On the pressure drop modeling of monofilament-woven fabrics

Pressure drop of monofilament-woven fabrics is often calculated via the so-called orifice model in which a discharge coefficient is assigned to the weave's unit cell. In all previous models of woven fabrics, the filaments were assumed to have circular cross-sections—an assumption which is not entirely accurate especially when there is a considerable tension in the warps and wefts. Following the methodology developed by Lu et al. [1996. Fluid flow through basic weaves of monofilament filter cloth. Textile Research Journal 66 (5), 311-323], a new set of expressions are derived for calculating the most constricted open area, and so the discharge coefficient, of plain-woven monofilament fabrics having filaments with elliptical cross-sections. Conducting numerical simulations for computing the pressure drop of such fabrics, we observed a logarithmic relationship between the discharge coefficient and the Reynolds number. It was also shown that the discharge coefficient decreases by increasing the aspect ratio of the filaments’ cross-section.     

Release rates of tetradecen-1-ol acetates from polymeric formulations in relation to temperature and air velocity

An apparatus was developed for investigating the release rates of pheromone formulations at temperatures and air velocities that correspond with those in the field. Polyurethane foam proved an excellent adsorbent for the recovery of tetradecen-1-ol acetates, allowing high air flows at low differential pressure and without breakthrough of these compounds. The experimental setup and procedures are described. The release rates of all formulations investigated were almost proportional to the square root of air velocity, and their logarithms were proportional to the reciprocal of temperature (K). When temperature is increased from 15°C to 25°C, the release rates increase by about 2-2.5 ×. Both relationships were combined into one equation that allows a reliable estimate to be made of the actual release rates of a formulation, under varying conditions, on the basis of its specific parameters and the relevant meteorological data.     

基于现有结构的空压机的改造设计

针对无法完全发挥效能的某厂二手空压机设备 ,结合厂方提出的改造目标 ,提出可在现有总体结构布置的情况下 ,采用通流能力好的三元叶轮、增加流道宽度等措施进行结构改造。经编制热力设计程序进行分析计算 ,结果表明这一方案切实可行     

湿式空气氧化法处理乙烯废碱液装置的技术改造

针对中国石化齐鲁石化公司烯烃厂乙烯装置废碱液处理系统在试运转过程中存在的问题,通过分析原因,提出并实施改进工艺的相关措施,得到一组适宜的工艺操作参数,保证了废碱液湿式空气氧化装置的稳定运行。     

Advancements in the design and validation of an air pollution integrated assessment model for Spain

This paper describes the design and application of the Atmospheric Evaluation and Research Integrated model for Spain (AERIS). Currently, AERIS can provide concentration profiles of NO₂, O₃, SO₂, NH₃, PM, as a response to emission variations of relevant sectors in Spain. Results are calculated using transfer matrices based on an air quality modelling system (AQMS) composed by the WRF (meteorology), SMOKE (emissions) and CMAQ (atmospheric-chemical processes) models. The AERIS outputs were statistically tested against the conventional AQMS and observations, revealing a good agreement in both cases. At the moment, integrated assessment in AERIS focuses only on the link between emissions and concentrations. The quantification of deposition, impacts (health, ecosystems) and costs will be introduced in the future. In conclusion, the main asset of AERIS is its accuracy in predicting air quality outcomes for different scenarios through a simple yet robust modelling framework, avoiding complex programming and long computing times.     

