From VIB‑to VB‑Group Transition Metal Disulfides:Structure Engineering Modulation for Superior Electromagnetic Wave Absorption

The laminated transition metal disulfides(TMDs),which are well known as typical two-dimensional(2D)semiconductive materials,possess a unique layered structure,leading to their wide-spread applications in various fields,such as catalysis,energy storage,sensing,etc.In recent years,a lot of research work on TMDs based functional materials in the fields of electromagnetic wave absorption(EMA)has been carried out.Therefore,it is of great significance to elaborate the influence of TMDs on EMA in time to speed up the application.In this review,recent advances in the development of electromagnetic wave(EMW)absorbers based on TMDs,ranging from the VIB group to the VB group are summarized.Their compositions,microstructures,electronic properties,and synthesis methods are presented in detail.Particularly,the modulation of structure engineering from the aspects of heterostructures,defects,morphologies and phases are systematically summarized,focusing on optimizing impedance matching and increasing dielectric and magnetic losses in the EMA materials with tunable EMW absorption performance.Milestones as well as the challenges are also identified to guide the design of new TMDs based dielectric EMA materials with high performance.

Computation of the Matching Performance of Diesel Engine with Variable Geometry Turbocharger

To compute the matching performance of diesel engine with variable geometry turboeharger（VGT）, the formerly used program is improved through adjustment of turbine mass flow rate and efficiency characteristics. The calculation result is applied to forecast the performance of J6110Z diesel engine with rotary-vaned VGT70, and to guide the improvement of engine fuel supply. The computed engine performance curve coincides with the experiment result well： the low-speed torque, fuel economy, exhaust temperature and boost pressure of the VGT engine are all improved.

Harmony search optimization applied to reservoir engineering assisted history matching

Based on the analysis of characteristics and advantages of HSO(harmony search optimization) algorithm, HSO was used in reservoir engineering assisted history matching of Kareem reservoir in Amal field in the Gulf of Suez, Egypt. HSO algorithm has the following advantages:(1) The good balance between exploration and exploitation techniques during searching for optimal solutions makes the HSO algorithm robust and efficient.(2) The diversity of generated solutions is more effectively controlled by two components, making it suitable for highly non-linear problems in reservoir engineering history matching.(3) The integration between the three components(harmony memory values, pitch adjusting and randomization) of the HSO helps in finding unbiased solutions.(4) The implementation process of the HSO algorithm is much easier. The HSO algorithm and two other commonly used algorithms(genetic and particle swarm optimization algorithms) were used in three reservoir engineering history match questions of different complex degrees, which are two material balance history matches of different scales and one reservoir history matching. The results were compared, which proves the superiority and validity of HSO. The results of Kareem reservoir history matching show that using the HSO algorithm as the optimization method in the assisted history matching workflow improves the simulation quality and saves solution time significantly.

Component Matching Based on Low Bypass Ratio Mixed Exhaust Turbofan Engine

In order to study component matching which exists in off-design situation at the initial design stage of turbine engine,by establishing performance analysis model of low bypass ratio mixed flow turbofan engine and components characteristic data,and by applying Newton-Raphson method to solve the nonlinear equations of offdesign points in flying envelop,the factors which affect matching between engine components are studied.The results show that low pressure turbine(LPT)must not operate in a critical condition,and the partial derivative(slope)of pressure ratio to similitude mass flow ratio of working point in LPT characteristic map affects the stability of engine.The smaller the slope is,the more stable the engine is.In addition,the engine is more stable when the fan characteristic map is steep.

基于ArcGIS Engine的数字地图逻辑拼接

针对目前GIS系统海量数据分幅存储与管理造成的地理要素在图幅边缘产生的缝隙问题,结合拼接相关理论,提出了一种兼顾空间位置关系和属性特征的拼接方法,并基于ArcGIS Engine 10以及Microsoft Visual Studio 2010的开发环境实现了该方法。实践证明,该方法很好地实现了数字地图的逻辑拼接。

OPTIMIZATION OF ACOUSTIC IMPEDANCE，GEOMETRIC STRUCTURE AND OPERATING CONDITION OF LINERS MOUNTED IN ENGINE DUCT

Acoustically absorptive treatment in aircraft engine nacelle is an essential part of the overall aircraft noise reduction effort. The investigation on the optimization of multi-liners plays an important role in noise reduction. Based upon the mode analysis method of sound propagation in a circular duct with multiple liners, a flexible tolerance method is used to optimize the acoustic parameters(impedance), geometric structure parameters(such as open area ratio, cavity depth and hole diameter) and operating condition parameters(such as blade passing frequency). The mathematical models for these kinds of optimization are presented here. The optimum values of the design variables are determined when the in-duct sound suppression approaches a maximum. It can be derived from the optimum results that the emphasis of the engineering optimization design of the perforated plate honey-comb structure should be placed on the optimum choice of the open area ratio and cavity depth. Some reference criteria for the engineering design of the multi-linings are also provided.

