纵向过载环境下变质量欧拉梁动特性分析方法

过载是火箭的真实环境.考虑纵向过载环境,根据Hamilton变分原理,得到了欧拉梁变系数横向自由振动微分方程,证明了该变系数系统存在满足刚度和质量正交条件的本征解,揭示了纵向过载环境下欧拉梁本征函数的非对称性.用本征向量叠加方法和改进欧拉中点直接积分算法求解了该变系数系统的动态响应,二者结果的一致性说明该理论推导的正确性和方法的可行性.     

Chlorella vulgaris culture as a regulator of CO2 in a bioregenerative life support system

It is the primary task for a bioregenerative life support system (BLSS) to maintain the stable concentrations of CO₂ and O₂. However, these concentrations could fluctuate based on various factors, such as the imbalance between respiration/assimilation quotients of the heterotrophic and autotrophic components. They can even be out of balance through catastrophic failure of higher plants in the emergency conditions. In this study, the feasibility of using unicellular Chlorella vulgaris of typically rapid growth as both “compensatory system” and “regulator” to control the balance of CO₂ and O₂ was analyzed in a closed ecosystem. For this purpose, a small closed ecosystem called integrative experimental system (IES) was established in our laboratory where we have been conducting multi-biological life support system experiments (MLSSE). The IES consists of a closed integrative cultivating system (CICS) and a plate photo-bioreactor. Four volunteers participated in the study for gas exchange by periodical breathing through a tube connected with the CICS. The plate photo-bioreactor was used to cultivate C. vulgaris. Results showed that the culture of C. vulgaris could be used in a situation of catastrophic failure of higher plant under the emergencies. And the productivity could recover itself to the original state in 3 to 5 days to protect the system till the higher plant was renewed. Besides, C. vulgaris could grow well and the productivity could be affected by the light intensity which could help to keep the balance of CO₂ and O₂ in the IES efficiently. Thus, C. vulgaris could be included in the design of a BLSS as a “compensatory system” in the emergency contingency and a “regulator” during the normal maintenance.     

Solar energetic particle events during the rise phases of solar cycles 23 and 24

We present a comparative study of the properties of coronal mass ejections (CMEs) and flares associated with the solar energetic particle (SEP) events in the rising phases of solar cycles (SC) 23 (1996–1998) (22 events) and 24 (2009–2011) (20 events), which are associated with type II radio bursts. Based on the SEP intensity, we divided the events into three categories, i.e. weak (intensity < 1 pfu), minor (1 pfu < intensity < 10 pfu) and major (intensity ? 10 pfu) events. We used the GOES data for the minor and major SEP events and SOHO/ERNE data for the weak SEP event. We examine the correlation of SEP intensity with flare size and CME properties. We find that most of the major SEP events are associated with halo or partial halo CMEs originating close to the sun center and western-hemisphere. The fraction of halo CMEs in SC 24 is larger than the SC 23. For the minor SEP events one event in SC23 and one event in SC24 have widths < 120° and all other events are associated with halo or partial halo CMEs as in the case of major SEP events. In case of weak SEP events, majority (more than 60%) of events are associated with CME width < 120°. For both the SC the average CMEs speeds are similar. For major SEP events, average CME speeds are higher in comparison to minor and weak events. The SEP event intensity and GOES X-ray flare size are poorly correlated. During the rise phase of solar cycle 23 and 24, we find north–south asymmetry in the SEP event source locations: in cycle 23 most sources are located in the south, whereas during cycle 24 most sources are located in the north. This result is consistent with the asymmetry found with sunspot area and intense flares.     

使用波导模型研究“长空一号”靶机喷气式发动机进气道的雷达反射特性

本文采用波导模型模拟发动机进气道,计算和实验测量了截面积为10×10厘米~2的矩形波导的RCS值,两者结果基本相符。通过这一方法,计算了“长空一号”靶机进气道的RCS值,与地面静态测量比较,结果令人满意。这样,对于复杂的喷气式飞机目标,其机头和机尾的RCS值就可通过波导模型的模拟来修正。     

