薄膜充气管充气展开特性试验

用展开导轨消除因重力产生的摩擦力,在不同充气速率与初始展开角条件下对薄膜材料充气管的充气展开特性进行了试验研究,获得了展开角,以及展开加速度和内气压的变化规律。试验及分析结果表明:充气管的充气膨胀与展开相互独立,充气膨胀过程近似为等压增容过程,折叠部位的气压变化特性与整体气压变化特性差异明显。     

Effect of tube-electrode inner diameter on electrochemical discharge machining of nickel-based superalloy

Nickel-based superalloys are widely employed in modern aircraft engines because of their excellent material characteristics, particularly in the fabrication of film cooling holes. How-ever, the high machining requirement of a large number of film cooling holes can be extremely chal-lenging. The hybrid machining technique of tube electrode high-speed electrochemical discharge drilling (TEHECDD) has been considered as a promising method for the production of film cooling holes. Compared with any single machining process, this hybrid technique requires the removal of more complex machining by-products, including debris produced in the electrical discharge machin-ing process and hydroxide and bubbles generated in the electrochemical machining process. These by-products significantly affect the machining efficiency and surface quality of the machined prod-ucts. In this study, tube electrodes in different inner diameters are designed and fabricated, and the effects of inner diameter on the machining efficiency and surface quality of TEHECDD are inves-tigated. The results show that larger inner diameters could effectively improve the flushing condi-tion and facilitate the removal of machining by-products. Therefore, higher material removal efficiency, surface quality, and electrode wear rate could be achieved by increasing the inner diam-eter of the tube electrode.     

通气模型内流道阻力直接测量技术

推阻特性是吸气式飞行器研制中最为关注的气动特性问题之一.为研究通气模型内流道阻力特性,在中国空气动力研究与发展中心(CARDC)超高速所的1m高超声速风洞上开展了吸气式飞行器通气模型内流道阻力直接测量技术研究.研究选取吸气式飞行器的一个内流道模块为研究对象,通过将内流道模块与模型其余部分进行分离设计、采用特种应变天平直接测量模型内流道气动力的方法得到通气模型内阻,同时进行了干扰因素分析和试验数据修正方法研究,开展了Ma=4条件下的内流道阻力测量试验并给出了典型试验结果.试验结果表明,通气模型内阻随攻角和喉道高度变化而变化.     

弹射座椅弹射筒上连接头挂耳断裂失效分析与研究

本文对弹射座椅弹射筒上连接头挂耳断裂失效现象、安装位置和作用进行了简要介绍;对可能造成上连接头挂耳断裂失效的原材料、尺寸、生产过程、断口、设计及工况强度等主要因素进行了系统排查、分析和验证,最终,找准了零件失效的机理,并准确定位,验证有效,对航空产品提升抗疲劳性能的设计应用起到积极的指导和借鉴意义。     

Space science education in Egypt and the 2006 solar eclipse

The space science research has been started in Egypt since 1910 by measuring the solar constant as indication of solar radiation at Helwan Observatory. The solar sunspot studies and its influence on the Nile flooding was erected and operated at Helwan as a first solar station in Egypt during 1957. Zeiss-Coude’ refractor was installed in 1964. Astronomy and space science educations started in Egypt at the university level since 1936 at Department of Astronomy and Meteorology of Cairo University. Undergraduate and graduate education in Egypt will be discussed in this work.     

耳朵识别身份系统

打击恐怖主义首先要预防恐怖分子,生物识别技术有助于将恐怖分子从人群中识别出来.耳朵是长期保持稳定的一个生物特征,并且耳朵的独特性十分明显.介绍了耳朵识别系统的系统功能和设计思路,采用VC 6.0和SQL SERVER 2000数据库,实现耳朵图像数据采集、图像预处理、图像存储等基本功能.     

Electrochemical micromachining of micro-dimple arrays on cylindrical inner surfaces using a dry-film photoresist

The application of surface textures has been employed to improve the tribological performance of various mechanical components. Various techniques have been used for the application of surface textures such as micro-dimple arrays, but the fabrication of such arrays on cylindrical inner surfaces remains a challenge. In this study, a dry-film photoresist is used as a mask during through-mask electrochemical micromachining to successfully prepare micro-dimple arrays with dimples 94 lm in diameter and 22.7 lm deep on cylindrical inner surfaces, with a machining time of 9 s and an applied voltage of 8 V. The versatility of this method is demonstrated, as are its potential low cost and high efficiency. It is also shown that for a fixed dimple depth, a smaller dimple diameter can be obtained using a combination of lower current density and longer machining time in a passivating sodium nitrate electrolyte.     

捷联惯导系统内杆臂补偿方法及试验验证

在实际捷联惯组中,三只加速度计的比力测量对应于不同的点位置,如果直接作为捷联惯导算法的输入,角运动条件下会引起导航误差。对于加速度计非正交安装情形,在常规静态标定模型基础上,推导了考虑内杆臂效应后的动态标定模型。以导航速度为观测量,建立了加计组合内杆臂补偿的一般模型方程。针对激光捷联惯性组合,设计了简便的试验方法用于辨识内杆臂参数,高强度的摇摆试验表明内杆臂补偿有效地提高了导航精度,速度误差降低达77%以上。       

级间通道构型对双脉冲发动机燃烧室局部受热的影响

为研究级间通道构型对双脉冲发动机一脉冲燃烧室气流再附着点的位置和对流换热系数的影响,本文采用基于格心的迎风型有限体积法数值求解雷诺平均Navier-Stokes方程组,空间离散采用AUSM-PW矢通量分裂格式,时间推进采用3阶三步TVD型Runge-Kutta显式方法,湍流模型采用适合模拟分离流动的改进SST湍流模型,并通过经验公式计算再附着点处的对流换热系数。结果表明:亚声速后台阶流动和固体火箭发动机燃烧室内流动的最大绝对误差分别为8.9%和5.8%;二脉冲工作的不同时刻,当二脉冲装药内孔直径大于级间通道直径时,级间孔直径每增大9.1%,气流再附着点位置平均减小28.2%,对流换热系数平均下降9.6%;其它条件相同时,级间孔宽度增加对气流再附着点位置和对流换热的影响比较小;级间孔角度变大使得气流再附着点的位置和对流换热系数分别平均下降3.4%和3.1%。