基于ArcGIS Engine的多幅数字地形图接边算法研究

随着社会信息化的发展,作为GIS基础数据的数字地形图在各领域起着越来越重要的作用。但是由于地形图分幅管理的习惯造成地理目标实体被人为分割,所以如何在确保精度的前提下,进行快速、准确、无图幅限制的接边是摆在我们面前的一个课题。本文总结了现有接边算法存在的不足,提出基于单条接边线的缓冲区分析来代替矩形接边线的缓冲区分析,避免地物的重复匹配,充分利用属性约束条件的接边算法。通过减少地物匹配的次数来提高接边的效率,并将其应用于实践,取得了很好的效果。

Analysis and Calibration of Internal Flow Force of EjectorPowered Engine Simulator System in Wind Tunnels

The ejector-powered engine simulator(EPES)system is an important piece of equipment in conducting an influence test of the intake and jet flow in low-speed wind tunnels.In this work,through the analysis of the structure and principle of EPES,three parts of the internal flow force were obtained,namely,the additional resistance before the inlet,the internal flow force in the inlet and the thrust produced by the ejector.On the assumption of one-dimensional isentropic adiabatic flow,the theoretical formulae for calculating the forces were derived according to the measured total pressure,static pressure and total temperature of the internal flow section.Subsequently,a calibration tank was used to calibrate the EPES system.On the basis of the characteristics of the EPES system,the process and method of its calibration were designed in detail,and the model installation interface of the calibration tank was reformed.By applying this method,the repeatability accuracy of the inlet flow rate calibration coefficient was less than0.05%,whereas that of the exhaust flow rate and velocity was less than 0.1%.Upon the application of the calibration coefficients to the correction of the wind tunnel experiment data,the results showed good agreement with the numerical simulation results in terms of regularity and magnitude before stall,which validates the reasonableness and feasibility of the calibration method.Analysis of the calibration data also demonstrated the consistency in the variation law and trend between the theoretical calculation and actual measurement of internal flow force,further reflecting the rationality and feasibility of the theoretical calculation.Nevertheless,the numerical difference was large and further widened with a higher ejection flow rate mainly because of the accuracy of flow measurement and the inhomogeneity of internal flow.The thrust deflection angle of EPES is an important factor in correcting this issue.In particular,the thrust deflection angle becomes larger with small ejection flow and becomes smaller with an increase in flow rate,essentially exhibiting a general change of less than 10°.

Error Searching System with Keyword Extraction and Keyword Fuzzy Matching

This paper has proposed an error searching method to search the solutions of errors that occurred in the unified commanding platform mix-deployed software (UCPMD). Because those errors belong to different stages or may be happened in different services, applications, IP ports, system software, or different versions of software, and those errors are also can be classified into different types. It is necessary to locate accurate reason that cause an error as well as find out its solution. The proposed error searching system applies Chinese keyword extraction and Chinese fuzzy matching between keywords, which considers the processed keywords as the index to find out the solutions of errors. Besides, the error searching system had made correspondence among errors, reasons, and solutions, and put them to different categories in terms of their characteristics, such that it is easy to manage, search, and use. Among others, we have added specialized thesaurus as the index of keywords, which enriches and completes the searching results. Because of the proposed error searching system evolves keyword extraction and keyword fuzzy matching technologies;it is more accurate to find out user-interested solutions.

考虑机组弹性的双层隔振系统刚度匹配方法

为解决柴油发电机组对不同类型和功率发电机的连接套与隔振系统刚度匹配问题,提出以广义弹性力做功为基础的能量解耦法来量化刚度匹配对双层隔振系统固有特性的影响.基于某内燃动力总成双层隔振系统建立3自由度和18自由度动力学模型进行分析.结果表明:3自由度模型能够反映系统耦合的主要特点,机组弹性模态频率与低阶刚体振动模态频率比大于2.96时可以降低刚体振动对弹性模态的影响;考虑惯性耦合和弹性耦合后,18自由度模型对应的频率比应大于4.10才可以显著降低该振动耦合.同一柴油机匹配不同惯性参数的发电机,均可参考小惯性参数发电机隔振设计时对应的频率比和刚度比进行双层隔振系统刚度匹配.

