基于仿真分析的燃油箱结构设计

为了减小油箱在受压状态下的变形量分布,针对同一油箱设计了3种油箱底面结构,并通过仿真得到了油箱的变形位移分布云图,然后根据模拟结果分析了3种不同结构的变形趋势以及可能原因,最后分析了3种因素对油箱壁面位移的影响。结果表明:加钢带的方案为最优设计;油箱设计应尽量减少大平面结构;油液蒸气压对油箱壁面位移的影响最大。     

轨道检测车油箱强度分析

为了准确的模拟车辆运行中油体晃动及油体对油箱的冲击作用,以某线路检测车油箱的强度分析为例,对分析过程中油体荷载施加方法进行了研究,提出了一种既基本符合车辆在各种工况下,油体对油箱施加荷载的实际情况,又非常简单可行的加载方法．运用这种方法,很好的完成了油箱的强度计算．根据计算结论,也对这种油箱的设计提出了一些建议．     

混合动力汽车燃油箱压力问题解决方案

针对混合动力汽车在纯电动行驶模式时燃油箱压力不断升高的问题,在一些高端车型上最近采用了一种叫做压力油箱电子控制系统的新技术。本文介绍了压力油箱的结构,并深入解析了压力油箱电子控制系统的电子控制原理。     

汽油车加油排放影响因素分析

通过对影响汽油车加油排放的外界环境（雷德蒸汽压）、裹入的空气速率和油箱的温度以及蒸发质量分数等主要因素进行分析,发现加油排放速率随空气的裹入速率和油箱的温度的变化呈线性关系;在给定的蒸发质量分数的条件下,汽油蒸汽压力的自然对数与温度的倒数呈线性关系;通过比较发现,车载汽油蒸汽回收装置的回收效率达93.9%以上.研究结果表明,可以通过降低雷德蒸汽压、降低空气的裹入速率和油箱的温度等途径来实现减少加油过程的排放.     

0.337715 一汽丰田全新PURIS普锐斯

普锐斯的油箱容量是45L,按照现在93号汽油7.85元的价格,加满普锐斯的油箱需要353.25元。普锐斯的综合工况百公里油耗4.3L,按照这个完美的数据,普锐斯一箱油可以行驶1046km。也就是说,普锐斯行驶一公里,你只需要支付0.337715元,如果你打算驾驶它行驶20万公里,你所支出的油费最低为67543元。     

轮胎式推土机的转向系统

介绍了轮胎式推土机的转向系统。转向系统由转向器、供需阀、油泵、油缸、油箱及管路等部件组成。     

嗅味辨故障

正有的车辆在行驶中,会散发出某些异味,作为驾驶人的您就一定要注意了,这必定是车辆的哪个部位发生了故障。当嗅到异味时,要根据不同的异味,有针对性地进行排查,并对故障及时修理。一、汽油味车辆在长时间使用后,输油管路会发生老化龟裂,稍有震动或管路内压力发生变化,燃油就有可能从这些部位渗漏出来。另外,如果油箱受到拖底等意外撞击,同样也会使油箱中的汽油发生渗漏。当驾驶人嗅到异常     

挑战哈雷

Exoelsior-Henderson:第一辆能跑到160公里／小时的摩托；第一个环游地球的摩托，第一个采用现今流线水滴形油箱，低位座椅的摩托，现在将以它辉煌的历史开始挑战Harley。     

玩转车生活 炫彩自驾游——自驾游征文

汽车是不是已经变成了你生活的一部分,成为不可或缺的伙伴?而开着爱车去旅游是不是也成为了你生活的一部分?开上爱车,加满油箱,带上帐篷,离开城市,走进自然……将一路的点点滴滴记录下来,与所有人分享。     

电车供电系统中的电容器常见故障及防范

1 常见故障 (1)渗漏油.由于焊接工艺不良或意外碰撞而引起电容器油箱焊缝和套管连接等地方发生渗漏油现象,必须及时处理.否则,由于密封遭到破坏,空气、水分或其它一些杂质会侵入容器内部,危害极大.     

Primary Research on Real-Time Fault Diagnosis Platform for Fuel Tank System of an Aircraft

Sub-tanks in fuel tank systems of aircrafts transfer fuel to engines in certain order. These sub-tanks and attached tank-accessories affect each other, and make fault diagnosis in such systems rather difficult. Without real measured data, this paper analyzes fault modes and fault effects of the fuel tank system, including its tankaccessories, of a given aircraft. Fault model of the system is built theoretically, and fault diagnosis criteria are deduced. Such criteria are then quantified to train a back propagation neural network(BPNN) as fault diagnosis model. To realize fault diagnosis of the real fuel tank system, a real-time fault diagnosis platform based on Lab View and Vx Works to perform this diagnosis method is discussed. This platform is a technical groundwork for fault diagnosis in real fuel tank systems.     

