板壳式换热器设置膨胀节的判定

介绍板壳式换热器的主要特点和应用。当壳体与板束温差较大时,笔者通过对产品开发的生产实践,提出解决板壳式换热器要否设置膨胀节的类似判定方法。     

不同氧磷比对磷酸盐包边玻璃性质的影响规律

包边技术是提高大尺寸激光玻璃饱和增益系数的关键技术.采用传统的方法熔制玻璃,研究了P2O5含量对P2O5-Al2O3-B2O3-CuCl-Na2O-ZnO磷酸盐包边玻璃的折射率、热膨胀系数、玻璃转变温度、膨胀软化温度以及化学稳定性的影响.结果表明:当P2O5的摩尔分数为60%左右,玻璃样品具有最高的折射率(1.5220)、最低的玻璃转变温度(352.4℃)、较好的化学稳定性[0.52mg/(cm2·d)]和适宜的热膨胀系数(128.427×10-7/℃),是用作钕磷酸盐激光玻璃硬包边的理想材料.     

Synthesis and densification of magnesium aluminate spinel: effect of MgO reactivity

Stoichiometric magnesium aluminate spinel was synthesized by reaction sintering of alumina with caustic and sintered magnesia. The volume expansion of 5–7% during MgAl₂O₄ formation was utilized to identify the starting temperature of spinel formation and densification by high temperature dilatometry. The magnesia reactivity was determined by measurement of crystallite size and specific surface area. Caustic magnesia and sintered magnesia behave differently vis-à-vis phase formation and densification of spinel. Densification of stoichiometric Mag-Al spinel was carried out between 1650 and 1750 °C. Attempts were made to correlate the MgO reactivity with microstructure and densification of spinel.     

蜂窝式构件长细比的计算方法

为了进一步研究蜂窝构件稳定承载性能,以现有长细比计算理论为基础,结合蜂窝构件的受力机理和界面特性,提出了蜂窝构件长细比计算中相关参数的计算方法．同时,结合理论推导和数值分析结果,提出了蜂窝构件换算长细比建议计算公式．     

超临界流体技术制备中药超细粉体

颗粒细、药效好、用量少已成为现代中药制剂的必然发展趋势。利用近年提出的超临界流体辅助雾化过程成功制备出了中药复方肝炎制剂的超细粉体,系统分析了混合器压力和温度及进液速率对微粒形态、粒径和粒径分布的影响。结果表明：利用超临界辅助雾化过程,以水和乙醇的混合溶液为溶剂,可制备出粒径范围为1.0～5.0μm的复方肝炎超细粉体,且大部分粒子形态呈完整的球形。各影响因素对粒径及粒径分布均有不同程度的影响,其中混合器压力及溶液浓度对粒径及粒径分布的影响最明显,进液速率次之,混合器温度的影响较小。在操作范围内较为理想的工艺条件为混合器压力为14 MPa,温度为60℃,进液速率为4.5 mL/min。     

三剪统一屈服准则在柱形孔扩张问题中的应用

基于三剪统一屈服准则,通过用3条折线来描述土体的本构特征,对柱形孔扩张问题进行分析,考虑岩土材料的软化和剪胀特性,推导出柱形孔扩张问题下的应力场、应变场、扩张压力、塑性区半径的解析解。算例表明,临界扩孔压力随土的软化程度的减小而增大,在一定剪胀和软化程度下,临界扩孔压力随b的增大而增大。     

NiCr-ZrO_2复合材料的制备及其热胀性能研究

以ZrOCl2.8H2O和Ni(NO3)2.6H2O,Cr2O3,NH4HCO3为原料,采用缓冲溶液法(一种改进的共沉淀法)制备出复合氢氧化物,将其焙烧得到复合氧化物粉末,最后通过高温还原制备得到NiCr-ZrO2复合粉体材料.通过TG-DSC,XRD,激光粒度仪等现代分析技术对材料的热物性、组成、粒度分布进行测定并研究复合材料热胀系数与其成分组成之间的关系.结果表明,NiCr-ZrO2复合材料的热胀系数随其金属含量的增加而增大.     

Precipitation and stability of reversed austenite in 9Ni steel

A new method was used to analyze the factors affecting the precipitation of reversed austenite during tempering. The samples were kept at various tempering temperatures for 10 min and their length changes were recorded. Then, the precipitation of reversed austenite which led to the length reduction was shown by thermal expansion curves. The results show that the effects of process parameters on the precipitation of reversed austenite can be determined more accurately by this method than by X-ray diffraction...     

Static solution on four-region spherial cavity expansion model in a pressure sensitive medium

Spherical cavity expansion model is often used to study the mechanic characteristics of pressure sensitive mediums. The most important one we do in the paper is that we construct a four-region model with σθ≠0 in damage region,which is different from what Satapathy did before and is more reasonable. By adopting this model,different constitutive equations were constructed by different method-elastic mechanics in elastic region,damage mechanics and fracture mechanics in damage region,and macro-micro mechanics theory in plastic region. Then using Durban's self-similarity assumption,the control differential equations with boundary conditions were established,and the static numerical solution of stress field and displacement field in the three different regions of elastic,damage and plastic area were discussed respectively. Results showed that this four-region model can describe precisely the mechanic characteristics of pressure sensitive mediums under initial pressure.     

Numerical investigation on bowed blades of Iarge meridional expansion Turbine

To improve the performance of the Turbofan engine,several measures should be considered during design process.Such measures,relating to aerodynamic characteristic design,include the maximum enthalpy per stage,the shortest axial length,the minimum blade rows and the highest efficient in design and off design condition.To satisfy theses design characters,the meridian geometry of the engine will he excurvature at a high degree transition part between HP and LP turbines.The study is to investigate the effect of blade bowing on flow loss at blade tip and root of the type of turbine.Such turbine,tending towards separation,with severe secondary flow at the tip and strong radial flow at exit,was simulated by the 3D N-S solver Numerea,and there were several different stacking line bowing schemes in all.The results show that tip negative bowing and root positive bowing is able to weaken radial flow,consequently reduce the flow loss at the tip and root.