智能充放电设备给航空锌银蓄电池充电的故障分析

针对智能充放电设备给航空锌银蓄电池充电时出现电压过高,致使充电意外提前结束的情况,分析了充电设备的充电方法与航空锌银蓄电池的一些特有特性,并提出了充电时的注意事项与操作方法。     

平流层螺旋桨多工况等离子体增效控制方案研究

基于S1223翼型建立了平流层螺旋桨3维模型,在螺旋桨上下表面设置等离子体激励器,设计了5种螺旋桨工况下的等离子体控制方案,采用唯象学等离子体体积力模型进行数值仿真,研究了5种工况下不同等离子体控制方案对螺旋桨拉力和效率的影响。结果表明,设计工况下不宜开启等离子体激励器,采用交流激励时等离子体对高转速前进工况下的螺旋桨控制效果不明显,低速重载工况和滑翔工况下螺旋桨拉力和效率增加,低转速抗风工况下螺旋桨拉力大。采用等离子体流动控制技术提高平流层螺旋桨性能是可行的,需要进一步开展大量研究以优化等离子体激励器的布置方案和控制方案,提高等离子体控制效果,以满足低速临近空间飞行器对推进系统的需求。     

应用等离子体抑制空腔噪声数值仿真研究

空腔在自由来流下将产生强烈的气动噪声,这种噪声会对飞机产生负面作用,需要寻求噪声控制方法抑制空腔噪声。等离子体是一门新兴的流动控制技术,可应用在噪声抑制方面。通过在空腔前缘、后缘以及底面10个不同的位置布置等离子体激励器,研究了等离子体激励对空腔噪声的影响。结果表明：等离子体激励可以降低空腔噪声,声压级最高降低约4 dB;降低了空腔离散噪声的峰值频率;在空腔前缘壁面施加等离子体激励,噪声抑制效果最好。     

Statistical study of electrostatic solitary waves associated with reconnection: Geotail observations

The role of waves in the dynamics of the magnetotail has long been a topic of interest in magnetospheric physics. The characteristics of Electrostatic Solitary Waves (ESWs) associated with reconnection have been studied statistically in the magnetotail by surveying the large amounts data obtained from Waveform Capture (WFC) which is an important component of Plasma Wave Instrument (PWI) on the Geotail spacecraft. About 150 reconnection events with WFC data available are selected, and approximately 10 thousands of ESW waveforms are picked up by hands for statistical study. The ESWs are observed near diffusion region and near the plasma sheet boundary layer (PSBL). Two kinds of waveforms of ESWs are observed: bi-polar and tri-polar pulses. It is found that the pulse width of the ESWs is in the order of 1–5 ms and the peak-to-peak amplitude is in the order of 0.1–5 mV/m. The amplitudes of ESWs are larger in the near-earth tail region than that in deep tail region. ESWs have been observed with or without guide magnetic field 〈By〉. The characteristics of ESWs in different reconnection region and under different strength of guild magnetic field, their possible generation mechanism will be discussed.     

弯曲壁上开孔倾角对气膜孔流量系数的影响

对弯曲壁上的多孔气膜冷却方式的流量系数进行了实验研究, 目的是确定在一定曲率的弯曲壁上不同开孔倾角冷却孔的平均流量系数随压力参数的变化规律, 并从流动损失方面进行深入分析.研究结果表明, 对于几何参数一定的多孔冷却方式, 影响其流量系数的气动因素用压力参数来表示是合理的, 但对于不同的开孔倾角, 压力参数对流量系数的影响效果有很大差别.      

二维静电孤立波的粒子模拟研究

利用二维粒子模拟程序研究了双流不稳定性激发静电波并演化为静电孤立波的物理过程.计算结果表明,在线性增长阶段,主要激发的是沿磁场传播的静电波;在非线性演化阶段,相邻的静电波会互相合并,直至形成静电孤立波,并可激发静电哨声波.还研究了磁场强度和离子温度对此过程的影响.当磁场强度比较小时,无法形成静电孤立波,只有磁场强度达到一定程度后静电孤立波才能形成;同时,离子温度会影响静电孤立波的稳定性,当离子温度比较小时,静电孤立波的稳定性减弱,在演化一段时间后会逐渐瓦解.      

Experimental study of rotating gliding arc discharge plasma-assisted combustion in an aero-engine combustion chamber

The combustion chamber is the core component of an aero-engine, and affects its reliability and security operation, even the performance of the aircraft. In this work, a Plasma-Assisted Combustion(PAC) test platform was developed to validate the feasibility of using PAC actuators to enhance annular combustor performance. Two plans of PAC(rotating gliding arc discharge plasma) were designed, Assisted Combustion from Primary Holes(ACPH) and Assisted Combustion from Dilution Holes(ACDH). Comparative experiments and analysis between conventional combustion and PAC were conducted to study the effects of ACPH and ACDH on the performances including average outlet temperature, combustion efficiency, pattern factor under four different excessive air coefficients(0.8, 1, 2, and 4), and lean blowout performance at different inlet airflow velocities. Experimental results show that the combustion efficiency is improved after PAC compared with that in normal conditions, and the combustion efficiency of ACPH increases2.45%, 1.49%, 1.04%, and 0.47%, while it increases 2.75%, 1.67%, 1.36%, and 0.36% under ACDH conditions. The uniformity of the outlet temperature field and the lean blowout performance are improved after PAC. Especially for ACPH, the widening of the lean blowout limit is8.3%, 12.4%, 12.8%, and 25% respectively when the inlet velocity ranges from 60 m/s to120 m/s. These results offer new perspectives for using PAC devices to enhance aero-engine combustors' performances.     

半封闭肋化通道射流冲击的实验

运用红外热像测试技术对半封闭肋化通道单排孔射流冲击进行了热像显示实验,揭示出射流雷诺数、冲击间距、肋型排布方式对传热特性的影响规律,并开展了冲击孔流量系数的研究.结果表明:在本文研究范围内,冲击间距与孔径比Zn/d=1时壁面射流区换热效果最好;V型肋化通道在壁面射流区获得了最佳换热效果;冲击孔流量系数随雷诺数增加而变大;在其它工况相同的情况下,V型顺流肋化通道内冲击孔流量系数最大.      

SMILE卫星低能离子分析仪的设计与仿真

针对SMILE卫星的大通量动态范围、大视场范围（FOV）、高分辨率等离子体探测需求，以带顶盖半球形静电分析器为基础设计了低能离子分析仪（LIA）。仪器利用顶盖电压控制方式实现可变几何因子，通过高聚焦特性离子光学系统和视场偏转系统设计实现高分辨和大视场探测。利用SIMION有限元仿真软件对仪器的性能参数和几何因子变化规律进行研究，并优化了离子光学系统设计。通过仿真可以获得仪器的主要技术指标参数：能量范围0.05 keV~20 keV，能量分辨率0.0791，方位角视场360°，俯仰角视场范围可达±45°。     

BGA 封装NC 管脚对ESD 测试的影响

焊球阵列封装电路已广泛应用在航空电子产品中，其静电放电测试参考的测试标准中不要求对未键 合空脚进行静电放电测试，在实际静电放电测试过程中发现，对焊球阵列封装电路未键合未键合空脚进行静电 放电测试后会产生电路失效现象。通过分布电容方法分析以及不同管脚组合测试验证，证明了焊球阵列封装电 路的未键合空脚在经过人体模型静电放电测试后，会对电路产生影响。