CNG发动机火核形成和发展的三维数值模拟研究

本文利用三维燃烧模型对CNG发动机的燃烧过程进行数值模拟,研究过量空气系数的循环变动对CNG发动机火核形成和发展及燃烧各阶段的影响。研究结果显示,过量空气系数的变动对初始火核参数的影响非常小,对燃烧过程三个阶段的影响程度也不同。主燃烧阶段受过量空气系数的变动的影响最大,火核形成和发展阶段受过量空气系数的变动的影响很小。过量空气系数的变动不是火核形成和发展产生变动的主要原因。     

Novel Oxygen Storage Components Promoted Palladium Catalysts for Emission Control in Natural Gas Powered Engines

A three-way catalyst comprised novel oxygen storage components for emission control in natural gas powered engines was prepared. The addition of novel oxygen storage components to the Pd/γ-Al2O3 catalysts resulted in improved activities of the fresh and aged catalyst by lowering the light-off temperature for methane in natural gas engines exhaust.     

从万花筒到组合镜面的成像规律

 万花筒,是许多人都曾经玩过的玩具,那其中复杂却又充满规律性的图影曾让我们浮想联翩。其中有哪些规律呢?这似乎是一个非常有趣的问题。     

动量守恒问题中运动的瞬时性

运用动量守恒定律列方程式，方程式同侧的速度必须要同一时刻的瞬时速度，很多人忽视这一问题，甚至在有些教科书、参考书中也有处理欠妥之处，文中以火箭推进问题，三只小船鱼贯而行问题，论述动量守问题中运动的瞬时性。     

Investigation of sound field for a standing wave tube system with flow and with lateral Helmholtz resonator Ⅰ. Theoretical analysis

A lateral Helmholtz resonator added to a standing wave tube without flow has been validated as a method of noise reduction for combustion noise radiated from combustion channel of rockets or turbines. But in fact there is a flow with low velocity in the combustion channel. Therefore the theoretical analysis carried out is aimed at sound field of standing wave tube with flow and with lateral Helmholtz resonator. Certainly a relevant math-physical model should first be formulated. Here three key problems need to be solved: (1) To formulate the discontinuity condition at the joint between the standing wave tube and Helmholtz resonator in the case of flow. (2) To determine the acoustic impedance of Helmholtz resonator, considering the effects of flow, viscous and multihole. (3) To formulate the reflection condition at the end of the standing wave tube. Some formulas for analysis of the sound field in the tube with flow and with lateral Helmholtz resonator are deduced. These theoretical works have been validated by experiments.     

基于DeltaE的驻波型热声发动机设计方法

在消化和吸收目前普遍接受的热声系统计算软件DeltaE(Design Environment for Low Amplitude Thermoacoustic Engines)的基础上,发展了驻波型热声发动机的结构设计方法;提出引入双参数评估法对发动机性能进行评估,以获取较高的热声转化效率。     

核动力航空推进探析

文献调研国外核动力航空推进相关技术研究,美国GE与PW公司通过ANP计划已试验验证了核动力航空推进的可行性;分析认为核动力航空推进当前最佳用途是长航时无人机与巡航导弹动力,关键技术是核屏蔽的轻量化设计、热交换效率与速率、热力系统设计与新型结构问题;核动力航空推进若采用蒸汽介质的二回路闭式循环驱动螺旋桨,蒸汽透平及动力系统设计没有技术障碍,闭式循环蒸汽流量关键取决于蒸汽透平汽耗率与热交换循环时间。     

新型热声谐振机构的理论分析和实验验证

谐振管作为热声发动机的重要组成部分,其长度占整个系统轴向长度的大部分。本文提出了一种利用液体和弹性膜组成谐振系统的方法,并使用这种谐振系统取代谐振管,使系统轴向尺寸减少为原来的1/5。文中利用线性热声理论对该谐振系统的谐振频率进行了计算,并对不同阻尼系数对系统的耗散做出了分析。实验结果表明,在利用驻波热声发动机驱动的情况下,谐振系统自激起振,谐振频率为360 Hz,实际谐振频率与计算值误差在5%以内。     

超燃冲压发动机性能的准二维计算方法

为了能在双模态超燃冲压发动机流道方案初步论证中提供一种较快速的发动机性能计算方法,在二维N-S方程基础上,引入一维完全燃烧计算方法,提出了预估超燃冲压发动机性能的准二维计算方法。该方法能够计入激波、边界层分离等对发动机性能的影响,可在较短时间计算出整机推力、比冲性能和沿程热力学参数。通过对自由射流发动机计算,验证了此方法。并在此基础上,初步分析了燃料喷注位置和流道构型对发动机性能的影响。 