吸气式PDE中心锥鳞片阀工作原理与试验研究

为了增强吸气式脉冲爆轰发动机进气阀的防倒流效果、缩短发动机的燃烧转爆轰时间,设计了中心锥鳞片阀(CCSV),并进行了中心锥鳞片阀(CCSV)与中心锥钝体阀(CCBV)的对比试验研究。采用精细雾化喷嘴作为雾化装置,成功实现了10Hz工况下中心锥鳞片阀吸气式脉冲爆轰发动机的协调工作,爆轰波平均峰值压力为1.65MPa,爆轰波速度为1371m/s。研究结果表明:中心锥鳞片阀(CCSV)具有良好的单向阀功能,有效地防止了燃气倒流,缩短了燃烧转爆轰时间。相比于中心锥钝体阀(CCBV),燃烧转爆轰时间下降了19.03%。     

民用支线飞机的军用潜力分析

由于技术发展和现实需求两方面的原因,民用支线飞机的军用潜力日益受到世界各国的重视。首先简要分析了世界范围内支线飞机市场开拓受限以及各国军方对支线飞机平台提出需求的相关情况,然后从载机平台和任务设备两方面对支线飞机改型发展军用飞机的可行性进行了研究,最后对国外支线飞机的军用改型发展近况做了概括分析。     

高校工会履行教育职能的对策探究

教育是高校工会组织的一项重要社会职能。从实施高校工会教育职能重要性和必要性入手，分析高校工会教育职能的实施现状及其原因，探讨研究高校工会教育内容的模式，提出方法、对策。     

英语写作元认知能力培养

为了解决英语写作教学费时低效的问题,根据元认知理论框架对54名高职高专商务英语专业二年级的学生进行了行动研究。研究方法包括收集相关材料、制订并实施改进写作教学的行动计划、评估计划实施的效果。结果是绝大部分学生对本学期的写作教学和在写作方面取得的成绩表示满意。最后对研究过程和结果作分析,针对不足之处提出了改进办法,并提出了有待研究的新问题。     

The Zadko telescope: A resource for science education enrichment

This paper describes plans for employing a new fully robotic optical telescope in Western Australia, the Zadko telescope, for evaluating education-outreach. A key feature of the telescope is the optimized observation-scheduling program, developed by our French collaborators who operate the TAROT robotic telescope network. It provides a simple interface for requesting observation time remotely, and has the potential for school students to participate in real astronomical research. The University of Western Australia and Curtin University are commencing a study for evaluating changes in student perceptions of science by participation in our astronomy research. Other areas of interest include broadening the program to include access of students from European countries, and exploring how remote access astronomy can be used to encourage awareness between different cultures.     

Improvements in the re-flight of spaceflight experiments on plant tropisms

In order to effectively study phototropism, the directed growth in response to light, we performed a series of experiments in microgravity to better understand light response without the “complications” of a 1-g stimulus. These experiments were named TROPI (for tropisms) and were performed on the European Modular Cultivation System (EMCS), a laboratory facility on the International Space Station (ISS). TROPI-1 was performed in 2006, and while it was a successful experiment, there were a number of technical difficulties. We had the opportunity to perform TROPI-2 in 2010 and were able to optimize experimental conditions as well as to extend the studies of phototropism to fractional gravity created by the EMCS centrifuge. This paper focuses on how the technical improvements in TROPI-2 allowed for a better experiment with increased scientific return. Major modifications in TROPI-2 compared to TROPI-1 included the use of spaceflight hardware that was off-gassed for a longer period and reduced seed storage (less than 2 months) in hardware. These changes resulted in increased seed germination and more vigorous growth of seedlings. While phototropism in response to red illumination was observed in hypocotyls of seedlings grown in microgravity during TROPI-1, there was a greater magnitude of red-light-based phototropic curvature in TROPI-2. Direct downlinking of digital images from the ISS in TROPI-2, rather than the use of analog tapes in TROPI-1, resulted in better quality images and simplified data analyses. In TROPI-2, improved cryo-procedures and the use of the GLACIER freezer during transport of samples back to Earth maintained the low temperature necessary to obtain good-quality RNA required for use in gene profiling studies.     

Proportional fuzzy feed-forward architecture control validation by wind tunnel tests of a morphing wing

In aircraft wing design, engineers aim to provide the best possible aerodynamic performance under cruise flight conditions in terms of lift-to-drag ratio. Conventional control sur-faces such as flaps, ailerons, variable wing sweep and spoilers are used to trim the aircraft for other flight conditions. The appearance of the morphing wing concept launched a new challenge in the area of overall wing and aircraft performance improvement during different flight segments by locally altering the flow over the aircraft's wings. This paper describes the development and appli-cation of a control system for an actuation mechanism integrated in a new morphing wing structure. The controlled actuation system includes four similar miniature electromechanical actuators dis-posed in two parallel actuation lines. The experimental model of the morphing wing is based on a full-scale portion of an aircraft wing, which is equipped with an aileron. The upper surface of the wing is a flexible one, being closed to the wing tip; the flexible skin is made of light composite materials. The four actuators are controlled in unison to change the flexible upper surface to improve the flow quality on the upper surface by delaying or advancing the transition point from laminar to turbulent regime. The actuators transform the torque into vertical forces. Their bases are fixed on the wing ribs and their top link arms are attached to supporting plates fixed onto the flex-ible skin with screws. The actuators push or pull the flexible skin using the necessary torque until the desired vertical displacement of each actuator is achieved. The four vertical displacements of the actuators, correlated with the new shape of the wing, are provided by a database obtained through a preliminary aerodynamic optimization for specific flight conditions. The control system is designed to control the positions of the actuators in real time in order to obtain and to maintain the desired shape of the wing for a specified flight condition. The feasibility and effectiveness of the developed control system by use of a proportional fuzzy feed-forward methodology are demon-strated experimentally through bench and wind tunnel tests of the morphing wing model.     

螺旋管成形模具的CAD/CAM方法研究

针对螺旋管成形模具的特点,采用Pro/Engineer进行三维实体设计、PowerMILL进行数控编程的设计制造方法,充分发挥Pro/Engineer三维实体的参数化设计和PowerMILL刀具路径轨迹优化的优势,缩短了螺旋管成形模具的设计制造周期,提高了螺旋管成形模具的加工精度。     

复合式气冷涡轮导叶综合冷效试验研究

介绍了复合式气冷涡轮导叶的冷却效果试验研究。试验结果表明，导叶在宽广的冷气流量比范围内，具有良好的冷却特性，经模化分析，在发动机状态下，叶片中截面相对冷却效果为0．69，达到了设计指标。     

三级轴向旋流器影响燃烧室性能的试验

对装有4种不同三级轴向旋流器的燃烧室开展了常压下不同进口速度、进口温度和油气比状态下的燃烧室性能试验研究,获得了不同三级轴向旋流器燃烧室的流阻性能和燃烧性能.研究结果表明:各方案中三级轴向旋流器燃烧室的总压损失系数均随着进口速度的增大(由40m/s增加到70m/s)而增加;进口温度的升高对点火和熄火均有利;旋向组合为顺时针—逆时针—顺时针的三级轴向旋流器燃烧室性能与旋向组合为逆时针—逆时针—顺时针的三级轴向旋流器燃烧室燃烧性能相比,总压损失系数稍大、贫油熄火性能较优、燃烧效率稍低;内旋流器空气流量的减少可使得三级轴向旋流器燃烧室的总压损失系数增大、贫油熄火油气比和燃烧效率均有所降低.