34 wt. % Ni alloy in dry CO₂ has been studied at 700—1000°C using thermogravimetry, metallography, and EPMA. Weight gains for oxygen consumption followed a linear-parabolic-linear sequence at all temperatures. During the initial linear stage the scale consisted mainly of magnetite and the activation energy of 133±25 kJ · mole^–1 is considered to be due to dissociation of CO₂ into CO and adsorbed oxygen on the outer magnetite surface. During the parabolic oxidation stage a continuous Ni-rich layer containing 70% Ni forms a barrier to the diffusion which has an activation energy of 192±79 kJ · mole^–1. The breakdown of the barrier layer causes a return to linear kinetics with an activation energy of 138±42 kJ · mole^–1 for dissociation of CO₂ on the outer surface. During the final linear stage there is pronounced general and intergranular subscale formation. Detailed information is presented of the Ni redistribution and concentrations during oxidation and its correlation with the kinetics and morphology.     

镍基变形高温合金在高温环境下的氧化行为(英文)

研究了617和Haynes230高温合金在含H2O和O2的不纯氦气、含氢的热蒸汽、空气以及纯氦气中的900℃氧化行为。与空气相比,氦气、含氢的热蒸汽对617合金的氧化速率没有明显影响,而Haynes230合金在氦气中表现出较慢的氧化速率。617合金的氧化层形貌和结构受环境的影响明显,而Haynes230受环境的影响不明显。在所有的氧化环境中,Haynes230合金的氧化层都包含有中间层Cr2O3和外保护层MnCr2O4,这使其具有较好的抗氧化性能。合金的表面抗氧化性能明显影响其力学性能,如蠕变和拉伸性能。因此,有必要采取表面处理来增强合金的抗氧化性能。     

0Cr20Ni32AlTi合金的高温微动磨损及摩擦氧化特性(英文)

在300和400℃、载荷80N的条件下,将0Cr20Ni32AlTi合金以水平垂直交叉接触方式进行微动磨损试验,并采用SEM和XPS对磨痕及磨屑进行分析。结果表明:当位移幅值为10和20μm时,微动分别对应于混合区和滑移区,且材料表面均发生严重的磨损和摩擦氧化。微动过程产生大量颗粒状磨屑,经往复碾压后易粘附、聚集于接触区。摩擦氧化反应的生成物主要由Fe3O4、Fe2O3、Cr2O3和NiO等组成。温度和摩擦作用是影响磨屑氧化转化反应速率的主要因素。微动摩擦作用可以增加0Cr20Ni32AlTi合金表面原子的氧化反应活性并降低氧化反应的活化能,从而加快磨屑氧化转化反应的速率。     

Oxidation of a chromia-forming nickel base alloy at high temperature in mixed diluted CO/H2O atmospheres

Corrosion of a chromia-forming nickel base alloy, Haynes 230^®, has been investigated under impure helium containing a few Pa of CO and H₂O at 900 °C. It has been found that this alloy reacts simultaneously with CO and H₂O. Oxidation by CO has been revealed to occur mainly in the first hours. CO diffuses through the scale via short-circuit pathways and oxidizes Al, Cr and Si at the oxide/metal interface. Kinetics of CO oxidation has been investigated and several rate limiting steps are proposed. In the long term, H₂O is the major oxidant of chromia-forming nickel base alloys in impure helium.     

Behavior of Galvalume coated sheet steel at elevated temperatures in O2 and O2/H2O atmospheres

Galvalume (trademark of Bethlehem Steel Corp.) sheet steel samples were heated in pure oxygen and 97% O₂/3% H₂O atmospheres at temperatures ranging from 300 to 670°C. Time at a particular temperature was varied but did not exceed 48 hr. Above 480°C, the Galvalume coating became rapidly alloyed with iron to form Al₁₃Fe₄, and zinc was lost by vaporization. The Zn content dropped to about 15 wt%. The time required to fully alloy the overlay at 490°C was less than 4 hr. Below 480°C, only minor microstructural changes occurred, and coating integrity was maintained. No differences in behavior were observed by the addition of 3% water vapor to the gas stream.