气动非谐对叶片非定常气动激振力影响

为降低转子叶片在前排静子叶片尾流激振情况下的共振应力, 提高转子叶片疲劳寿命, 对静子叶片的气动非谐设计进行研究.对静子叶片的气动非谐设计考虑了两种方案, 一种为非均匀叶栅设计, 另一种为不对称叶栅设计.通过对静子-转子模型流场进行非定常计算, 比较了两种非谐设计思想下转子叶片表面气动激振力频谱成分和幅值大小.分析结果标明:非均匀叶栅非谐设计并不能降低转子叶片表面激振力, 同时会引起频率成分和幅值都较大的倍频成分;不对称叶栅非谐设计虽然会引起与转速同频的较大幅值激振力成分, 但从整体考虑可有效降低叶片振动应力.      

Temporal evolution of the EIA along 95°E as obtained from GNSS TEC measurements and SAMI3 model

The total electron content (TEC) derived from GNSS measurements at a trans-hemispheric meridional chain of ground stations around 95°E longitude are used to study the quiet time inter-hemispheric structure and dynamics of the equatorial ionization anomaly (EIA) during the period March 2015 to February 2016. The stations are Dibrugarh (27.5°N, 95°E, 43° dip), Kohima (25.6°N, 94.1°E, 39° dip), Aizawl (23.7°N, 92.8°E, 36° dip), Port Blair (11.63°N, 92.71°E, 9° dip) and Cocos Islands (12.2°S, 96.8°E, 43° dip). The observation shows that the northern crest of the EIA lies in the south of 23°N (Aizawl) in all seasons but recedes further south towards the equator during December solstice. The largest poleward expansion of the northern (southern) EIA is observed in the March equinox (December solstice). The equinoctial and hemispherical asymmetry of TEC is noted. The winter anomaly is observed in the northern hemisphere but not in the southern hemisphere. The highest midday TEC over any station is observed in the March equinox. The TEC in southern summer (December solstice) is significantly higher than that in the northern summer (June solstice). The observed northern EIA contracts equatorward in the postsunset period of solstice but the southern EIA persists late into the midnight in the December solstice. The asymmetry may be attributed to the different geographic location of the magnetically conjugate stations. The SAMI3 simulations broadly capture the EIA structure and the inter-hemispheric asymmetry during solstices. The difference between observations and the SAMI3 is higher in March equinox and December solstice. The higher E?×?B vertical drift in the 90–100°E sector and the large geographic-geomagnetic offset in observing stations may have contributed to the observed differences.     

具有不对称间隙的二元机翼自激振动的混沌分析

利用数值方法分析了无预荷载情况下具有不对称间隙的气动弹性非线性与结构非线性耦合的二元机翼颤振问题的动力学响应.通过研究速度比U*/U*L从零逐渐增大到1时系统的全局演化规律,发现在无预荷载的不对称分段线性系统中存在混沌运动形式,并对其进行具体分析,得到产生混沌的原因,为进一步控制和减小颤振提供理论帮助,对飞机的飞行结构设计及飞机结构的日常维护具有指导意义.     

The impact of spherical symmetry assumption on radio occultation data inversion in the ionosphere: An assessment study

‘Onion-peeling’ is a very common technique used to invert Radio Occultation (RO) data in the ionosphere. Because of the implicit assumption of spherical symmetry for the electron density (N(e)) distribution in the ionosphere, the standard Onion-peeling algorithm could give erroneous concentration values in the retrieved electron density profile. In particular, this happens when strong horizontal ionospheric electron density gradients are present, like for example in the Equatorial Ionization Anomaly (EIA) region during high solar activity periods. In this work, using simulated RO Total Electron Content (TEC) data computed by means of the NeQuick2 ionospheric electron density model and ideal RO geometries, we tried to formulate and evaluate an asymmetry level index for quasi-horizontal TEC observations. The asymmetry index is based on the electron density variation that a signal may experience along its path (satellite to satellite link) in a RO event and is strictly dependent on the occultation geometry (e.g. azimuth of the occultation plane). A very good correlation has been found between the asymmetry index and errors related to the inversion products, in particular those concerning the peak electron density NmF2 estimate and the Vertical TEC (VTEC) evaluation.     