空气气氛中烧成Si3N4-SiC复合材料的性能、相组成和显微结构

以氮化硅细粉(粒度＜0.088 mm,w(β-Si3N4)＞95%)、碳化硅(w(SiC)＞98%,粒度分别为2.8～0.9mm、0.9～0.15 mm、＜0.115 mm和＜0.063 mm四级)、硅粉(粒度＜0.045 mm,w(Si)＞98%)和硅灰(w(SiO2)=98.3%)为原料,以木质素磺酸钙水溶液作成型结合剂,采用150 MPa的压力成型为65 mm×114 mm×230mm的Si3N4-SiC、Si3N4-SiC-Si和Si3N4-SiC-SiO2三种试样.在空气气氛中,以50℃·h-1的升温速度升至800℃保温4 h,再升至1450℃保温2 h,自然冷却至室温后,测定烧成后试样的常温耐压强度、常温抗折强度、1400℃下的高温抗折强度、显气孔率、体积密度和残氮率,并采用XRD、SEM和EPMA等手段分析烧后试样的相组成和显微结构.结果表明3种试样在空气气氛中烧成后的高温(1400℃)和常温抗折强度都比较高,显气孔率都比较低,而耐压强度则以Si3N4-SiC试样的最高;烧成后试样中心区域的残氮率以Si3N4-SiC-Si试样的最高,Si3N4-SiC-SiO2试样的次之,Si3N4-SiC试样的最小;在空气气氛中烧成后,Si3N4-SiC试样中的Si3N4分解较多,SiC-Si3 N4-Si试样的表面和内部都明显含有单质Si,SiC-Si3N4-SiO2试样表面区域的Si2N2O晶体发育很好,而内部区域的晶体发育较小.     

CAE技术在解决胶带座注塑缺陷中的应用

介绍了CAE技术在注塑产品生产中的应用。针对胶带座在注塑成型过程中产生的缺陷，借助CAE软件验证了产生缺陷的位置，找出了产生缺陷的原因。并在工艺、模具和产品设计上进行了修改，从而解决了实际生产中遇到的问题，为实际生产提供了指导。     

Air sampling of volatile sex pheromone components in a closed jar

A cotton wool plug, used as the source for pheromone release, was placed in closed 1-quart Mason jars, either at the mouth or at the rear of the jar. Air sampling of the two components of the sex pheromone (total 2.2 mg at the source) of the almond moth (Ephestia cautella) female showed that the saturation period near the source in still air was 20–22 hr and that far from the source was 40–50 hr, reaching a level of less than 1 ng/ml air. The ratio between the components (Z,E)-9,12-tetradecadienyl acetate, designated D, and (Z)-9-tetradecenyl acetate designated M, in the air was close to the original ratio for both sampling sites, albeit somewhat richer in the more volatile (Z)-9-tetradecenyl acetate (source 77.023.0 DM, air 73.0– 74.327.0–25.7; source 80.119.9, air 77.622.4; source 25.174.9, air 23.976. 1 DM). The total amount of pheromone per milliliter of air was two to three times larger near the source than far from it at the early stages of the evaporation and saturation process. When the amount of pheromone applied to the source was tripled (7 mg), the amount far from the source was almost tripled, or the saturation time was cut by factor of two to three.     

水力旋流器内清水流场空气柱的三维数值模拟

本文依据计算流烙动力学（CFD）的计算方法,利用Fluent软件对带有空气柱的固-液分离用水力旋流器内清水流场进行了三维数值模拟研究。文章中首次采用“mixture”模型对空气柱进行模拟,模拟所得的流场与实测结果作对比,证明效果良好。本文的工作对进一步研究旋流器固-液分离现象提供了一定的基础和参考。     

航空通信数据结构的脆弱点检查模型仿真

对航空通信数据结构进行鲁棒性检测,找到脆弱点对航空安全至关重要.航空通信数据与传统的通信数据不同,包含大量和飞行时产生的随机数据.由于通信数据结构处在不断变化中.传统的数据结构脆弱点检测中,以固定数据结构为前提,没有考虑航空数据结构实时变化造成的的干扰,存在严重的遮蔽效应,降低了航空通信数据结构脆弱点检测方法的准确性.提出了一种依据多维熵值航空通信数据结构的脆弱点检测模型,采用Filter-ary-Sketch及时存储航空通信数据结构信息,间隔一定周期进行基于多维熵值的航空通信数据结构脆弱点检测,若发现异常,按照Filter-ary-Sketch保存的通信数据结构信息定位脆弱点,检测出一个脆弱点,立即进行修正,再进行下一个脆弱点的检测,避免出现遮蔽效应,实现航空通信数据结构脆弱点的准确检测.实验结果说明,对比传统检测模型,所提模型具有较高的检测效率和精度,取得了较好的效果.