双层板激光焊接/ 超塑成形数值模拟及工艺研究

选取TC4 钛合金四层板加强结构中双层板为研究对象,采用激光穿透焊接工艺代替传统超塑成

形/ 扩散连接(SPF/ DB)工艺中涂止焊剂连接。借助ABAQUS 有限元分析软件对超塑成形过程进行分析,得到

优化的压力-时间(p-t)曲线,作为双层板超塑成形过程的气压加载曲线,进行实验验证。结果表明:成形后零

件壁厚分布均匀,焊缝处无撕裂现象,与有限元模拟结果保持一致;用此新工艺代替传统SPF/ DB 工艺中的止

焊剂具有可行性。

     

Multiple Coulomb scattering method to reconstruct low-energy gamma–ray direction in the GAMMA-400 space-based gamma–ray telescope

The GAMMA-400 currently developing space-based gamma-ray telescope is designed to measure the gamma-ray fluxes in the energy range from ～20?MeV to several TeV in the highly elliptic orbit (without shadowing the telescope by the Earth) continuously for a long time. The physical characteristics of the GAMMA-400 gamma-ray telescope, especially the angular and energy resolutions (at 100-GeV gamma rays they are ～0.01° and ～1%, respectively), allow us to consider this space-based experiment as the next step in the development of extraterrestrial high-energy gamma-ray astronomy. In this paper, a method to improve the reconstruction accuracy of incident angle for low-energy gamma rays in the GAMMA-400 space-based gamma-ray telescope is presented. The special analysis of topology of pair-conversion events in thin layers of converter was performed. Applying the energy dependence of multiple Coulomb scattering for pair components, it is possible to estimate the energies for each particle, and to use these energies as weight in the angle reconstruction procedure. To identify the unique track in each projection the imaginary curvature method is applied. It allows us to obtain significantly better angular resolution in comparison with other methods applied in current space-based experiments. When using this method for 50-MeV gamma rays the GAMMA-400 gamma-ray telescope angular resolution is about 4°.     

Simultaneous observations of spread F irregularities over Southeast Asia longitude using Sanya VHF radar,GPS and C/NOFS

Through concurrently measurements by Communication/Navigation Outage Forecasting System (C/NOFS), Sanya VHF radar and GPS ionospheric scintillation receiver on 12 March 2010, five plasma bubbles were found and three of them were observed by all those instruments. Two well-developed plumes with strong backscatter echoes were measured by Sanya radar and their corresponding depletions were observed by C/NOFS in Orbit 10317, 10318 and 10319. Broad plasma depletions resulting from merging process were found in orbit of 10318. The occurrence time and geophysical positions of scintillations correlate well with observations implemented by Sanya VHF radar and C/NOFS. Observations from three types of instrument indicate that the spread F irregularities have distinct scale. There were longitudinal differences between Sanya VHF radar and C/NOFS as irregularities measured, and the eastward drift of developed bubbles are responsible for these differences.     

Exploration life support technology challenges for the Crew Exploration Vehicle and future human missions

As NASA implements the U.S. Space Exploration Policy, life support systems must be provided for an expanding sequence of exploration missions. NASA has implemented effective life support for Apollo, the Space Shuttle, and the International Space Station (ISS) and continues to develop advanced systems. This paper provides an overview of life support requirements, previously implemented systems, and new technologies being developed by the Exploration Life Support Project for the Orion Crew Exploration Vehicle (CEV) and Lunar Outpost and future Mars missions. The two contrasting practical approaches to providing space life support are (1) open loop direct supply of atmosphere, water, and food, and (2) physicochemical regeneration of air and water with direct supply of food. Open loop direct supply of air and water is cost effective for short missions, but recycling oxygen and water saves costly launch mass on longer missions. Because of the short CEV mission durations, the CEV life support system will be open loop as in Apollo and Space Shuttle. New life support technologies for CEV that address identified shortcomings of existing systems are discussed. Because both ISS and Lunar Outpost have a planned 10-year operational life, the Lunar Outpost life support system should be regenerative like that for ISS and it could utilize technologies similar to ISS. The Lunar Outpost life support system, however, should be extensively redesigned to reduce mass, power, and volume, to improve reliability and incorporate lessons learned, and to take advantage of technology advances over the last 20 years. The Lunar Outpost design could also take advantage of partial gravity and lunar resources.     

液氧／甲烷气液喷注器试验研究

介绍了液氧／甲烷气液喷注器热试验情况,试验燃烧室压力7．1～7．4MPa,混合比3．5～3．9。研究了不同的喷嘴结构参数对燃烧性能和流量特性的影响。获得了燃烧效率、流量系数、振动、点火性能以及积炭特性等重要参数。     

高压球形气瓶焊缝结构设计与焊接工艺

研究了气瓶赤道焊缝区的结构优化设计和焊接工艺改进措施,焊缝区渐变补强设计提高了焊缝区的应变协调性,改进电子束与焊缝作用方式解决了内部飞溅问题,采用优化的电子束工艺参数进行焊接。结果表明:焊接接头质量达到了GJB1718A—2005《电子束焊接》标准Ⅰ级焊缝,焊缝及热影响区力学性能与母材相当,气瓶进行鉴定试验,性能指标满足设计要求。气瓶焊缝结构优化设计,降低了焊缝处应力水平,减少应力集中,通过改进焊接工艺提高了电子束焊缝质量。     

真空中多孔氮化硅的高温弯曲强度

研究了高温真空环境下多孔(气孔率>50%)氯化硅陶瓷的弯曲强度,并进行了初步分析.结果表明,多孔氮化硅陶瓷在真空中的高温强度随温度上升而降低,由于没有氧化作用,晶界玻璃相在高温下的软化成为影响其强度的主要因素.     

限制性四体问题中的时间相关不变流形

借助有限时间Lyapunov指数（FTLE）定义了拉格朗日拟序结构（LCS）,并将LCS作为不变流形的替代物。针对日-地-月双圆模型（BCM）,利用LCS研究了限制性四体问题（R4BP）中的时间相关不变流形（TDIM）的性质。采用数值方法验证了TDIM是运动分界面和轨道不变集。继而,利用二分法对给定Poincare截面上的LCS进行了精确提取,通过一系列等能量面上的LCS描绘出TDIM在给定截面上的构形。最后,借助TDIM,初步研究了低能奔月轨道在非自治系统BCM中的直接构建。     

基于软件无线电技术的4G数字接收系统设计

研究了基于软件无线电技术的体系结构,设计了一种基于软件无线电技术的4G数字接收系统,并对该系统各主要部分电路设计进行了详细阐述。该设计系统具有双通道,采样速率可达到65MHz,分辨率12bit。由于该设计采用了FPGA作为信号处理器,其设计灵活及可编程等特点使得该设计具有较强的通用性,适合4G通信中应用。     

~4He量子干涉仪陀螺的数学模型(英文)

建立了4He量子干涉仪陀螺的数学模型,包括驱动方程,流量方程和位置方程。该数学模型可以完整地描述4He量子干涉仪陀螺系统。由驱动方程可知,采用热驱动的陀螺能够长期工作,但采用压力驱动的陀螺只能短时间工作。由流量方程可知,流过弱连接的超流体流量中,不仅含有表示旋转通量的交流流量,还含有由驱动引起的其他流量。位置方程表达了薄膜的位移,该位移是陀螺系统中唯一能被检测的物理量。基于实验参数的仿真验证了数学模型的有效性。根据本文建立的数学模型,可以进一步研究4He量子干涉仪陀螺的性能和分析该陀螺的误差。