海流能轮机叶片翼型的水动力学特性模拟

基于卧式海流能发电装置,采用雷诺平均N-S方程,对来流攻角从0°~26°情形下的叶片翼型进行数值模拟,分析比较不同攻角下水动力学特性的变化规律。结果表明:一定范围内增加攻角可有效提高升阻比,但升力系数最大时,升阻比、水翼捕能效率不一定最高,失速角也不一定是最佳攻角,验证了水翼失速的根本原因是边界层的分离;水翼吸力面与压力面的压差较大,此压差为水翼提供较高的升力系数,主要来自于水翼的前半部。此外,还分析了水翼周围流场的速度分布、压力分布等水动力特性与攻角的关系,为设计高效的海流能转换叶片提供了理论参考。     

港珠澳大桥建设对珠三角地区物流业的影响

港珠澳大桥将改变珠江口东西两岸之间的空间运输联系方式,从而改变整个珠三角地区的物流格局.从珠三角地区城市空间布局结构、产业特点出发,总结珠三角地区物流业特点,对港珠澳大桥影响珠三角物流格局的途径进行介绍；并逐一分析港珠澳大桥建成后对香港、深圳、珠海等珠三角主要城市物流业的不同影响.     

改进的锤击法测量原点阻抗

机械阻抗是机械系统特性的集中参数表示, 是解决机械系统耦合问题的一个重要工具。现有的机械阻抗方法有激振器激振传感器,冲击锤敲击实验结构等方法,但都有各自的局限性。本文提出了改进的锤击法测量原点阻抗。通过实验对比,对其可行性进行了研究,证明了此种方法可以快速并较为准确的获得结构的原点阻抗,具有工程实用性。     

计及移相角的多边形自耦变压器12脉波整流系统分析

多边形自耦变压器一定程度上减小了整流系统的体积,节约了变压器制造成本。为使多边形自耦变压器输出较大的二次侧电压值,优化多边形自耦变压器移相角,分析多边形自耦变压器移相角对12脉波整流系统输入侧电流谐波总畸变率,输出侧电压纹波系数,变压器、平衡电抗器、零序电流抑制器等效容量的影响;对比移相角在π/6、π/2时各个参数的值;提出适用于升压场合的多边形自耦变压器升压移相角;仿真实验验证了理论分析的正确性。同匝比时,多边形自耦变压器采用新移相角其输出电压幅值约为输入电压幅值1.4142倍,等效容量约为62.8%,较传统隔离式变压器等效容量小约37.2%。     

基于有限元分析的船用配电板抗冲击设计

本文介绍某船配电板抗冲击设计。通过对现有冲击计算方法的理论分析,选取了一种适合某配电板冲击仿真的计算方法并对配电板研制阶段进行了抗冲击性能分析及优化,减小了系统冲击响应。产品在国家标准要求下进行了冲击试验,实验结果满足工程设计实际需求,为后续同类产品设计及优化提供了理论支撑与设计参考。     

船用EH36高强钢无缝药芯焊丝焊接接头组织和冲击韧性研究

本文以SRSF501无缝药芯焊丝在船用EH36高强钢中的焊接应用为目的,研究了国产无缝药芯焊丝SRSF501在船用EH36高强钢焊接中的组织和冲击韧性。通过试验表明：SRSF501焊接EH36钢接头各区域的冲击性能均满足船级社要求；多层多道焊时,焊缝组织由粗大的柱状组织和细小的等轴晶组织组成,底层焊缝和末道焊缝柱状晶区域较大；盖面层两侧接头热影响区存在粗晶区,其它位置接头的热影响区不存在粗晶区；焊接接头中熔合线外2mm处,晶粒最细,冲击韧性最好。     

