涡轮盘多轴低循环疲劳寿命预测及试验验证

应用单轴及多轴疲劳寿命预测的Von Mises等效应变模型和临界平面模型对某两级涡轮盘传动臂销钉孔的疲劳寿命进行预测.组装和调试了全尺寸两级涡轮盘联合试验件,在旋转试验器上完成了低循环疲劳试验,得到两级涡轮盘传动臂销钉孔试验失效寿命.预测寿命与试验寿命对比分析显示单轴和Von Mises等效应变模型预测误差较大;临界平面模型误差较小,尤其是拉伸型失效SWT(Smith-Watson-Topper)模型误差为9.26%.      

高速压气机涡轮转子结构轴系非线性 振动性能试验

基于气动轴承与轴系耦合调频技术,对高速压气机涡轮转子结构的空气循环制冷机轴系进行非线性振动性能的试验研究,进一步分析了柔性轴系存在转子运动、轴承失稳及碰摩故障的一些非线性特征.研究结果表明:在保证转速设计裕度的前提下,工作转速由40000r/m提高到了60000r/m.      

Impact of rogue active regions on hemispheric asymmetry

The solar dipole moment at activity minimum is a good predictor of the strength of the subsequent solar cycle. Through a systematic analysis using a state-of-the-art $2\times 2$D solar dynamo model, we found that bipolar magnetic regions (BMR) with atypical characteristics can modify the strength of the next cycle via their impact on the buildup of the dipole moment as a sunspot cycle unfolds. In addition to summarizing these results, we present further effects of such “rogue” BMRs. These have the ability to generate hemispheric asymmetry in the subsequent sunspot cycle, since they modify the polar cap flux asymmetry of the ongoing cycle. We found strong correlation between the polar cap flux asymmetry of cycle i and the total pseudo sunspot number asymmetry of cycle $i+1$. Good correlation also appears in the case of the time lag of the hemispheres of cycle $i+1$.     

Characterization of GPS-TEC over African equatorial ionization anomaly (EIA) region during 2009–2016

This study characterizes total electron content (TEC) measured by Global Positioning System (GPS) over African equatorial ionization anomaly (EIA) region for 2009–2016 period during both quiet geomagnetic conditions (Kp?≤?1) and normal conditions (1?>?Kp?≤?4). GPS-TEC data from four equatorial/low-latitude stations, namely, Addis Ababa (ADIS: 9.04°N, 38.77°E, mag. lat: 0.2°N) [Ethiopia]; Yamoussoukro (YKRO: 6.87°N, 5.24°W, mag. lat: 2.6°S) [Ivory Coast]; Malindi (MAL2; 3.00°S, 40.19°E, mag. lat: 12.4°S) [Kenya] and Libreville (NKLG; 0.35°N, 9.67°W, mag. lat: 13.5°S) [Gabon] were used for this study. Interesting features like noontime TEC bite-out, winter anomaly during the ascending and maximum phases of solar cycle 24, diurnal and seasonal variations with solar activity have been observed and investigated in this study. The day-to-day variations exhibited ionospheric TEC asymmetry on an annual scale. TEC observed at equatorial stations (EIA-trough) and EIA-crest reach maximum values between ～1300–1600 LT and ～1300–1600 LT, respectively. About 76% of the high TEC values were recorded in equinoctial months while the June solstice predominantly exhibited low TEC values. Yearly, the estimated TEC values increases or decreases with solar activity, with 2014 having the highest TEC value. Solar activity dependence of TEC within the EIA zone reveals that both F10.7?cm index and EUV flux (24–36?nm) gives a stronger correlation with TEC than Sunspot Number (SSN). A slightly higher degree of dependence is on EUV flux with the mean highest correlation coefficient (R) value of 0.70, 0.83, 0.82 and 0.88 for quiet geomagnetic conditions (Kp?≤?1) at stations ADIS, MAL2, NKLG, and YKRO, respectively. The correlation results for the entire period consequently reveals that SSN and solar flux F10.7?cm index might not be an ideal index as a proxy for EUV flux as well as to measure the variability of TEC strength within the EIA zone. The estimated TEC along the EIA crest (MAL2 and NKLG) exhibited double-hump maximum, as well as post-sunset peaks (night time enhancement of TEC) between ～2100 and 2300 LT. EIA formation was prominent during evening/post-noon hours.     

The characteristics of valley phase as predictor of the forthcoming solar cycle

Is Solar Cycle 24 anomalous? How do we predict the main features of a forthcoming cycle? In order to reply such questions, this work partitions quantitatively each cycle into valley, ascend, peak, and descend phases, statistically investigate the correlations between valley phase and the forthcoming cycle. We find that the preceding valley phase may dominate and can be predictor of the forthcoming cycle: (1) The growth rate in ascend phase strongly negatively correlates to valley length and strongly positively correlates to cycle maximum. (2) The cycle maximum strongly negatively correlates to valley length, and strongly positively correlates to cycle minimum. (3) The cycle period strongly negatively correlates to the valley variation. Based on these correlations, we conclude that the solar cycle 24 is a relatively weak and long cycle which is obviously weaker than Cycle 23. The similarity analysis also presents the similar result. The Cycle 25 is also inferred possibly to be a weak cycle. These results can help us understanding the physical processes of solar cycles.     

