高风险场所安全防范系统不确定性分析与评估

安全防范系统运行的有效性是保证被防护对象的关键。然而,安全防范系统本身及其运行环境存在多种不确定性因素,这些不确定性的存在将导致场所内存在很大的风险性,如果分析处理不当会产生严重的后果。在给出物理系统不确定性模型的基础上,分析了安全防范系统中存在的不确定性因素,提出了层次分析和灰色理论相结合的方法,评估不确定风险因素的权重,实现对入侵报警系统不确定性的评估。     

Variations of ionospheric total electron content before three strong earthquakes in the Qinghai-Tibet region

We investigate the ionospheric total electron content (TEC) anomalies occurred in the Qinghai-Tibet region before three large earthquakes (M > 7.0). The temporal and spatial TEC variations were used to detect the ionospheric possible precursors of these earthquakes. We identified two TEC enhancements in the afternoon local time 9 days and 2–3 days before each earthquake, between which a TEC decrement occurred 3–6 days before earthquakes. These anomalies happened in the area of about 30° in latitude and the maximum is localized equatorward from the epicenters. These TEC anomalies can be found in all three earthquakes regardless the geomagnetic conditions. The features of these anomalies have something in common and may have differences from those caused by geomagnetic storms. Our results suggest that these ionospheric TEC perturbations may be precursors of the large earthquakes.     

DDV作动器余度数字伺服系统工程设计与实现

 介绍一种直接驱动阀（DDV）式作动器的余度数字式伺服系统设计与实现,描述了系统的余度配置、设计思想及组成,建立了DDV作动器的结构参数化模型及数字伺服回路的模型,并进行了仿真,分析了作动器动静态特性、采样频率及监控器的设计性能。最后,采用快速原型实时仿真,对余度数字式伺服系统完成了的性能试验验证,结果表明系统性能令人满意。     

无损检测技术在姿控发动机总装中的应用探析

阐述了目视检测、射线照相检测、泄漏检测等三种无损检测技术在姿控发动机上的应用情况。重点介绍了泄漏检测技术,针对发动机的结构特点、不同系统的性能要求及总装接头连接处各种密封形式在装配测试中分别采用了浸泡法、皂泡法及氦质谱简易包封积累法等不同的泄漏检测技术。经过对几种泄漏检测方法的对比分析,得出了针对不同的系统性能要求。需要采用不同的泄漏检测方法来满足设计要求的结论。     

基于BP神经网络的国防企业技术创新能力评价

结合自组织理论提出了国防企业技术创新评价体系,构建了BP神经网络模型,运用MATLAB软件进行了模型仿真.研究发现仿真结果与专家评价结果基本一致.可见,运用BP神经网络方法对国防企业技术创新能力进行评价有一定的通用性、便捷性和实用性.     

细节信息容量与MTF相关分析

文章从信息容量的角度出发,对图像宏观质量做出评价,再通过研究图像的细节信息容量参数,对在宏观上质量相当的图像做出更进一步的评价,挑选出边缘清晰、纹理等细节信息丰富的图像。然后将该评价参数与Ealing仪测得的调制传递函数(MTF)值的变化趋势作曲线回归分析,实验结果表明,细节信息容量与数字成像系统的MTF值的变化有着很好的正相关关系,这对评价数字成像系统MTF变化情况具有较好的实际应用价值。     

仿生硬件及其进展

文章详细介绍了仿生硬件的概念、主要特征及用途 ,阐述了仿生硬件的进化原理及实现思想 ,重点分析了仿生硬件的关键技术———可进化硬件电路、硬件进化方法 ,并总结了研究状况与最新进展 ,讨论了需要解决的核心难点问题及其解决思路 ,最后指出了仿生硬件的研究方向及发展前景。     

基于某微型发动机对比分析轴流涡轮与向心涡轮的气动性能与减重

为了确定厘米级微型涡轮发动机在相对较大功率、流量需求时的涡轮形式,以实现发动机更高的性能,本文基于某直径12厘米微发样机开展研究。本文估算了该样机整机环境下单级轴流涡轮的做功能力,并按参数优选规律设计了一台微型轴流涡轮,将之与该样机所采用的微型向心涡轮进行对比,基于CFD和CAD工具分析了两种叶轮在功率、效率及尺寸重量方面的差别。研究表明：在先进微小型发动机总压比提高（4～6,本文设计采用4.2）的情况下,涡轮为了在保持效率的同时满足压气机更高的功率需求,轴流式必须采用双级方案,向心式单级就可满足要求;在压气机压比4～6条件下,进一步对比双级轴流与单级向心方案的结果显示,当流量小于500g/s时,向心式具有尺寸重量优势,发动机能实现较高的推重比。针对厘米级微型发动机,在发动机增压比较高且没有超出单级向心涡轮做功能力的范围时,向心涡轮方案是更好的选择。     

Automatic differentiation based discrete adjoint method for aerodynamic design optimization on unstructured meshes

A systematic methodology for formulating, implementing, solving and verifying discrete adjoint of the compressible Reynolds-averaged Navier-Stokes (RANS) equations for aerodynamic design optimization on unstructured meshes is proposed. First, a general adjoint formulation is con-structed for the entire optimization problem, including parameterization, mesh deformation, flow solution and computation of the objective function, which is followed by detailed formulations of matrix-vector products arising in the adjoint model. According to this formulation, procedural components of implementing the required matrix-vector products are generated by means of auto-matic differentiation (AD) in a structured and modular manner. Furthermore, a duality-preserving iterative algorithm is employed to solve flow adjoint equations arising in the adjoint model, ensur-ing identical convergence rates for the tangent and the adjoint models. A three-step strategy is adopted to verify the adjoint computation. The proposed method has several remarkable features:the use of AD techniques avoids tedious and error-prone manual derivation and programming;duality is strictly preserved so that consistent and highly accurate discrete sensitivities can be obtained; and comparable efficiency to hand-coded implementation can be achieved. Upon the cur-rent discrete adjoint method, a gradient-based optimization framework has been developed and applied to a drag reduction problem.     

航天器复合材料胶接连接工艺分析

文章叙述了航天器复合材料胶接工艺应具备的条件,航天器产品常用胶粘剂及其特性,研制航天器复合材料耐久型胶接结构基本要素及复合材料胶接连接工艺特性和品质控制等内容。