悬挂式单轨平面圆曲线乘客舒适度控制标准取值研究

乘客舒适度标准是确定线路平纵断面设计参数最为重要的控制指标,也是必须满足的强制性指标。为合理平衡乘客舒适度与工程建设成本之间的跷跷板关系,通过系统总结国内外各种现有制式取值标准,就悬挂式单轨乘客舒适度控制标准取值开展理论分析研究,并提出相应建议。与平面圆曲线半径相关的乘客舒适度指标为车体偏转角及未被平衡离心加速度,随着偏转角和未被平衡离心加速度数值的增加,其对最小圆曲线半径的影响逐渐减弱,恶化舒适度条件并不完全等同于工程效益的减小。悬挂式单轨最大偏转角理论上可突破传统轮轨铁路7.7°的限制,但增大偏转角对限界造成的影响不可忽略。人体可忍受的振动持续作用时间与未被平衡离心加速度大小成反比,将加速度控制在0.4～0.8 m/s~2是合理的。     

冲压机械振动对高铁桥梁及行车动力影响分析

高速铁路桥梁的平顺性和稳定性对运营列车的平稳性和安全性有很大影响。为研究冲压机械产生的外部振动激励对高铁桥梁的影响,首先通过对此机械引起的地面振动进行实测,并结合有限元分析软件,确定最大冲击荷载作用下产生的地面振动及传播至桥墩处的振动;然后通过建立列车-轨道-桥梁耦合动力学模型,将桥墩处的地面振动作为激励输入,分析列车以不同速度通过时车辆、桥梁动力学响应。结果表明:地面冲击振动有限元模型计算结果与实测结果基本相符,验证了模型的可靠性;地面振动对桥梁响应会产生一定的影响,距振源50 m处地面振动对桥梁所产生的影响较距振源80 m处(桥墩处)的大,但对运行车辆的影响很小;随着车速由250 km/h至350 km/h,车辆及桥梁各结构的动态响应均有所增大,但都未超出安全限值。因此,冲压机械冲击作用导致的地面振动对列车-轨道-桥梁系统动态服役性能影响非常有限。     

Fueling for contingencies: The hidden cost of unpredictability in the air transportation system

The aviation community is increasing its attention on the concept of predictability when conducting aviation service quality assessments. Reduced fuel consumption and the related cost is one of the various benefits that could be achieved through improved flight predictability. A lack of predictability may cause airline dispatchers to load more fuel onto aircraft before they depart; the flights would then in turn consume extra fuel just to carry excess fuel loaded. In this study, we employ a large dataset with flight-level fuel loading and consumption information from a major US airline. With these data, we estimate the relationship between the amount of loaded fuel and flight predictability performance using a statistical model. The impact of loaded fuel is translated into fuel consumption and, ultimately, fuel cost and environmental impact for US domestic operations. We find that a one-minute increase in the standard deviation of airborne time leads to a 0.88 min increase in loaded contingency fuel and 1.66 min in loaded contingency and alternate fuel. If there were no unpredictability in the aviation system, captured in our model by eliminating standard deviation in flight time, the reduction in the loaded fuel would between 6.12 and 11.28 min per flight. Given a range of fuel prices, this ultimately would translate into cost savings for US domestic airlines on the order of $120–$452 million per year.     

Can we reliably assess climate mitigation options for air traffic scenarios despite large uncertainties in atmospheric processes?

Air traffic has an increasing influence on climate; therefore identifying mitigation options to reduce the climate impact of aviation becomes more and more important. Aviation influences climate through several climate agents, which show different dependencies on the magnitude and location of emission and the spatial and temporal impacts. Even counteracting effects can occur. Therefore, it is important to analyse all effects with high accuracy to identify mitigation potentials. However, the uncertainties in calculating the climate impact of aviation are partly large (up to a factor of about 2). In this study, we present a methodology, based on a Monte Carlo simulation of an updated non-linear climate-chemistry response model AirClim, to integrate above mentioned uncertainties in the climate assessment of mitigation options. Since mitigation options often represent small changes in emissions, we concentrate on a more generalised approach and use exemplarily different normalised global air traffic inventories to test the methodology. These inventories are identical in total emissions but differ in the spatial emission distribution. We show that using the Monte Carlo simulation and analysing relative differences between scenarios lead to a reliable assessment of mitigation potentials. In a use case we show that the presented methodology can be used to analyse even small differences between scenarios with mean flight altitude variations.