修正的阿伦方差对调相闪烁噪声的抑制

在时频领域内,普遍采用阿伦方差来表征频率稳定度,但阿伦方差对于调相闪烁噪声的抑制能力有其本身算法的缺陷。提出了用修正阿伦方差来表征频率稳定度,以降低噪声对频率稳定度的影响。分析并研究了修正的阿伦方差对调相闪烁噪声的抑制机理。通过卫星共视时间比对试验,对氢原子钟与原子时标国家计量基准的比对数据进行评估,利用噪声模型对评估结果进行论证。验证了修正阿伦方差对于调相闪烁噪声抑制的有效性。     

Inverse free steering law for small satellite attitude control and power tracking with VSCMGs

Recent developments in integrated power and attitude control systems (IPACSs) for small satellite, has opened a new dimension to more complex and demanding space missions. This paper presents a new inverse free steering approach for integrated power and attitude control systems using variable-speed single gimbal control moment gyroscope. The proposed inverse free steering law computes the VSCMG steering commands (gimbal rates and wheel accelerations) such that error signal (difference in command and output) in feedback loop is driven to zero. H_∞ norm optimization approach is employed to synthesize the static matrix elements of steering law for a static state of VSCMG. Later these matrix elements are suitably made dynamic in order for the adaptation. In order to improve the performance of proposed steering law while passing through a singular state of CMG cluster (no torque output), the matrix element of steering law is suitably modified. Therefore, this steering law is capable of escaping internal singularities and using the full momentum capacity of CMG cluster. Finally, two numerical examples for a satellite in a low earth orbit are simulated to test the proposed steering law.     

RBCC-RKT两级入轨飞行器飞行轨迹优化方法

针对火箭基组合循环（RBCC）发动机比冲和推进剂质量流量随飞行条件改变而不断变化的特点,提出了通过增广拉格朗日遗传算法优化飞行器飞行轨迹的方法,在飞行器气动参数和发动机比冲已知、最大飞行动压给定等条件下,进行了火箭基组合循环发动机-液体火箭（RKT）发动机推进的水平起飞两级入轨（TSTO）飞行器飞行轨迹优化计算。研究结果表明：在飞行俯仰角和发动机推进剂质量流量变化范围已知的情况下,利用该方法能够在较好满足给定约束条件的情况下,优化得到飞行俯仰角和发动机流量随时间的变化关系,为飞行轨迹初步设计提供参考。     

Evolution of Dst index,cosmic rays and global temperature during solar cycles 20–23

We have studied conditions in interplanetary space, which can have an influence on galactic cosmic ray (CR) and climate change. In this connection the solar wind and interplanetary magnetic field parameters and cosmic ray variations have been compared with geomagnetic activity represented by the equatorial Dst index from the beginning 1965 to the end of 2012. Dst index is commonly used as the solar wind–magnetosphere–ionosphere interaction characteristic. The important drivers in interplanetary medium which have effect on cosmic rays as CMEs (coronal mass ejections) and CIRs (corotating interaction regions) undergo very strong changes during their propagation to the Earth. Because of this CMEs, coronal holes and the solar spot numbers (SSN) do not adequately reflect peculiarities concerned with the solar wind arrival to 1 AU. Therefore, the geomagnetic indices have some inestimable advantage as continuous series other the irregular solar wind measurements. We have compared the yearly average variations of Dst index and the solar wind parameters with cosmic ray data from Moscow, Climax, and Haleakala neutron monitors during the solar cycles 20–23. The descending phases of these solar cycles (CSs) had the long-lasting solar wind high speed streams occurred frequently and were the primary contributors to the recurrent Dst variations. They also had effects on cosmic rays variations. We show that long-term Dst variations in these solar cycles were correlated with the cosmic ray count rate and can be used for study of CR variations. Global temperature variations in connection with evolution of Dst index and CR variations is discussed.     

补燃循环发动机推力调节过程建模与仿真研究

以补燃循环液氧煤油发动机为研究对象,对其推力调节特性进行了研究.建立了描述补燃循环发动机瞬变过程的数学模型,提出了求解供应系统管路内液体瞬变流控制方程的Chebyshev伪谱方法,应用该模型对补燃循环液氧煤油发动机的推力调节特性进行了仿真计算,并将计算结果与试验数据进行了对比分析,验证了模型和算法的合理性.研究结果表明：对于所研究的补燃循环发动机系统而言,通过调节发生器中较少组元的流量,改变涡轮泵的功率,可很好地实现调节推力的目的,且该推力调节系统具有良好的动态调节品质和很强的抗干扰性.