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201.
Yuming Fu Hui Liu Lingzhi Shao Minjuan Wang Yu A. Berkovich A.N. Erokhin Hong Liu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Vegetable cultivation plays a crucial role in dietary supplements and psychosocial benefits of the crew during manned space flight. Here we developed a ground-based prototype of horn-type sequential vegetable production facility, named Horn-type Producer (HTP), which was capable of simulating the microgravity effect and the continuous cultivation of leaf–vegetables on root modules. The growth chamber of the facility had a volume of 0.12 m3, characterized by a three-stage space expansion with plant growth. The planting surface of 0.154 m2 was comprised of six ring-shaped root modules with a fibrous ion-exchange resin substrate. Root modules were fastened to a central porous tube supplying water, and moved forward with plant growth. The total illuminated crop area of 0.567 m2 was provided by a combination of red and white light emitting diodes on the internal surfaces. In tests with a 24-h photoperiod, the productivity of the HTP at 0.3 kW for lettuce achieved 254.3 g eatable biomass per week. Long-term operation of the HTP did not alter vegetable nutrition composition to any great extent. Furthermore, the efficiency of the HTP, based on the Q-criterion, was 7 × 10−4 g2 m−3 J−1. These results show that the HTP exhibited high productivity, stable quality, and good efficiency in the process of planting lettuce, indicative of an interesting design for space vegetable production. 相似文献
202.
It is difficult to quantitatively detect defects by using the time domain or frequency domain features of Lamb wave signals due to their dispersion and multimodal characteristics.Therefore,it is important to discover an intrinsical parameter of Lamb waves that could be used as a damage sensitive feature.In this paper,quantitative defect detection in aluminium plates is carried out by means of wavenumber analysis approach.The wavenumber of excited Lamb wave mode is a fixed value,given a frequency,a thickness and material properties of the target plate.When Lamb waves propagate to the structural discontinuity,new wavenumber components are created by abrupt wavefield change.The new wavenumber components can be identified in the frequency-wavenumber domain.To estimate spatially dependent wavenumber values,a short-space two-dimensional Fourier transform(FT)method is presented for processing wavefield data of Lamb waves.The results can be used to determine the location,size and depth of rectangular notch.The analysis techniques are demonstrated using simulation examples of an aluminium plate with a rectangular notch.Then,the wavenumber analysis method is applied to simulation data that are obtained through a range of notch depths and widths.The results are analyzed and rules of the technique with regards to estimating notch depth are determined.Based on simulation results,guidelines for using the technique are developed.Finally,experimental wavefield data are obtained in aluminium plates with rectangular notches by a full noncontact transceiving method,i.e.,laser-laser method.Band-pass filtering combined with continuous wavelet transform is used to extract a certain frequency component from the full laser-induced wavefield with wide band.Shortspace two-dimensional FT method is used for further processing full wavefield data at a certain frequency to estimate spatially dependent wavenumber values.The consistency of simulation and experimental results shows the effectiveness of proposed wavenumber method for quantitative rectangular notch detection. 相似文献
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204.
介绍了波纹板成型模数控加工工艺方法及特点,详细论述了数控加工的优点,并结合实例进行工艺方案分析。实践证明,该项加工技术不仅加工质量好,且大大提高了生产效率,降低了生产成本。 相似文献
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206.
刘佳颖 《中国民航飞行学院学报》2014,(4):48-49
对空中乘务人员的素质要求越来越高,其中要求最高的就是在英语能力方面。本文基于在让乘务专业学生学习专业知识的同时,如何更有效地提高他们的英语水平,简要阐述了目前这方面教学的现状,分析了空乘专业的课程设置,并对如何实施双语教学提出了几点对策。 相似文献
207.
激光有源干扰是目前光电干扰领域发展的热点,如何对其实现成功防御是一个重要课题。主要讨论了激光有源干扰的各种防御措施,重点是激光测距机和半主动激光制导武器的抗干扰措施、激光防护器材的防护原理以及新体制导弹的强激光防护技术。 相似文献
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209.
舰载飞机弹射滑跑起飞特性计算 总被引:3,自引:0,他引:3
给出舰载飞机从航空母舰上弹射滑跑起飞的动力学模型,基本解算方法和示例计算结果。考虑了起落架油液减震装置的柔性对起飞滑跑特性的影响,列出了起落架受力的数学模型和飞机纵向动力学方程,根据编制的计算机源程序,以典型的A-6舰载机为算例,给出在整个弹射滑跑起飞过程中的a,x,x,y和y等弹射运动参数的动态反应特性。 相似文献
210.
本文应用广义阶梯函数对承受边缘弯矩和局部线性分布荷载的筒支圆板进行塑性极限分析,文中考虑了局部线性分布荷载的4种可能分布形式,给出了简支圆板在Tresca屈服条件下边缘弯矩和线性荷载所满足的关系式。 相似文献