壁稳电弧等离子体温度和辐射标准设备的研制

研制了氩壁稳电弧等离子体装置,其最大功率25kW,电流0～140A,4小时内电流的稳定性0.005%,纹波系数0.1%。在可靠的状态诊断实验基础上测试了主要性能。当压力为0.1～0.5MPa、电流不小于20A 时,电弧轴心区等离子体是LTE(局部热力学平衡)的。60A 电流下4小时内 ArI430.0nm 谱线辐射的稳定性±1.0%,1个月内的再现性±1.8%,温度可调范围10000～16000K,不确定度0.4%。同时测定了某些特定谱线斯塔克宽度与电子密度的实验关系。结果表明,性能完全达到了建立10000～15000K温度和近紫外高强度及真空紫外辐射标准的要求。     

CNC系统中提高回原位精度的实现

提高回原位精度是计算机数值控制ＣＮＣ系统开发中的关键技术问题之一,本文在指出了以往回原位算法的缺陷并分析了引起数控系统回原位误差因素的基础上,提出了引入回原位国界参数和最终逼近原位方向参数,从而提高数控系统回原位精度的算法,并提出了在闭环或半闭环数控系统中利用检索脉冲输入从而消除原位开关激活边界位置误差的思想,提出了适用于闭环或半闭环数系统的全新的高精度的回原位算法。     

飞机电热防冰用BaTiO3热敏陶瓷力学性能的改进

飞机电热防冰系统用ＢａＴｉＯ３基ＰＴＣ热敏陶瓷材料要求有低电阻及优良的ＰＴＣ效应,同时有良好的力学性能。本文叙述了在ＢａＴｉＯ３为基的ＰＴＣ材料中,通过配方组成设计及先进的工艺制备手段,获得了居里温度５０℃,室温体电阻率８０Ω·ｃｍ,ＰＴＣ效应１０６数量级,耐电压２４０Ｖ／ｍｍ,断裂韧性ＫＩＣ１９．１４ＭＮ／ｍ３／２,冲击韧性２．６Ｊ／ｃｍ２,抗弯强度１０８ＭＰａ,综合性能优良的ＰＴＣ材料。初步实验表明,该发热体陶瓷具有较强的防冰和化冰能力。     

飞机无刷交流发电机设计原则及试验仿真研究

旋转整流器式无刷交流发电机是飞机恒速恒频、变速恒频及高压直流电源系统的核心部件。随着电机制造材料的发展,无刷交流发电机的设计也在不断发展与完善。变速恒频及高压直流电源中的无刷交流发电机后级带整流负载,因而电机结构有别于恒速恒频电源中的发电机。为实现体积小、重量轻、性能好的设计目标,讨论了变速恒频电源中无刷交流发电机的设计原则。并结合某一样机实例,对无刷交流发电机进行了数字仿真并对样机进行了性能试验,样机试验及仿真结果基本吻合,说明数字仿真的正确性。针对该样机的设计不足,本文提出了一种改进方案,从而进一步改善了电机结构和工艺性。     

开关点预置最优SPWM变换器控制方案研究

开关点预置的正弦脉宽调制变速恒频电源,对开关点进行最优设定,使得输出电压性能优良。由于ＧＴＲ的开关频率限制,传统的开关点预置控制方案为９块波开关点预置最优ＳＰＷＭ控制方案。本文详细地讨论了开关点预置ＳＰＷＭ控制方案的理论,并针对以ＩＧＢＴ作为主功率模块的变换器,通过提高斩波频率,采用１７块波的开关点预置最优ＳＰＷＭ控制方案,进一步提高了输出电压质量和输出滤波器的谐振频率,减轻了输出滤波器体积重量,     

编入碳纤维编织复合材料的光纤光学性能实验研究

三维编织复合材料是当前先进复合材料领域研究的热点并已开始广泛应用于航空航天等许多领域.三维编织复合材料具有很多优点,但这种材料的性能也较复杂.文中提出一种研究三维编织复合材料性能的新方法,也即将光纤传感器多个编入编织复合材料实现编织智能复合材料,以监测三维编织复合材料的RTM工艺过程,研究其力学性能及监测其在使用过程中的健康状况.对于光纤传感器而言,光纤的光学性能的好坏同光纤传感器的性能密切相关,因此,着重通过实验提出了一种光纤编入三维编织复合材料的方法并对光纤编入材料前后及编入后随材料进行RTM固化前后的光学性能进行了测试对比研究.