基于樽海鞘群极限学习机的进/发一体化性能寻优控制模型研究

为充分发挥航空推进系统的性能,提高性能寻优控制的实时性,将樽海鞘群算法(SSA)与极限学习机(ELM)相结合,基于进/发一体化部件级模型建立数据集,提出一种基于SSA-ELM的数据驱动模型。将该建模方法与广义回归神经网络(GRNN)、BP神经网络(BPNN)和极限学习机(ELM)比较,结果表明,相比于BPNN,ELM,GRNN,SSA-ELM用于预测可以使安装推力的均方根误差(RMSE)分别降低7.41%,17.01%,72.57%,安装油耗的RMSE分别降低4.32%,19.41%,66.77%,具有更高的预测精度。将基于SSA-ELM的数据驱动模型作为机载模型应用到性能寻优控制,结果表明,该机载模型能够维持理想的寻优效果。针对最大安装推力模式开展实时性分析,该机载模型相比于进/发一体化部件级模型,平均计算时间由184.05 ms缩短至1.357 ms,实时性得到显著改善,大大提高了寻优效率。

基于Zukauskas关系式的预冷发动机进气道流动特性研究

为了研究预冷发动机进气道流动特性,以二维变几何轴对称进气道为研究对象,利用Zukauskas横掠管束绕流关系式,对进气道流场展开了数值仿真研究,探究预冷器的冷却效应及换热管直径对进气道流场、性能的影响。结果表明:Zukauskas关系式能较好地预测气流在预冷器管束间的流动损失;经过预冷后,涡轮通道总温大幅下降,但总温分布不均匀,温度梯度明显,对流换热对上游流体总温产生的影响很小;在Ma_(∞)=2~5飞行工况下,换热功率随着飞行马赫数的增加而增大,涡轮通道的出口总温较预冷前降低了22%~60%,出口马赫数降低了17%~51%,反压比增加了10%~26%,总压恢复系数增加了3%~8%;当预冷器的管径从1 mm增大至2.5 mm时,涡轮通道出口速度降低了16.5%,反压比降低了1%,总压恢复系数呈现先下降后上升的趋势。将虚拟预冷器管束排布方式改为顺排,预冷器的换热功率下降,出口总温上升,涡轮通道的出口速度上升了11%~30%。

基于改进飞蛾扑火优化算法的船机桨匹配设计研究

基于改进飞蛾扑火优化(Improved Moth-Flame Optimization,IMFO)算法,以两艘现有船舶为计算实例,展开了综合考虑螺旋桨推进效率、空泡性能和桨叶强度的船机桨匹配工作。以遗传算法(Genetic Algorithm,GA)和原始飞蛾扑火优化(Moth-Flame Optimization,MFO)算法为对比算法,分析了IMFO辅助船机桨匹配工作时的性能。数值实验的结果表明,在解决船机桨匹配问题时,IMFO算法的收敛时间相比GA算法在两个算例中分别缩短了44.24%和54.14%,相比MFO算法分别缩短了23.9%和23.12%。此外,在求解精度方面,在计算示例1中,IMFO算法相比GA算法和MFO算法略有提升;而在计算示例2中,IMFO算法相比GA算法提高了3.66%,较MFO算法提高了0.98%。最后,通过对两个算例的可行解空间进行可视化表示,进一步讨论了IMFO算法的求解性能。上述结果对比证明了IMFO算法具备强大的全局搜索能力,在解决船机桨匹配问题时具有良好的竞争力和鲁棒性。

铁路工程接口工序工期匹配研究

铁路工程项目涉及参与方众多,专业交叉深入,形成大量工程接口,因此参与方协调配合,接口界面平顺衔接是保证铁路工程项目顺利完成的关键,而确保铁路工程接口工序工期匹配便是解决铁路工程接口匹配问题的基础。考虑影响接口交换时间各因素的相互作用,结合Shapley值法进行仿真模拟,建立接口工序工期预测模型。在此基础上,提出3种基本的接口工序工期匹配手段,结合任务要求的接口匹配状态形成13种接口工序工期匹配方式。根据工程实际情况选择相应的匹配方式调整接口工序工期,能够使接口上、下游双方实时获取接口信息,避免由于工期不匹配导致的返工和重复做工等问题,最终实现节约资源,提升铁路工程质量。

