直升机飞行控制三维动画仿真平台设计与实现

为了更好地分析和设计直升机飞行控制系统,开发了直升机飞行控制三维动画仿真平台.该平台适用于采用内外回路方法设计的飞行控制系统,可以载入和显示各种控制器、直升机模型,并用数字、曲线和三维动画显示仿真结果.本仿真平台利用Visual C++6.0编写软件主界面,MATLAB引擎提供后台计算服务,Direct3D实现实时动画显示,实现了三者接口平滑、无缝的互连.以UH-60A黑鹰直升机飞行控制系统的设计仿真为例,验证了此仿真平台的可行性.     

低温等离子体汽油重整对稀燃极限影响的实验

为提高稀薄燃烧汽油机的稀燃极限,提出了一种借助低温等离子体,利用稀薄燃烧发动机排气中的氧气和水蒸气对燃油进行重整,以制得富氢的混合气体辅助发动机进行稀薄燃烧的方法．设计了一套等离子体排气重整系统,并对其进行了排气重整性能的研究．在一台稀燃发动机上进行了低温等离子体燃油重整对稀薄燃烧极限影响的实验,实验结果表明：利用等离子体排气重整系统,能够进一步扩大发动机的稀燃极限;重整比例每增大10％,发动机燃烧极限增大约1～2个空燃比单位．     

Influence of contaminations on combustion kinetics in hydrogen-fueled engine

In this work, we investigate the combustion of hydrogen fuel through the wind tunnel tests. Two kinds of fuel, the pure hydrogen and the hydrogen-ethene mixture, have been chosen to heat the oxygen-enriched air. It is found that the stable pressure in the engine combustor and the thrusts is almost the same in two cases. A valuable feature we revealed is that the heating pattern of hydrogen and ethene mixture leads to a considerable delay of the establishment of the wall pressure in the combustor, compared with the pure hydrogen case. This phenomenon implies a longer ignition delay time for the mixture case. The shorter ignition delay resulting from the hydrogen heater is attributed to the continuity of chain propagation and the exclusion of the less active C-containing radicals.     

边界参数对HCCI发动机燃烧影响的模拟研究

为了研究边界参数对柴油均质压燃(HCCI)发动机燃烧过程的影响,应用CHEMKIN化学动力学软件包中的SENKIN程序以及正庚烷(n-heptane)氧化反应简化模型,模拟了不同进气温度、进气压力和当量比等边界参数对HCCI发动机燃烧及排放特性的影响.结果表明,在相同当量比条件下,增压可以拓宽HCCI发动机负荷工况范围,同时保持氮氧化物排放基本不变;过浓或过稀的混合气导致CO排放增加;混合气浓度分层增加NO排放.     

Two-port network model and startup criteria for thermoacoustic oscillators

The startup process of a thermoacoustic engine is a self-excited oscillation process generated in inhomogeneous acoustic media. To reveal these coupling relations between various influential factors is an important task of basic research on thermoacoustics. In this paper thermoacoustic engines are regarded as thermoacoustic oscillators consisting of the active network and the passive network. Accordingly, the two-port Y-parameter for relevant component is derived, and standing wave and traveling wave thermoacoustic engine are described by the negative-resistance and feedback model, respectively. The relevant two-port network topology is given as well. The startup criteria for thermoacoustic oscillators are obtained by using Nyquist instability criterion. The model prediction of startup parameters, particularly, startup frequency and mode characteristic are in agreement with that of experimental results reported in the literature. Moreover, with topological graphs it is verified that standing wave engines would start up in a negative-resistance state and there would exist high frequency modes in thermoacoustic-Stirling engines. By investigating into the frequency response of thermoacoustic system, this method proposed can achieve such an objective that these effects of operating and structural parameters of engine on startup modes and startup temperature can be revealed in an analytical way. Thus this approach to test and check thermal stability can be provided in a design phase, instead of using empirical frequency to design thermoacoustic systems. Electronic Supplementary Material  Supplementary material is available for this article at and is accessible for authorized users. Supported by National Natural Science Foundation of China (Grant Nos. 50576024 and 51076013)     

用于哼唱识别精确匹配的线性伸缩动态规划算法

提出一种用于哼唱识别精确匹配的线性伸缩动态规划算法。该算法将哼唱旋律切割成句子,对每一句子进行线性伸缩匹配,同时在句子层次进行动态规划获得最优路径。该算法更有效地利用了哼唱语音的分段特性并克服了动态规划在长路径搜索时可能丢失全局最优路径的缺点。在含5 223首M ID I的数据库上同等条件下该算法正确率分别比线性伸缩、动态规划及递归匹配方法提高10.5%、6.0%和2.8%。该算法具有更高的准确率和更小的时间复杂度,是一种更有效的精确匹配算法。     

汽油机排放控制技术的研究

分析了汽油机排放物的构成、对人体的危害及其形成机理,探讨了各种减少排放污染的有效措施。     

基于Web智能的网络广告监测器研究与设计

为了解决网络广告投放效果监测困难的问题,基于网络广告的搜索引擎和网络爬虫等Web智能技术,设计了一种独立的、第三方的网络广告监测器,描述了当前网络广告的发展现状、系统的结构模块设计、时序调度设计以及相应的系统实现方案和核心算法。通过实验评测表明,该系统能够取得较好的效果。     

简谐力矩作用柴油机轴系的主共振

应用拉格朗日方程,得到了柴油机轴系的非线性振动微分方程,根据非线性振动的多尺度解法,求得系统满足主共振情况的一次近似解,并对其进行数值计算,绘制系统相图、时间响应曲线,分析外激力、谐调值等对系统的影响.     

斯特林发动机燃油系统压力波动仿真

为研究斯特林发动机燃油系统的动态特性,以压力波动幅值为控制目标,建立了燃油系统的仿真模型,综合分析了高压油泵柱塞直径、蓄压器容积和长径比、蓄压腔出油口位置对压力波动幅值的影响,优化设计系统参数,并依此试验,取得良好的稳压效果。该仿真系统能够反映斯特林发动机燃油系统的实际工作过程,参数优化后的系统能够减小蓄压腔中燃油压力的波动。