吹喷氧化物质点改善铁基合金的高温耐磨性

为了节省能源,国内外广泛开展了煤的流化床燃烧技术的研究。然而,流化床中埋管材料及其上面所焊鳍片材料耐高温磨蚀性能的提高,是推广这一技术的关键。采用共沉法或机械合金化方法已成功地制成氧化物弥散强化高温合金,不仅高温强度可以维持到合金的熔点附近,而且可以改善高温耐磨性,但这类合金制造工艺复杂、成本高,不适宜大量用于能源工业。向钢水中吹喷氧化物质点可以明显提高镇静钢的室温和高温强度,而且价     

Borides at interfacial zone of IC6 TLP bonded joints

1　INTRODUCTIONTransientliquidphase (TLP)bondingtechniquehasbeensuccessfullyusedinjoiningheatresistantal loys ,likeHastelloyX ,Inconel713C ,In10 0 ,Udimet5 0 0 ,70 0 ,MarM 2 0 0 ,0 0 7,2 4 7,30 2 ,Rene′80 ,TD NiCr ,MA75 4,6 0 0 0 ,PWA14 2 2 ,CSMX 2etc ,whicharesusceptibletohotcrackingor post weldheat treatmentcrackingproblemsduringfusionweld ing[14 ] .Inaddition ,therewerereportsofjoiningNiAlandTiAlintermetallicsbyTLPbondingmethod[510 ] .Forexample ,Galehadinvestigatedthemic…     

The early stage oxidation and evaporation of Mg-9%Al-1%Zn alloy

Thermogravimetric technique was used to determine the oxidation and evaporation behaviour of AZ91D magnesium alloys with 5 and 10 ppm of beryllium at temperatures between 200 and 500 °C. Depending on temperature and time, the alloy experienced protective or non-protective oxidation with linear or accelerated oxide growth kinetics. During reaction in an oxidizing atmosphere, the additions of beryllium delayed the transient from the protective to non-protective scale formation. In an inert atmosphere, increased beryllium contents reduced the magnesium evaporation rate.     

铸件内析出性气孔形成及演化的直接观察与分析

采用透明模型合金实时观察了铸件析出性气孔的形成发展,结果发现,纯物质凝固时,析出性气孔的产生发生于凝固型壳形成之后,随着凝固自型壁向中心凝固,呈现自周边向中心的气条生长。对于合金凝固,析出性气孔在凝固基本完成之后伴随着热裂及缩松的发生开始产生,呈现一定的偏聚现象。浇注前熔体过热度的提高将使析出性气孔更加密集,铸型和环境温度的降低有利于降低气孔的数量及分布范围,采用真空除气,可有效地抑制析出性气孔的产生和热裂缩松缺陷的形成。     

Wear resistance of ceramic coating on AZ91 magnesium alloy by micro-arc oxidation

The ceramic coating formed on AZ91 magnesium alloy by micro-arc oxidation （MAO） was characterized. The results show that the ceramic coating （3.4-23 μm in thickness）on the surface ofAZ91 alloy was attained under different micro-arc oxidation treatment conditions, which consist mainly of MgO, Mg2SiO4 and MgSiO3 phases. Nano-hardness in a cross-sectional specimen was determined by nano-indentation experiment. The MAO coatings exhibit higher hardness than the substrate. Dry sliding wear tests for the MAO coatings and AZ91 alloy were also carded out using an oscillating friction and wear tester in a ball-on-disc contact configuration. The wear resistance of the MAO coatings is improved respectively under different treatment time as a result of different structures of ceramic coatings formed on AZ91 alloy.     

固溶处理对电解制备的A356合金硅颗粒的影响

以电解低钛铝基合金为原料制备了A356合金,研究了在535℃下固溶处理时间对合金共晶硅相细化、球化和分布的影响.测量了硅颗粒的长径和短径,计算了颗粒的直径和长短径比值等参数,分析了上述参数随固溶时间的变化及其概率密度分布.实验结果表明:由该电解合金制备的A356合金经2～4 h的固溶处理,共晶硅就可得到较好的细化和球化效果,具有较高的分布集中度;A356合金的固溶处理时间可有效缩短.     

Corrosion of metals and alloys in mixed gas environments at elevated temperatures

The attack of nickel, cobalt, iron, and alloys of these metals containing chromium and aluminum, by gases containing sulfur-oxygen, carbon-oxygen, and nitrogen-oxygen has been studied at temperatures of 600 and 900°C. The degradation of these metals and alloys was characterized by using standard analytical techniques with emphasis on optical metallography. Three types of accelerated degradation were identified for the attack of alloys by gases containing another oxidant in addition to oxygen. One type of degradation occurred because of the formation of reaction products composed of mixtures of phases involving both of the oxidants. Another type resulted from the reaction of second oxidant phases with oxygen. The third form of degradation involved the development of less protective phases due to thermodynamic instabilities. Thermodynamic stability diagrams are used to help account for the effects produced by different elements in the alloys.     

合金元素对镁合金的性能影响研究

研究了新型镁铝锌合金的性能,分析了不同含量的Al、Zn、Pb等元素对镁合金性能的影响.结果表明,随着Al含量的增加,合金的冲击韧性下降而硬度提高;随着Zn含量的增加,冲击韧性和硬度都下降;而随着Pb含量的增加,合金的冲击韧性和硬度都提高.     

High cycle fatigue behaviour of Ti–6Al–4V alloy at elevated temperatures

High cycle fatigue behaviour of Ti–6Al–4V alloy was studied at 623 K and 723 K. Fatigue strength decreased at elevated temperatures compared with at ambient temperature. In the short life regime, fatigue strength was lower at 723 K than at 623 K, but in the long life regime it was nearly the same at both temperatures. At elevated temperatures, cracks were generated earlier at applied stresses below the fatigue limit at ambient temperature, indicating lowered crack initiation resistance. Small cracks grew faster at elevated temperatures than at ambient temperature, which became more noticeable with increasing temperature. After allowing for the elastic modulus, small cracks still grew faster at elevated temperatures.     

AI-Li/SiCp composites and Ti-AI alloy powders and coatings prepared by a plasma spray atomization (PSA) technique

There has been increasing use of Al-Li alloys in the aerospace industry, due mainly to the low density and high elastic modulus of this material. However, the problem of low ductility and fracture toughness of this material has limited its present application to only weight- and stiffness-critical components. Development of Al-Li/ceramic composites is currently being investigated to enhance the service capabilities of this material. The Ti-Al alloy is also of interest to aerospace-type applications, engine components in particular, due to its attractive high-temperature properties. Preparation of fine powders by plasma melting of composite feedstock and coatings formed by plasma spraying was carried out to examine the effect of spray parameters on the microstructure and properties of these materials. Characterization of the powders and coatings was performed using the scanning electron microscope and image analyzer. Examination of the plasma-sprayed powders and coatings has shown that in the Al-Li/SiC composite there is melting of both materials to form a single composite particle. The SiC reinforcement was in the submicron range and contributed to additional strengthening of the composite body, which was formed by a cold isostatic press and consolidated by hot extrusion or hot forging processes. The plasma-sprayed Ti-Al powder showed four categories of microstructures: featureless, dendritic, cellular, and martensite-like.