Variable stiffness design of redundantly actuated planar rotational parallel mechanisms

Redundantly actuated planar rotational parallel mechanisms (RAPRPMs) adapt to the requirements of robots under different working conditions by changing the antagonistic internal force to tune their stiffness. The geometrical parameters of the mechanism impact the performances of modulating stiffness. Analytical expressions relating stiffness and geometrical parameters of the mechanism were formulated to obtain the necessary conditions of variable stiffness. A novel method of variable stiffness design was presented to optimize the geometrical parameters of the mechanism. The stiffness variation with the internal force was maximized. The dynamic change of stiffness with the dynamic location of the mechanism was minimized, and the robustness of stiff-ness during the motion of the mechanism was ensured. This new approach to variable stiffness design can enable off-line planning of the internal force to avoid the difficulties of on-line control of the internal force.     

小展弦比飞翼亚、跨、超声速支撑干扰研究

通过数值模拟方法研究了小展弦比飞翼标模在0.6、0.9、1.5三个典型马赫数下的支撑干扰特性,分别考虑了近场尾部外形局部畸变和尾支杆干扰及远场风洞中部支架干扰,并基于表面压力系数差异为准则尝试对近场干扰量进行分解。研究得到如下结论:马赫数0.6时,远场支撑阻力系数和俯仰力矩系数的干扰量约占总支撑干扰量的30%,升力系数约占20%;马赫数0.9、迎角2°时,阻力系数远场支撑干扰量占总支撑干扰量的40%,迎角18°时,远场支撑干扰使得涡破裂位置提前;马赫数1.5时,远场支撑干扰可以忽略;基于表面压力系数差异将支撑干扰量分解的方法在亚声速支撑干扰前传明显时不适用,在马赫数0.9、迎角2°时求得近场支撑干扰使得马赫数减小约0.02,迎角减小约0.1°,马赫数1.5时用此法求得马赫数和迎角的干扰量均约等于0。     

轴压开口圆柱薄壳屈曲分析与试验

开口圆柱薄壳结构的轴向承载能力和稳定性分析是空间薄壁管式伸展机构(STEM,Storable Tubular Extendable Member)设计的关键问题之一.基于特征值屈曲分析方法,研究了轴压铍青铜开口圆柱薄壳结构在两端固支条件下的屈曲载荷与设计参数间的关系,利用幂函数拟合的方法建立了一种轴压开口圆柱薄壳屈曲载荷模型.通过铍青铜开口圆柱薄壳轴向压缩试验对特征值屈曲分析和所建立的轴压开口圆柱薄壳屈曲载荷模型进行了验证.结果表明:特征值屈曲分析方法可用于各向同性材料开口圆柱薄壳结构在两端固支条件下的轴向承载能力与稳定性分析;使用轴压开口圆柱薄壳屈曲载荷模型计算各向同性材料的开口圆柱薄壳在两端固支条件下受轴压作用时的屈曲载荷,最大误差为21%.     

新型行波光调制器单脊波导的微波电路研究

设计了一种采用单脊波导作为微波电路的新型行波光调制器。分析计算了脊缝间距小于１．００ｍｍ的脊波导中的电场分布、截止波长、频带宽度和特性阻抗；设计了与矩形波导联接的过渡段。结果表明：采用单脊波导作为光调器将使微波电场得到充分的利用，将提高调制效率；使波导单模工作频带增宽；具有较低的特性阻抗；通过过渡段易与矩形波导联接及保证单模传输。最后，经论证选择了切实可行的脊波导各几何参数ａ＝１３．００ｍｍ，ｂ＝１０．１６ｍｍ，ｄ＝０．５０ｍｍ，ｓ＝１．００ｍｍ。     