基于双线性差值法的船舶燃油加装精确计算方法

随着燃油价格的不断上涨,燃料费用在船舶营运费用中所占的比例越来越大。船舶营运方正逐渐加强对燃油管理各个环节的控制。保证加装燃油时有足额的燃油进油舱,是降低燃油费用的有效途径之一。要进行科学、严谨的舱容测量,需要对传统的测量方式和测量习惯进行修正,并充分考虑各种因素对油舱测量的影响,尤其是在使用舱容表时,应该用插值法来代替传统的粗略估算法,以精确计算燃油的加装数量。     

液化气体蒸气爆炸事故机理研究进展

结合近年来发生的一系列液化气体蒸气爆炸事故，对液化气体蒸气爆炸的事故机理进行了分析．总结了国外的一些实验成果，结合国内的理论研究现状，对储液罐受火焰包围情况、罐体破裂泄漏失效情况和受到冲击振动而引起爆炸的情况进行了机理分析，尤其是针对储液罐在受到冲击振动情况下的爆炸机理进行了详细的阐述，并提出了进一步的研究方向。     

潜艇内置式调整水舱的有限元计算

内置式调整水舱属于耐压液舱,而耐压液舱是耐压结构中最复杂的结构.参照前苏联的“耐压液舱强度和稳定性的计算方法”,设计了单壳体潜艇的内置式调整水舱的新结构形式,确定了主要参数,并在耐压液舱承受与舷外水相等的压力时,对内置式调整水舱区域的耐压船体、耐压液舱壳板、实肋板等结构进行了有限元计算.     

Study on launch dynamics of the tank marching fire

As an army main battle equipment, it is required that the tank should have high firing accuracy and high first round hit probability during marching. The initial disturbance of the projectile is the premier factor that takes effect on the marching fire accuracy of the tank. And the marching fire accuracy of the tank depends on the launch dynamics behaviors of the tank. In this paper, the launch dynamics theory of a tank marching fire is studied, and its launch dynamics model is established. Based on the transfer matrix method for multibody system(MSTMM) and the automatic deduction theorem of overall transfer equations, the overall transfer equation and the overall transfer matrix of a tank multibody system are deduced; the launch dynamics equations of the tank marching fire are deduced, and the dynamic response of the tank system, the motion of projectile in barrel, the initial disturbance of the projectile and the vertical target dispersion are exactly simulated; meanwhile, the results of simulation are verified by tests. This work provides both theoretical foundation and simulation approaches for improving the marching fire accuracy of the tank.     

基于多物质ALE的列车水箱晃动三维模拟及箱壁动应力研究

列车中水箱晃动问题是典型的流固耦合非线性行为,同时也涉及到多相流之间的相互耦舍问题．基于多物质ALE（ArbitraryLagrange—Euler）方法建立了列车水箱晃动三维数值模型,数值模型求解采用考虑流固耦合负载平衡的区域分解并行计算技术,分析列车制动工况下水箱中水的大幅晃动及箱壁动态应力变化行为．分析结果表明,制动减速度超过0．8m／s2时水箱应力峰值呈非线性增大趋势;储水量增加,水箱最大应力相应增加;水箱中设置防波板,可明显降低水流对箱壁的冲击作用．     

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为了重现和预演铁路危险货物罐车配置方案与风险水平之间的动态关系,在对铁路危险货物罐车运输系统进行成本分析和风险分析的基础上,针对铁路危险货物罐车数量与来源结构、系统风险与成本及运输需求等因素间的多重反馈关系,采用系统动力学方法建立了基于风险控制的铁路危险货物罐车优化配置仿真模型,并进行了仿真实例分析。仿真结果证明,该模型可以直观地反映出系统各变量在不同风险水平下的动态变化趋势,有望用于在一定的可接受风险水平下的铁路危险货物罐车配置方案比选和在一定铁路危险货物罐车配置条件下的风险水平预测。     

空重车混编对列车稳定性的影响

为了考察空重车混编列车的稳定性,建立了混编列车动力学模型,利用循环变量法解决了列车的"自由度爆炸"难题,利用模块化建模法解决了列车混合编组的建模难题,而且充分考虑了列车纵向、横向和垂向性能之间的耦合关系.利用新型的列车动力学模型,分析了空重罐车各种不同的编组形式对列车稳定性的影响.发现空罐车编组在列车尾部和头部时的稳定性较差,而编组在列车中部时的稳定性较好,因此在空重罐车混和编组时,为了提高列车稳定性,尽量把空罐车编组在列车的中部.     

Influence of excitation frequency on slosh-induced impact pressures of liquefied natural gas tanks

Liquid sloshing phenomena in No. 2 tank of 140 km³ liquefied natural gas (LNG) carriers have been studied numerically and experimentally. The scale of the model tank was selected as 1/55.9. Roll and pitch motions were tested. For measuring impact pressures, seventeen pressure sensors were installed on the tank model. A large number of excitation frequencies and filling heights were investigated. The experimental results showed that when the frequency of tank motion is close to the natural frequency of fluid inside the tank, large impact pressures may be caused. Resonance frequencies and maximum impact pressures of different filling height were presented. Among all the experimental situations, the maximum impact pressure always occurs at the place near 70% height of tank where should be especially concerned. A computational fluid dynamics (CFD) model was developed to simulate the sloshing in the tank. The model was based on the Reynolds-averaged Navier-Stokes (RANS) equations, with a standard κ-ɛ turbulence model. The volume of fluid (VOF) method was used to predict free surface elevations. Dynamic mesh technique was used to update the volume mesh. Computations for pressure time histories and peak pressures were compared to experimental results. Good agreement was observed.