大型舱体螺纹孔位置精度测量方法分析

通过螺纹孔测量试验,获得了三坐标测量机测量的光孔与螺纹孔孔位偏差、激光跟踪仪和三坐标测量机测量的螺纹孔孔位偏差,分析了螺纹孔孔位偏差与其轴线相对端面垂直度的相关性,并获得了螺纹配合的间隙量。试验数据表明,激光跟踪仪和三坐标测量机测量的螺纹孔数据一致性较好,基于测量工装的螺纹孔位置测量数据与光孔测量数据最大偏差约0.2mm,螺纹孔垂直度误差是造成此偏差的一个因素,但螺纹配合的不确定性和容差性使此偏差对螺纹孔的使用影响较小。     

谈高校统计档案资料的整理与利用

文章从高校统计工作生成的档案资料出发,阐述了建立高校统计档案资料的重要性。对统计档案资料的收集、整理、保管和利用等问题进行了探讨,提出了一些基本思想。     

低重力环境下基于超弹性铰链的某折展机构展开动力学研究

针对地外行星、月球探测中杆状天线对轻量化折展机构的需求,提出了一种基于超弹性铰链的两折杆折展机构,天线展开长度可达1.3 m,折展机构重量小于200 g;建立了超弹性铰链的薄壳大变形模型和机构的有限元分析模型,同时引入重力场影响,对不同重力场下机构展开动力学行为、展开时序进行了分析,并对天线末端特征点最大位移进行了预测;利用该折展机构原理样机开展了地球重力条件下的展开试验,使用高速摄影对展开过程进行记录并反演获得特征点位移信息,验证了特征点实际最大位移与分析值的一致性.基于超弹性铰链的两折杆折展机构的设计思路与分析方法,可以为我国后续深空探测更长尺度天线折展机构的设计与分析提供新的思路.     

Fabrication and Investigation on Double-Hollow Shell CoFe Oxide@TiO2 Nanocube with Superior Electromagnetic Properties

Electromagnetic wave absorbing materials are urgently required in the fields of medicine, communication, and military. However, the thickness, weight, narrow effective bandwidth, and weak absorbing ability of the materials restrict their further application. In this work, a double-layer hollow nanocube with a dielectric titanium dioxide (TiO2) shell and a magnetic CoFe oxide inner shell is prepared. Prussian blue (PB) is prepared by the hydrothermal method, and used as the template to prepare PB@CoFe PB analogue (PBA). After selective etching and further calcination, hollow CoFe oxide particles are obtained. The obtained particles are then coated with SiO2 and TiO2, respectively, and the intermediate layer is dislodged to obtain the final CoFe oxide@TiO2 with the hollow double shell structure. The obtained double-layer hollow structure can effectively capture the incident electromagnetic waves, and increase the propagation path. Moreover, the obvious enhancement of interface polarization and the improvement of impedance matching enhance the wave absorbing ability of the material. The analysis results show that, the structure is stable and the dispersion is good. The maximum reflection loss (RL) at 10 GHz is as high as -46.1 dB with the sample thickness of 1.6 mm. The light-weight and high-efficiency CoFe oxide@TiO2 absorber is promised to be used in commercial and military aerospace fields.     

双组元离心式喷注器10 N发动机偏工况试验

根据国内外同类发动机研制经验,双组元10 N发动机在入口压力为0.8~2.2 MPa范围内,入口压力偏差会使发动机真空比冲、燃气温度等性能产生较大变化。为了获得双组元离心式喷注器10 N发动机在落压推进系统要求的入口压力范围内性能,通过采用小流量喷雾试验台和42 km高模试验台,对偏工况条件下的冷态性能及热试性能进行试验研究。试验结果表明:该发动机额定入口压力1.58 MPa时真空比冲为2881 N·s/kg;当入口压力在0.6~2.5 MPa变化时,对应真空推力从4.7 N增加到14 N,落压比为3;入口压力0.6 MPa时真空比冲为2600 N·s/kg,入口压力2.5 MPa时真空比冲为2956 N·s/kg;入口压力在0.6~2.5 MPa试验范围内,发动机燃烧室壁温均低于材料许用温度,表明发动机热设计优良,可满足双组元落压推进系统对姿控发动机的性能需求。     

Risk Index Prediction of Civil Aviation Based on Deep Neural Network

Safety is the foundation of sustainable development in civil aviation. Although catastrophic accidents are rare,indicators of potential incidents and unsafe events frequently materialize. Therefore,a history of unsafe data are considered in predicting safety risks. A deep learning method is adopted for extracting reactions in safety risks. The deep neural network(DNN)model for safety risk prediction is shown to extract complex data characteristics better than a shallow network model. Using extended unsafe data and monthly risk indices,hidden layers and iterations are determined. The effectiveness of DNN is also revealed in comparison with the traditional neural network. Through early risk detection using the method in the paper,airlines and the government can mitigate potential risk and take proactive measures to improve civil aviation safety.     

UHMWPE/LDPE层合板复合材料损伤声发射信号识别

为了掌握UHMWPE/LDPE复合材料的损伤机理,运用声发射技术结合聚类分析方法建立不同损伤形式的声发射信号训练样本,通过神经网络实现损伤信号的识别,并分别探讨了训练函数、传递函数、网络结构等因素对识别率的影响。研究表明,由系统聚类可提取幅度、峰值频率、持续时间为模式特征,结合Kmeans聚类可建立11个类别共583信号的训练样本。以混淆矩阵为识别率指标,当训练函数为traingdx、隐层/输出层传递函数为tansig/logsig、隐层神经元数量为70时,网络的识别率达97.2%,为基于声发射技术的热塑性基体复合材料损伤识别提供参考。     

再入飞行器偏离稳定判据的研究与应用

针对动态偏离敏感参数(CnβDYN)和侧向操纵偏离参数(LCDP)无法预测飞行器在大侧滑角飞行条件下偏离失稳特性的不足,推导建立了大攻角、大侧滑角条件的飞行器动态偏离判据和操纵偏离判据,指出该判据包含了飞行器的所有飞行状态,能够更精确的反映系统的静稳定性需求,可作为一种通用的预测偏离失稳的判据,并对某再入飞行器应用新偏离稳定判据,进行了偏离稳定性分析.     

模糊自组织神经网络在航空发动机故障诊断中的应用

介绍了模糊自组织神经网络在航空发动机故障诊断中的应用方法,并通过实例验证了该方法在发动机故障分类中的实用性。该方法具有结构算法简单、无监督自学习和侧向联想等功能。它有很好的应用前景,可以广泛应用于发动机的故障诊断。      

Ni47Ti44Nb9形状记忆合金耐蚀性能和抗氧化性能研究

采用高温氧化、电化学腐蚀测试,并结合SEM,XRD等分析手段,研究了Ni47Ti44Nb9合金的氧化性能和抗腐蚀性能。结果表明,Ni47Ti44Nb9合金在450℃下氧化非常轻微,600～800℃下合金的氧化增重曲线近似符合抛物线规律。经高温氧化后,合金表面形成的氧化层具有分层结构,氧化截面由外氧化层和过渡层组成。电化学腐蚀结果表明,溶液中NaCl含量越低,溶液温度越低,合金的腐蚀电流密度越小,腐蚀电位正移,保护膜的稳定性提高。