三维打印技术在粉末材料快速成形中的研究现状评述

基于微喷射的三维打印快速成形技术,集CAD/CAM、数据处理、材料科学、微滴喷射和数控等多种技术于一体,是当前较成熟的快速成形技术之一。     

光电技术在中国深空探测中的应用

文章简单回顾了中国深空探测已走过的历程和正在进行的项目,展望了今后的发展;分析了深空探测器及其有效栽荷对光电技术的需求;重点对中国已发射的月球探测器"嫦娥一号"、"嫦娥二号"中应用的光电技术和获取的成果,正在研制的"嫦娥三号"探测器中所应用的光电技术,月球探测三期和今后可能发展的深空探测项目中预计采用的光电技术的研制工...     

天问一号探测器高动态着陆惯导系统设计与试验

考虑到火星探测任务着陆过程动态变化大,稀薄大气环境下开伞会对探测器产生剧烈晃动,为此天问一号探测器研制了一套高动态着陆惯导系统,从硬件产品、使用时序到导航算法方面均进行了针对性设计,以适应着陆过程中的高动态环境.此外,为验证天问一号探测器高动态着陆惯导系统的性能,设计了模拟火星开伞工况的火箭弹高空开伞试验,结果表明该高...     

一种基于数据驱动的装备信息系统软件快速设计框架

针对装备信息系统类软件特点,提出了一种基于数据驱动的软件设计框架.该框架采用数据土壤生成服务森林的核心设计思想,形成一套快速实现该类软件的设计模式,以及面向表单型、流程型、可视化型等常用业务类型开发的辅助工具,支撑软件的敏捷构建.针对装备数据的异构多源特性,与框架配合提出了面向装备信息的数据规范模型,支撑设计框架的通用化、智能化使用.该设计框架形成了一套面向装备信息类软件的研发指导思路,降低了软件的设计复杂度,提升了软件可靠性.     

Clipper“快船”概念气动特性初探

设计新型高效低廉的运输工具,把有效载荷送入近地轨道是人们不断追求的目标.已成功实现载人天地往返的运输工具包括研制周期长、造价昂贵的可重复使用航天飞机和结构简单、一次性使用的载人飞船两类.为进一步降低发射成本,设计介于航天飞船和航天飞机之间的新型飞行器,集飞船和航天飞机特点于一体的升力再入飞船返回舱也许更为切实可行.俄罗斯联邦空问局提出的可多次使用"快船"概念值得关注,其升阻比高、机动性强、稳定性好、过载低、空间大、成本低,而且可以部分重复使用,代表了未来低成本天地往返运输系统的重要发展方向.     

静叶吸气对某轴流压气机裕度影响的研究

运用Numeca CFD对某大弯度叶栅和某轴流压气机流动进行数值模拟,为减小由于边界层分离而带来的损失,拓宽稳定工作范围,提出叶片吸力面表面开缝抽气方案.综合研究开缝位置、开缝长度、及吸气量大小对流动分离结构和裕度的影响.结果表明通过静子叶片上边界层抽气引出分离区域的低能量气流,可以明显的改善气动性能,分离得到很好的抑制,稳定工作裕度得到了提高.      

锥柱形药柱环形槽内传热现象的数值研究

采用标准k-ε湍流模型和离散传递热辐射模型对不同来流雷诺数下锥柱形药柱前向环形槽内的流场与传热进行了数值研究。对槽内各表面与热气流之间的换热量进行了比较,并对努塞尔数沿环形槽各表面的变化进行了分析。结果表明来流雷诺数的大小影响环形槽内的旋涡数和旋涡区域的分布,进而影响槽内温度的分布,最终影响槽内装药表面与点火热气流之间的换热量。整个计算结果可为装药设计和分析推进剂的热解燃烧提供参考。     

Drag Reduction for an Airship with Proper Arrangement of Propellers

In this article, the flow field around an airship with propellers blowing is calculated on the basis of the Reynolds-averaged Navier-Stokes equations with SST turbulent models. Modeled each as an actuator disk, the propellers are arranged at different positions around the body of airship in the flow direction. The numerical results show that the blowing propellers produce open outer flows. They drive the separated vortexes off the body thus reducing the drag coefficients. The results also show that the position after leading sucking peak is the best place for a propeller to blow. When the propellers are positioned after sucking peak, the longer the area which the propellers work on, the more the profile drag coefficients can be reduced. If the working position of propeller moves from the sucking peak forward to the leading edge, the friction drag coefficient will increase. The bigger the diameter of the propellers and the stronger the pressure jump, the more the drag coefficient will be reduced. The results also reveal that for the design of circularly-positioned propellers with space intervals, the more drag coefficient reduction results, the smaller the space interval is specified.     

新一代战斗机机动作战决策与仿真

近距空战要求新一代战斗机具有较好的机动性能.根据基本的空战机动模式进行机动作战决策的建模,在综合飞行/火力/推进分布式计算机实时仿真系统中,运用大机动非线性鲁棒飞行控制律进行了典型的机动作战仿真.仿真结果表明,具有大机动性能的飞机在空战过程中显示出了很好的效益优势.      

Acceleration sensors based modal identification and active vibration control of flexible smart cantilever plate

Some flexible appendages of spacecrafts, such as solar panels, are cantilever plate structures. Thus, vibration problem is unavoidable when there is slewing maneuver or external disturbance excitation. Vibration of such cantilever plate structures includes coupled bending and torsional motion. Furthermore, the low amplitude vibration near the equilibrium point is very difficult to be quickly suppressed due to nonlinear factors of the hardware in the system, which is harmful to stability and attitude control accuracy. To solve these problems, acceleration sensor-based modal identification and active vibration control methods are presented for the first two bending and the first two torsional modes vibration of the cantilever plate. Optimal placements of three acceleration sensors and PZT patches actuators are performed to decouple the bending and torsional vibration of such cantilever plate for sensing and actuating, and identifications are achieved by experiments. A nonlinear control method is presented to suppress both high and low amplitude vibrations of flexible smart cantilever plate significantly. Experimental comparison researches are conducted by using acceleration proportional feedback and the presented nonlinear control algorithms. The experimental results demonstrate that the presented acceleration sensor-based methods can suppress the vibration of cantilever plate effectively.