二元超声速混压式进气道亚临界稳定裕度研究

为了研究内收缩比和来流马赫数对二元超声速混压式进气道亚临界稳定裕度的影响规律及失稳机制,采用二维非定常仿真方法研究了内收缩比(ICR)为1.04~1.25的进气道在来流马赫数Ma0为2.4的条件下,以及内收缩比为1.08的进气道在来流马赫数为2.2~2.8条件下,其由稳态向失稳状态转变的过程。研究结果表明:(1)当Ma0=2.4时,在1.04≤ICR≤1.12内,随着ICR增加,亚临界稳定裕度ζ减小;1.16≤ICR≤1.25内,随着ICR增加,亚临界稳定裕度增大。(2)在内收缩比为1.08的条件下,马赫数变化引起的分离激波角和分离包再附压升两个关键因素变化共同主宰着进气道亚临界稳定裕度的变化趋势。(3)总体上,根据稳定亚临界初始状态的三相点无量纲高度?b是否大于1可将进气道的亚临界稳定裕度变化情形分为两类,当?b<1时,ζ随着?b的增加而减小;当?b> 1时,ζ随着?b的增加而增加。

重型柴油机二级增压系统匹配仿真研究

为了降低重型柴油机的燃油消耗率,采用GT-POWER软件建立仿真模型,在一台单级可变截面涡轮增压器(variable geometry turbocharger,VGT)柴油机上开展了二级增压匹配与增压系统参数优化工作。仿真结果表明,所提出的二级增压系统在匹配点能够以最高效率运行,在全工况都能提供足够的进气流量;完全关闭低压级废气旁通阀,正交优化高压级废气旁通阀开度和米勒循环度,能够进一步降低二级增压发动机的燃油消耗率;降低级间中冷温度能够降低泵气损失,提高增压压力,温度由100℃降至50℃在标定点能够使燃油消耗率降低约3 g/(kW·h)。对二级增压及参数优化工作的燃油消耗率改善效果进行了试验验证,低速工况燃油消耗率整体有所下降,高效点燃油消耗率下降4.1%。

航空发动机进口帽罩结/防冰特性试验研究

航空发动机进口帽罩作为发动机重要的进口部件,防冰能力关乎发动机性能甚至影响飞行安全。为了研究航空发动机进口帽罩防冰性能,通过冰风洞对进口帽罩进行结/防冰试验,得到了进口帽罩表面结冰状况随热气流量、来流温度、来流风速的影响规律。试验结果表明:进口帽罩防冰能力从尖锥头部到帽罩后端逐渐增强;帽罩防冰能力随热气流量增加而提升;帽罩表面冰型随来流温度、来流风速变化而发生改变;帽罩表面结冰区域随风速增加而扩大。研究成果可以为进口帽罩防冰系统设计和验证提供重要指导。

医疗陪诊服务管理系统的设计与实现

随着社会老龄化进程的加快和信息化技术的发展,医疗陪诊服务的需求也越来越大。为了让就医者在医院看病时能够得到更好的服务和帮助,提高医疗服务的质量和效率,特设计一种医疗陪诊服务管理系统。该系统中专业的陪诊员可以代替患者家属完成预约挂号、排队、问诊、取药等事宜,有效节省患者的就医时间,提升患者的就医体验。同时该系统的陪诊人员还可以成为患者和医生之间的沟通桥梁,增进医患信任,提高患者就医的舒适性和便利性。

航空发动机风扇机匣声衬与进气道声衬联合设计方法

对于现代的大涵道比涡扇发动机,风扇噪声是主要的噪声源。风扇机匣声衬(风扇前)与进气道声衬能显著降低风扇前传噪声。该两段声衬距离接近,所处的声场互相影响,有必要研究风扇机匣声衬(风扇前)与进气道声衬的联合设计方法。首先结合国内外进展,对声衬优化设计方法、声传播计算模型、声源模型、声阻抗模型、代价函数等声衬设计的关键环节进行讨论,并选择合适的方法形成一套完备的声衬设计体系与设计工具。同时,对航空发动机风扇机匣声衬(风扇前)与进气道声衬进行联合设计,得到单自由度与双自由度声衬两套方案,证明该工具的工程可行性与有效性。最后,对两种声衬方案进行了不同方面的评估,包括叶片通过频率(blade passing frequency,BPF)噪声降噪效果、宽频降噪效果等。评估表明,在该设计思路下,两方案在飞越、边线、进场前两阶BPF噪声都能得到很好的降噪效果,并且双自由度声衬能够在更宽的频率范围内显示出降噪优势。但是,如果代价函数能够进一步囊括声衬的宽频吸声效果,双自由度声衬能够具有更优的宽频降噪效果。