乘用车DCT车型的动力性提升分析与实施

为满足公司的发展战略要求,需要打造一款高性能、运动操控性车型,为提升该款乘用车DCT车型的动力性和操控型,分别从车辆的起步、加速过程的扭矩发挥和换挡结束的扭矩恢复、换挡过程的扭矩交替时间和转速同步时间、换挡线加速度和动力升挡换挡线及硬件五个方面进行优化。论文对该车型的起步加速过程以及换挡过程的扭矩控制进行详细分析,并将五个优化方向分解为13个子项,分别对各子项优化效果进行分析,通过INCA软件对车辆的控制系统进行优化,经过实际道路测试满足了目标开发要求。     

PHEV能量管理策略研究

针对一款串联型插电式混合动力公交车,文章基于MTLALB建立整车和各部件数值模型。在中国典型城市公交工况下,建立基于全局优化的DP策略,并与CD-CS策略和PMP策略进行能耗对比分析。结果表明:(1)基于CD-CS策略的后期SOC在一定范围内波动,DP策略与PMP策略的SOC轨迹近似呈线性变化。(2)CD-CS策略较DP策略的能耗成本高22.68%,PMP策略比DP策略的能耗成本高0.30%。DP策略与PMP策略可以合理分配能量源,实现全局最优,但DP策略相比PMP策略计算量大。     

A signal decomposition method based on repeated extraction of maximum energy component for offshore structures

Contrary to most signal decomposition methods that usually decompose an original signal into a series of components simultaneously, a novel approach based on repeated extraction of Maximum Energy Component (MEC) is proposed. The approach starts from determination of the MEC referring to the estimated Power Spectral Density (PSD) function, and then represents the MEC by employing an exponential function to fit the original signal. By defining a stopping criterion based on two adjacent estimated PSDs, each MEC can be accurately extracted with an improved performance throughout the entire signal decomposition. To verify the proposed method, a single degree-of-freedom system subject to harmonic loads has been examined. Numerical results show that the analytical response can not only be decomposed into four MECs corresponding to the excitation and the system, respectively, but also provide an accurate estimation of natural frequency and damping ratio of the system. Meanwhile, by observing results from the Ensemble Empirical Mode Decomposition (EEMD), Variational Mode Decomposition (VMD) and Prony based on state-space model (Prony-SS), an improved decomposition accuracy has been achieved from the proposed approach. Furthermore, experimental data from the Norwegian Deepwater Programme and two sets of field-test data from one fixed offshore platform and an offshore wind turbine have been used to demonstrate the correctness of the developed signal decomposition method. It is noted that divergence in results by Prony-SS can be observed when a very large model order is used, while the proposed method provides the better decomposition and reconstruction of signals.     

微机控制的船用发电机继电保护实验装置

由于微机控制的继电保护与常规保护比较起来有许多优点,因此微机控制的船用发电机继电保护实验装置有其取代原有实验装置的必要性。本文就微机控制的船用发电机继电保护实验装置的硬件结构、软件算法和软件抗干扰技术进行了探讨。     

汽车动力总成弯曲振动应力响应及其激励灵敏度分析

本文利用文献（５）建立的汽车动力总成弯曲有限元分析模型，计算分析离合器壳的动应力响应，并考察了动应力关于不平衡质量位置的灵敏度，对计算分析进行了实验验证。     

基于结构疲劳动态可靠性分析的船舶结构概率损伤容限设计

本文根据结构可靠性理论，提出了一种基于结构疲劳动态可靠性分析的损伤容限分析方法，给出结构疲劳裂纹随机扩展过程中疲劳寿命分布和结构疲劳可靠性的表达式。在给定与疲劳寿命有关的各参数条件下求得动态可靠性曲线，从而在结构设计中根据可靠性要求确定或选择设计参数。     

机车车辆动力学研究及发展

机车车辆动力学在最近10年得到迅速发展,考虑车辆—轨道耦合作用的耦合模型得到广泛应用。随着大跨距跨江铁路桥的建设,车和桥的耦合振动会引起接触网的振动,进而影响弓网的耦合振动。因此十分有必要开展接触网—受电弓—机车车辆—线路—桥梁耦合大系统动力学的研究。进行机车车辆动力学性能优化,必须首先确定机车车辆动力学三要素的优先关系,即运行的稳定性—安全性—平稳性,建立以列车为研究对象的模型,同时在模型中考虑机车车辆结构弹性和频变特征悬挂参数以及气流扰动的影响,进而进行灵敏度分析和参数优化。给出考虑频变特性的钢弹簧等效计算方法以及基于循环变量的列车系统动力学建模和计算方法,并验证了计算方法的有效性。     

自适应神经网络用于船舶动力定位系统

船舶动力定位（DP）采用一种控制系统驱动装在船上的侧推器和尾部推进器或者几个全回转的推进器，使船定位在海平面的要求位置上。船受到风、浪及流等海洋环境力的作用时会漂移离开原位置，传统的控制方法是采用PID（比例、积分、微分）反馈控制。顾和李（1994）提出了一种新的基于人工神经网络的控制方法，它具有许多优越性：①一个可随意调节的目标函数以适合不同的需求──定位精度高或节约定位能量后前馈控制并能自适应于不同的环境力变化包括非线性的波浪漂力；本文在目标函数中引入了与速度相关的项，从而提高控制质量。这一方法也可用于自动驾驶船舶沿设定的轨迹航行。计算机模拟结果表明本方法能达到很好的控制效果。     

牙周炎患者红细胞免疫功能及发病机理研究

采用酵母菌花环试验对31例牙周炎患者红细胞免疫粘附功能、循环免疫复合物、补体C_3含量进行了检测,并与正常组进行了比较。结果显示:牙周炎患者红细胞膜免疫复合物及循环免疫复合物均升高,补体C_3含量降低,且皆与正常组有显著性差异。作者认为:免疫复合物在牙周炎发病机理中有一定的意义,牙周炎患者红细胞免疫对清除循环免疫复合物起着重要作用。     

Experimental ivnestigation on flow fields of viscous fluid around two-dimensional wings and comparison with computational results

To examine the flow field of a viscous fluid around the trailing edge of a wing with respect to the Kutta condition or the Joukowski hypothesis, an experimental investigation into the velocity fields around two-dimensional (2D) wings NACA0012 and NACA4412 was carried out using an X-type hot-wire anemometer in a wind tunnel and the method of colored milk injection in a circulating water channel. The results of these investigations revealed that the flow of a viscous fluid at the trailing edge of a 2D wing is tangential to the face on the pressure side, and that the flow is very slow or reversed on the suction side due to separation when the angle of attack is greater than 7.5°. By flow visualization, a Kármán vortex street was found in the wake of both wings (NACA0012 and NACA4412) when the angle of attack was 5°. These results show that the ordinary Kutta condition with respect to the direction of outflow at the trailing edge is not necessarily satisfied in a viscous fluid, but the Kutta condition with respect to the pressure at the trailing edge is satisfied as usual. Numerical results, which have been obtained as the solution of Reynolds-averaged Navier-Stokes equations, show good agreement with above-mentioned experimental results. Therefore, CFD (Computational Fluid Dynamics) simulation has proved to be very effective for studying steady viscous flow around the trailing edge of a 2D wing.