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81.
82.
固溶处理对电解制备的A356合金硅颗粒的影响 总被引:3,自引:1,他引:3
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. 相似文献
83.
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. 相似文献
84.
85.
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. 相似文献
86.
K. A. Khor F. Y. C. Boey Y. Murakoshi T. Sano 《Journal of Thermal Spray Technology》1994,3(2):162-168
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. 相似文献
87.
Biaxial forming behavior is investigated for three aluminum sheet alloys (Al 5182 containing 1% Mn (5182+Mn), Al 5754, and
6111-T4) using a heated die and punch in the warm forming temperature range of 200–350 °C. It is found that, while all three
alloys exhibit significant improvement in their formability compared with that at room temperature, the non-heat-treatable
alloys 5182 + Mn and 5754 give higher part depths than that of heat-treatable 6111-T4. The formability generally increases
with decreasing BHP (BHP), but increasing the forming temperature and/or BHP minimizes the wrinkling tendency and improves
the forming performance. The stretchability of the sheet alloys increase with increasing temperature and increasing BHP. For
the alloys and forming conditions involved in the current study, the formability, measured in terms of part depth, comes mainly
from the drawing of metal into the die cavity, although stretching effects do influence the overall forming behavior. The
optimum formability is achieved by setting the die temperature 50 °C higher than the punch temperature to enhance the drawing
component. Setting the die temperature higher than the punch temperature also improves the strain distribution in a part in
such a manner that postpones necking and fracture by altering the location of greatest thinning. 相似文献
88.
F. Sommer 《Journal of Alloys and Compounds》1995,220(1-2):174-178
Trends in the dependences on temperature and concentration of experimentally determined heat capacities of liquid and undercooled liquid metals and alloys are discussed. A new adiabatic calorimeter for determining the heat capacity of liquid alloys up to 1500 K is described. The ability of several approximations and models to describe the different characteristics of the heat capacity of liquid and supercooled liquid metals and alloys is demonstrated. 相似文献
89.
New high-temperature copper alloys 总被引:3,自引:0,他引:3
S Constantinescu A Popa J. R. Groza I Bock 《Journal of Materials Engineering and Performance》1996,5(6):695-698
New high-strength, high-temperature Cu-Ni-Si alloys have been developed using additions of Cr, Zr, and/or Ti. These new alloys
remain as precipitation hardenable as the base alloy, but the main strengthening phase may be different than Ni2Si (e.g., Cr2Ti). Substantial increases in mechanical strength were observed at both room and high temperature (773 K) when additions of
Cr+Zr+Ti and Cr+Zr were made. Industrial testing of these alloys indicated a sevenfold increase in the lifetime of lateral
blocks in continuous casting equipment of copper alloys. 相似文献
90.
Cu-Al-Be形状记忆合金的应力腐蚀性能 总被引:2,自引:0,他引:2
用恒载荷法和慢应变速率法及SEM研究了Cu-Al-Be形 状记忆合金在甘油、海水和氨介质中的应力腐蚀性能.结果表明,Cu-Al-Be合金具有良 好的抗海水应力腐蚀性能和较低的氨介质应力腐蚀倾向.单相马氏体有较 好的耐海水腐蚀能力,可减少腐蚀引起的裂纹源;外应力下马氏体的孪晶变形和变体间的界 面迁移,则有利于松弛应力集中,阻碍和延缓腐蚀裂纹源的扩展,从而提高Cu-Al-Be合金的 应力腐蚀能力. 相似文献