“中青年教育研究基金”管理初探

"中青年教育研究基金"课题，是民航学院科研工作普遍展开的一个侧重面。简要地分析了"中青年教育研究基金"设立后的现状和存在的问题；重点探讨了科学选题与充分论证是提高课题申报水平和完成率的关键；提出了在加深认识的同时，应采取措施从管理上增大工作保障的力度。通过提高申报水平，加强管理，保证"中青年教育研究基金"课题的质量和圆满完成，使"中青年教育研究基金"课题走上一条健康发展的研究道路。     

Mutations in cauliflower and sprout broccoli grown from seeds flown in space

Cauliflower and sprout broccoli are widely planted vegetables particularly in Fujian Province, China. To study the mutation in these two types of vegetables induced from spaceflight, we flew the seeds on the 20th Chinese recoverable satellite which orbited the Earth for 18 days. After returning to the Earth, the cauliflower seeds were planted for two generations and the sprout broccoli seeds for one generation at the Xiamen Agriculture Research Institute. Of the 12 cauliflowers planted for the first generation, two showed significant phenotypical changes in both the size of the plant and the weight of the flower head. In addition, most of the space flown plants were found to be resistant to the black rot attack in the field. Cauliflowers planted for the second generation from the seeds in one of the two plants that displayed phenotypical changes in the first generation showed similar mutations. For the first generation of sprout broccoli, the rate of emergence from the flown seeds was lower than that of the control by 30%. No significant changes in the phenotype between the sprout broccolis planted from the flown seeds and the control were observed except one of the mutated sprout broccolis showed a change in the appearance in the lesser bud of the chief flower head. Results of the study demonstrated that DNA damages in some of the genes may have occurred in the seeds flown in space, and some of the changes in the genes may have inherited from the first to the second generation. The improved resistance to the black rot attack and increased size of the flower head are apparently beneficial.     

Comparing topside and bottomside-measured characteristics of the F2 layer peak

The ionospheric characteristics of the F2 layer peak have been measured with ionosondes from the ground or with satellites from space. The most common characteristics are the F2-peak density NmF2 and peak height hmF2. In addition to these two parameters this paper studies the F2-peak scale height. Comparing the median values of hmF2 and NmF2 obtained from topside and bottomside sounding shows good agreement in general. The Chapman scale height values for the F2 layer peak derived from topside profiles, H_m,top, are generally several times larger than H_m,bot derived from bottomside profiles.     

教练机用户技术资料体系的研究

在航空综合保障的活动中,技术资料作为法规性文件,对装备的使用和维修起着指导作用。本文全面系统地阐述了对国内的军机用户技术资料和国外用户资料体系;比较了各自的特点;并特别解剖了美军机的TO体系和国内K8教练机用户技术资料体系。探讨了以K8模式的资料体系对构建我国教练机用户技术资料体系的重要意义。首创国内航空企业按照美军标T.O体系、ATA标准、S1000D,并结合我国飞机使用和维护的实际情况;编制飞机用户技术资料的模式,对后续教练机技术资料体系的构建提供了有益的参考。     

Stability and shape analysis of relative equilibrium for three-spacecraft electromagnetic formation

The invariant shapes for close formation flying with inter-craft electromagnetic force ensure several potential space applications. However, the 6-DOF relative equilibrium problem has not been systematically investigated. This paper mainly analyzes the invariant shapes of relative equilibrium for the three-spacecraft electromagnetic formation, and studies the families of invariant shape solutions with real and constant magnetic moments as well as their linear stability. The problem is examined based on the full nonlinear coupled dynamic models for collinear and general triangular configurations. The relative equilibrium conditions are analyzed to determine whether an invariant shape do exist, and the corresponding families of invariant shape solutions are identified for static and spinning configurations respectively. Finally, the linear stability of such invariant shapes is numerically discussed, which have shown that most invariant shapes are unstable and controllable.     

基础力学中的素质教育方法探讨

论文结合基础力学教学活动,对如何通过素质教育教学来提高学生的学习兴趣、培养学生的学习能力及实践能力等方面进行了探讨,并对学生反馈的意见进行分析,指出了值得进一步探索的方向。