40Cr/T10A钢激光预处理后固相焊接工艺优化

进行了 4 0Cr T10A钢激光表面淬火预处理后实施等温固相焊接的工艺优化试验。结果表明 ,4 0Cr T10A钢待焊接面经激光淬火预处理后 ,在 75 0～ 780℃、预压应力 2 0～ 5 6 .6MPa的条件下 ,仅需 2 .5～ 7.5min短时保温就可实现两种钢的异材固相焊接 ,接头强度达母材强度 ,且焊接变形很小。其中以 780℃、2 0MPa预压应力下保温7.5min为较适宜的固相焊接工艺参数 ,焊后接头强度达母材强度 ,试样轴向变形仅 1.2 %。     

新甘交界北山地区大泉断裂走滑特征及ESR测年证据

卫星图片显示穿过大泉断裂的水系有被左行扭曲的特征,结合野外断层面上擦痕、断裂带中劈理观测统计和室内对断层岩显微构造的分析,确定了大泉断裂是以左行为主的走滑断裂带。对断层泥的ESR年代学测定,确定了大泉断裂开始活动时间为早更新世1.2～1.5Ma,其分支断层的活动时间在晚更新世300ka左右。大泉断裂活动时间与青藏高原在上新世末-早更新世初开始强烈隆升时间一致,表明大泉断裂的形成与青藏高原的隆升过程密切相关,是晚新生代印度和欧亚两大板块持续碰撞挤压和青藏高原隆升的远程效应。     

Finds in Testing Experiments for Model Evaluation

To evaluate the fault location and the failure prediction models, simulation-based and codebased experiments were conducted to collect the required failure data. The PIE model was applied to simulate failures in the simulation-based experiment. Based on syntax and semantic level fault injections, a hybrid fault injection model is presented. To analyze the injected faults, the difficulty to inject (DTI) and difficulty to detect (DTD) are introduced and are measured from the programs used in the code-based experiment. Three interesting results were obtained from the experiments: 1) Failures simulated by the PIE model without consideration of the program and testing features are unreliably predicted; 2) There is no obvious correlation between the DTI and DTD parameters; 3) The DTD for syntax level faults changes in a different pattern to that for semantic level faults when the DTI increases. The results show that the parameters have a strong effect on the failures simulated, and the measurement of DTD is not strict.     

按行程速比系数K设计空间曲柄滑块机构的图解计算法

讨论了按行程速比系数Ｋ（≤１）设计滑块与曲柄运动平面互相垂直的空间曲柄滑块机构的图解计算方法，提出了根据机构运动连续性条件确定曲柄固定铰链中心Ａ的选取原则和选择区域的正确方法。     

Orbit determination of Chang＇E-3 and positioning of the lander and the rover

Chang＇E-3 landed on the east of Sinus Iridum area on December 14, 2013, performing China＇s first successful soft landing on the lunar surface. We present the results on precision orbit determination and positioning of the lander and the rover. We and methods used to achieve period December 2-21, 2014. describe the data, modeling, position knowledge over the In addition to the radiometric X-band range and Doppler tracking data, delta differential one-way ranging data are also used in the calculation, which show that they strongly improve the accuracy of the orbit reconstruction. Total position overlap differences are about 20 and 30m for the 100km × 100km and 100 kmx 15 km lunar orbit, respectively, increased by ,- 50 % with respect to CE-2 and at the same level as other lunar spacecrafts of recent era such as SELENE and lunar reconnaissance orbiter （LRO）. The position error of the soft landing trajectory is less than 100 m. A kinematic statistical method is applied to determine the position of the lander and relative position of the rover with respect to the lander. The position difference of the lander is better than 50 m compared to LRO photograph result. Compared with the delta very long baseline interferometry （VLBI） group delay between the lander and the rover, the delta VLBI phase delay can improve the relative position of the rover from ～ 1,000 to ～1 m.     

汽车离合器传动片设计研究

汽车离合器传动片是离合器传递载荷的重要零件 ,承受复杂载荷 ,而汽车离合器传动片设计方法的研究却不多 笔者分析了汽车离合器传动片工作时的各种受力情况及其变形量的大小 ,给出了传动片设计计算的双端固定梁的力学模型和进行强度、稳定性校核准则 ,并进行了应力和变形试验 ,试验结果与理论计算基本吻合     

非齐次Hamilton系统的Birkhoff表示

本文首先讨论了Hamilton系统与Birkhoff系统的关系,以及Birkhoff系统研究的理论意义和实际价值．进一步研究了非齐次Hamilton系统的Birkhoff化理论、Birkhoff方程的实现条件、构造方法,指出了Birkhoff动力学研究的主要困难和未来应该重点关注的基本问题;最后给出了广义Birkhoff系统动力学方程的形式以及研究广义Birkhoff方程的重要意义,并探讨了赝广义Birkhoff方程的形式以及构造动力学系统赝广义Birkhoff方程的目的和意义．     

柴油机电控蓄压式喷油系统的开发与应用

开发和应用电控蓄压式喷油系统。采用蓄压式泵－喷嘴系统及高速电磁阀来实现燃油增压过程和燃油喷射过程;采用电液比例溢流阀实现共轨燃油压力的调节过程;确定喷油量、喷油压力和喷油定时的电控实现途径;开发实验监控系统以满足喷油系统与柴油机匹配的需要。实现了喷油量、喷油压力和喷油始点的柔性（电子）控制,而且最高喷油压力已达１１３．５ＭＰａ,初步进行了喷油系统与１１５０Ｇ柴油机的匹配实验。在喷油压力与柔性控制方     

计算再入飞行器可达区域的快速算法

以无量纲反值能量为自变量建立了飞行器3自由度运动方程组,提出了一种改进的计算再入飞行器可达区域的快速算法.引入倾侧角反向策略,使计算的可达区域更精确;改进产生可达区域中间边界的插值方式,使计算结果更加均匀;改进了终端约束处理方法,使弹道更加平滑.以一种乘波体模型为例进行仿真验证,仿真结果表明改进算法计算的可达区域比现有算法更精确且弹道更平滑.     

低轨道移动卫星信道中的DDPSK调制特性

针对低轨道卫星移动通信信道的大范围快速时变的多普勒频移特性,提出并分析了双差分相位调制方式（DDPSK）。结果证明,DDPSK与相关相位调制、差分相位调制相比,对于频率变化有很好的稳定性,能够克服大频偏对于移动通信的影响。并进一步给出了它在带遮蔽效应的莱斯信道的误码特性。