单通道控制的旋转弹锥形运动稳定性研究

锥形运动是旋转弹角运动的基本形式,其稳定性问题一直是旋转弹领域的研究热点。以一对鸭舵作用下的单通道控制旋转弹为研究对象,给出了弹体坐标系下的线性化角运动模型,通过数值仿真,揭示了一对鸭舵带来的气动不对称对其角运动特性的影响规律。利用劳斯判据,给出了解析形式的锥形运动稳定条件,该条件可等效为锥形运动稳定条件下的转速范围,不同转速下的仿真结果证明了该稳定条件的正确性。在相同的转速条件下,正弦式鸭舵的控制频率在慢模态衰减频率附近时,可诱发强烈的共振不稳定。研究结果可为一对鸭舵作用下的旋转弹总体设计及制导控制系统设计提供参考。     

基于磁极电流分配的电磁轴承控制器设计

 电磁轴承是机、电、磁一体化的复杂系统, 针对不对称、强耦合电磁轴承结构, 提出基于磁极电流分配的电磁轴承控制器设计。该方法将原来控制器分为反馈控制器和电流分配器两部分, 以简化控制器设计。主要讨论了轴承磁极电流分配器设计, 并应用于圆锥电磁轴承系统中, 设计它的磁极电流分配器。     

Some features of disturbed rotational motion of a satellite with a strong onboard magnet

A disturbed rotational orbital motion of an asymmetrical satellite with a strong magnet in the geomagnetic field is considered. It is shown that operating disturbances result in appearing of non-resonant phenomena in the satellite rotation caused by resonance effects.     

多相开路故障下的双三相PMSM统一容错控制策略

多相电机在定子开路故障下具有良好的容错性能,与此相关的设备和控制策略改进方面的研究理论也不断被提出。然而,却少有基于统一模型的适用于多相开路故障的容错控制策略。提出了一种应用于双三相永磁同步电机(PMSM)系统三相或三相以下开路故障的容错控制策略,并获得了良好的电机电力和动态性能。针对发生单相到三相开路故障的PMSM提出了统一数学模型,提取出每种故障下对应电机不对称性的矩阵。通过电压方程,推导出每种故障对应的解耦变换矩阵。为了对相电流中的每种谐波进行无差别抑制,建立了谐波子空间。考虑开路故障相数的增加,提出了用于三相开路的有中性点电流的容错控制策略,达到了降低相电流幅值和提升系统冗余度的目的。最后通过试验和仿真结果,验证了理论分析的正确性。     

A300-600飞机前缘缝翼故障排除

介绍了A300—600飞机前缘缝翼系统的工作原理,对于航线维护中出现的典型故障进行了详细的分析,简述了故障的排除方法,给出了提高该系统可靠性的维护建议。     

三维试验粒子轨道法在磁层粒子全球输运中的应用

根据磁层粒子动力学理论, 通过偶极磁场模型验证利用三维试验粒子轨道方法模拟近地球区(r < 8R_e)带电粒子运动特征的可靠性. 在此基础上, 以太阳风和磁层相互作用的全球MHD模拟结果为背景, 利用三维试验粒子轨道方法, 对非磁暴期间南向行星际磁场背景下太阳风离子注入磁层的情形进行数值模拟, 并对北向行星际磁场背景下太阳风离子注入极尖区以及内磁层的几种不同情形进行了单粒子模拟. 模拟结果反映了南向和北向行星际磁场离子向磁层的几种典型输入过程, 揭示出行星际磁场南向时太阳风粒子在磁层内密度分布的晨昏不对称性以及其在磁鞘和磁层内的大致分布, 并得出统计规律. 模拟结果与理论预测和观测结论相一致, 且通过数值模拟发现, 行星际磁场北向时靠近极尖区附近形成的非典型磁镜结构对于能量粒子经由极尖区注入环电流区域过程有重要的影响和作用.