主动导向转向架的多体动力学仿真与试验研究

对主动导向转向架的半车模型进行了多体动力学计算,并进行了滚动台试验,计算结果和试验结果基本一致。将半车模型扩展为整车模型后,进行了计算分析,研究结果表明,主动导向转向架可以大大提高转向架的曲线通过性能。     

牵引变电所换相连接方式研究

针对石家庄西变电所施工改造中,2008年3月发生的变电所母线和变压器换相连接问题,利用理论和测试的方法进行了分析,找出了原因。同时结合运行和施工中其他2例换相故障,提出了几项切实可行的措施。     

网络服务技术在轨道交通综合监控系统中的应用

针对在轨道交通综合监控系统开发中各承包商所面临的选择开发平台及开发语言的困扰问题,提出了采用Web Services(网络服务)技术来解决。首先分析了Web Services中的两大关键技术:WSDL(网络服务描述语言)和SOAP(简单对象访问协议)。然后,以集成闭路电视系统为例,规划了系统总体架构。最后,通过反复研究和测试,解决了系统开发中的关键问题:Web Services与综合监控系统之间的通信,并成功地应用到了深圳地铁3号线的综合监控系统项目开发中。     

编组站系统能力协调度的计算分析

以编组站实际作业过程为研究背景,基于编组站车流到达的不均衡性,将每一时段[ti-1,ti)的车流输入强度划分为3种不同的到达状态,结合对车流状态及编组站各系统能力的分析,得出编组站系统作业能力的协调度计算公式,最后,根据某编组站的实际车流量,计算出该编组站车流密集到达状态下的系统协调度。实例计算分析表明:所得出的协调度计算结果能够反映出编组站系统能力协调的薄弱环节,为提高编组站整体作业能力提供了一种新的方法。     

正交异性板疲劳裂纹夹芯板加固方案的力学分析

通过有限元软件中多种单元的尝试,得到了正交异性板桥面裂纹的夹芯板加固方法中夹心层的合理的有限元模拟方式,进而对正交异性板夹芯加固进行了有限元分析,得到了夹芯加固法的有效性,并对夹心层材料的弹性模量进行了参数化分析,得出了此参数对夹芯加固效果的影响,最终提出了合理的裂纹加固方案。     

铁路建设项目环境影响后评价指标体系初步研究

在目前国内外研究现状的基础上,结合铁路建设项目的特点,初步建立了以生态环境、噪声与振动环境、电磁环境、水环境、大气环境、固体废弃物和社会环境等7个互为关联和补充环境因子构成的铁路建设项目环境影响后评价指标体系,并利用构建的指标体系对成都至都江堰铁路环境影响后评价进行了分析。     

激光堆焊工艺在修造领域的应用现状及发展趋势

本文详细阐述了激光堆焊工艺在工业修造领域的应用现状及发展趋势,介绍了激光束的能源、输送和聚焦系统、堆焊材料及激光设备。重点说明了其在修造领域的应用工艺。     

供需链环境下提高企业订单执行效率分析

在企业的生产、管理过程中,如何提高订单执行力的研究仍是一个空白。此文针对当前制造业生产环境存在的主要问题,即生产面临复杂的环境、市场变化的不确定性导致激烈的市场竞争、订单执行过程的协调性较差,进行分析与探讨,提出提高企业订单执行力的方法和可采取的4个方面的措施,从而建立起一套在供需链管理模式下的高效订单执行力体系,使企业快速拓展市场,实现增值和稳步发展。     

A simple formulation for predicting the ultimate strength of ships

The aim of this study is to derive a simple analytical formula for predicting the ultimate collapse strength of a single- and double-hull ship under a vertical bending moment, and also to characterize the accuracy and applicability for earlier approximate formulations. It is known that a ship hull will reach the overall collapse state if both collapse of the compression flange and yielding of the tension flange occur. Side shells in the vicinity of the compression and the tension flanges will often fail also, but the material around the final neutral axis will remain in the elastic state. Based on this observation, a credible distribution of longitudinal stresses around the hull section at the overall collapse state is assumed, and an explicit analytical equation for calculating the hull ultimate strength is obtained. A comparison between the derived formula and existing expressions is made for largescale box girder models, a one-third-scale frigate hull model, and full-scale ship hulls.List of symbols A _B total sectional area of outer bottom - A _B total sectional area of inner bottom - A _D total sectional area of deck - A _S half-sectional area of all sides (including longitudinal bulkheads and inner sides) - a _s sectional area of a longitudinal stiffener with effective plating - b breadth of plate between longitudinal stiffeners - D hull depth - D _B height of double bottom - E Young's modulus - g neutral axis position above the base line in the sagging condition or below the deck in the hogging condition - H depth of hull section in linear elastic state - I _s moment of inertia of a longitudinal stiffener with effective plating - l length of a longitudinal stiffener between transverse beams - M _E elastic bending moment - M _p fully plastic bending moment of hull section - M _u ultimate bending moment capacity of hull section - M _uh ,M _us ultimate bending moment in hogging or sagging conditions - r radius of gyration of a longitudinal stiffener with effective plating [=(I _s /a _s )^1/2] - t plate thickness - Z elastic section modulus at the compression flange - Z _B ,Z _D elastic section modulus at bottom or deck - slenderness ratio of plate between stiffeners [= (b/t)(_y/E)^1/2] - slenderness ratio of a longitudinal stiffener with effective plating [=(l/r)(_y/E)^1/2] - _y yield strength of the material - _yB , _yB , _yD yield strength of outer bottom, inner bottom - _yS deck, or side - _u ultimate buckling strength of the compression flange - _uB , _uB , _uD ultimate buckling strength of outer bottom - _uS inner bottom, deck, or side     

Uncertain demand,modal competition and optimal price-capacity adjustments in air transportation

A new microeconomic model for the operation of an airline facing modal competition with uncertain total demand is developed to analyze optimal price capacity combinations. The novelty is the treatment of the capacity restriction, which is not viewed as affecting negatively individual preferences (e.g. probability of a full flight), but does influence aggregate utility. A mode choice model is used to represent unrestricted individual preferences assuming full availability (phone call demand); air capacity is treated as a variable that acts on the actual choice set. Restricted choices and total demand stochasticity are integrated in welfare calculations (users' benefits and profits). Numerical examples are given and results are analyzed in terms of load factors fare levels, and sensitivity to the stochasticity of requests.This research was partially funded by FONDECYT, Chile, Direction Génerale de l'Aviation Civile, France, the Andes Foundation and the Fulbright Commission.