太阳系边际探测飞行任务规划

针对太阳系边际探测任务,开展了星际多目标飞越的任务规划,采用小推力混合优化设计方法完成了基于借力飞行及电推进技术的行星际转移轨道联合优化设计,对比研究了面向日球层鼻尖和尾部探测的星际多目标探测飞行方案.研究表明,探测器在2024-2025年发射,可飞抵日球层鼻尖区域,在2027-2030年发射可飞抵日球层尾部区域,并可...     

航天器近程编队自主协同相对导航方法

针对GNSS(全球导航卫星系统)拒止环境下近圆轨道多航天器近距离编队自主协同相对导航问题,提出了利用测角相机偏离航天器质心安装时的杆臂效应和多航天器之间几何一致性约束来实现相对导航的方法.首先,在第二轨道坐标下分别建立了基于Hill-Clohessy-Wiltshire方程的多航天器编队相对轨道演化模型、测角相机偏离质...     

Experimental study of curvature effects on jet impingement heat transfer on concave surfaces

Experimental study of the local and average heat transfer characteristics of a single round jet impinging on the concave surfaces was conducted in this work to gain in-depth knowledge of the curvature effects. The experiments were conducted by employing a piccolo tube with one sin-gle jet hole over a wide range of parameters: jet Reynolds number from 27000 to 130000, relative nozzle to surface distance from 3.3 to 30, and relative surface curvature from 0.005 to 0.030. Exper-imental results indicate that the surface curvature has opposite effects on heat transfer characteris-tics. On one hand, an increase of relative nozzle to surface distance (increasing jet diameter in fact) enhances the average heat transfer around the surface for the same curved surface. On the other hand, the average Nusselt number decreases as relative nozzle to surface distance increases for a fixed jet diameter. Finally, experimental data-based correlations of the average Nusselt number over the curved surface were obtained with consideration of surface curvature effect. This work con-tributes to a better understanding of the curvature effects on heat transfer of a round jet impinge-ment on concave surfaces, which is of high importance to the design of the aircraft anti-icing system.     

平面磨削石英陶瓷比磨削能正交试验研究

通过大量的正交试验,研究陶瓷材料在低速下的磨削性能,优化陶瓷磨削参数,对于丰富陶瓷磨削理论,指导实际生产实践具有重要的现实意义.     

运输类飞机发动机短舱火焰防护设计与验证

通过对CCAR-25部运输类飞机发动机短舱火焰防护适航条款的要求进行分析,按照防火、耐火要求将条款内容进行对比,参考美国联邦航空局的咨询通告和修正案,对火焰防护的确定原则、设计要求与验证方法进行了研究,明确发动机短舱内的材料和零部件的防火、耐火要求。     

Real-time and reliability analysis of time-triggered CAN-bus

Real-time performance and reliability are two most important issues in applications of time-triggered controller area network (CAN) bus systems at present. A scheduling matrix of time-triggered CAN-bus system is established using average-loading algorithm. Periodic messages are guaranteed to transmit without delay by distributing independent transmission windows within the system matrix. Considering the traditional CAN-bus transmission mechanism and the time-triggered feature, an algorithm is improved to calculate the worst-case delay of event-triggered messages in time-triggered CAN-bus systems. The failure probability is calculated for event-triggered messages whose worst-case delay exceeds their deadlines. Different levels of redundant structures of CAN-bus circuits are analyzed and the maintenance management is proposed to improve the system reliability. Finally, the reliabilities of different structures are calculated and the influences of maintenance on the system reliability are analyzed.     

航空发动机高能X射线测试系统

综合介绍了高能X射线测试系统在航空发动机试验中的作用和基本组成以及国内外高能X射线测试技术开发应用情况。     

基于面向对象技术的典型工艺知识库系统

建立了多层次的典型工艺结构,充分利用相似特征具有相似工艺的理论;研究了工艺查询、工艺评价和工艺设计等应用子系统的功能结构,开发了面向对象的典型工艺知识库系统。     

Dispersion-free quantum clock synchronization via fiber link

We proposed a fiber-based quantum clock synchronization protocol by employing the dispersion cancellation feature of the frequency anti-correlated entangled source under the quantum interference measurement. It is shown that, the accuracy of the synchronization is mainly dependent on the bandwidth of the frequency entangled biphoton spectrum and on the temperature variation induced fluctuations in both the reference fiber coiling and the fiber link. With this proposal, synchronization between two clocks at a distance of ten kilometers can be implemented with an accuracy below a picosecond.