基于UGNX4．0的整体叶轮曲面造型

应用三次B样条曲线对图纸所给的叶片中性面上的轴盘曲线和盖盘曲线上的离散数据点进行插值,得到轴盘曲线和盖盘曲线,将曲线上的对应点相连得到直纹面形式的叶片中性面;根据图纸给出的叶片上不同点的厚度值,构造轴盘曲线和盖盘曲线的左右偏置曲线,进而得到直纹面形式的叶片曲面.最后将计算所得数据导入UGNX4.0软件,应用此软件对整体叶轮进行实体建模.     

圆柱刀侧铣叶片曲面的刀位规划

依据叶轮叶片给出的初始型值点,利用四重节点的三次准均匀B样条插值方法,建立直纹面形式的叶片曲面.研究圆柱刀侧铣叶片曲面的刀位规划,利用两点偏置法进行初始刀位的确定,在此基础上,建立圆柱刀初始刀轴轨迹面在多点处逼近叶片曲面等距面的超定方程组,并利用求解线性最小二乘问题的豪斯荷尔德变换法求解,进行进一步的刀位优化,最后给出具体的计算结果.计算结果表明利用这一操作过程来进行圆柱刀侧铣叶片曲面的刀位规划是行之有效的.     

基于Bezier曲线法对径流式涡轮机动叶的设计

根据叶轮初步设计公式,结合Bezier曲线构造方法依靠NUMECA软件Design3D模块以径流向心式涡轮机效率0.5为目标值,对叶轮子午面型线以及动叶型线进行设计。并通过NUMECA软件对所设计的叶片以及子午流面进行流体计算,得出了符合效率目标值的叶型和子午流面参数,以及子午流面的绝对温度和绝对压力的分布,提出了以径流向心式涡轮机效率为目标值,结合Bezier曲线构造法的叶片型线和子午流面型线的设计方法。     

轴肩过渡曲线形状优化研究

将有限元分析与优化技术相结合，设计了轴肩过滤曲线形状优化软件，提出能在较大程度上降低轴肩过渡曲线应力集中的优化线型。     

涡轮叶片逆向建模与特征参数提取

为了在已有涡轮叶片实物基础上进行再创新设计,采用激光扫描仪对涡轮叶片进行数字化扫描,提出了在三维测量得到涡轮叶片点云数据的基础上,准确进行逆向建模、反求几何参数和提取气动特征参数的逆向设计方法.根据涡轮叶片的几何参数反求和提取气动特征参数要求,基于获取涡轮叶片的截面点云图,用五次多项式曲线拟合叶盆和叶背,并用圆弧逼近叶形前后缘.基于该方法,采用Matlab软件对涡轮截面线点云进行拟合,反求得到了叶身型线方程,拟合偏差控制在之内,能够获得准确的叶片截面型线和气动特征参数.      

双曲抛物面薄壳屋盖的制作与设计

为了方便双曲抛物面薄壳屋盖的制作,采用数学建模的方法对双曲抛物面薄壳屋盖进行理论计算,得到了直母线钢筋数以及直母线钢筋在空间的位置、锚固面方程以及与直母线交点、直母线之间的交点和直母线与锚固面的法线之间夹角的数学表达式。利用Matlab软件经过实例计算验证了其有效性,为今后双曲薄壳屋盖的制作提供了理论依据。     

交错轴齿轮的接触强度分析

建立了互相啮合的渐开螺旋面齿轮副的曲面方程和啮合线的曲线方程，以多种数学软件和CAD软件作为辅助工具，应用三维弹性非赫兹滚动接触理论分析了啮合线上各点的接触应力分布情况，包括了各种啮合参数对接触强度的影响，为交错轴齿轮副的强度设计方法提供了理论依据。     

基于CAXA软件的曲线台阶数控加工方法研究

本文以CAXA自动编程软件为基础,以泵盖曲线台阶面加工为例,研究平面轮廓加工法、参数线加工法、平面区域加工法和自动区域加工法,提出了该类台阶面数控加工的最佳方案。     

用激光位移传感器检测轮对踏面缺陷

介绍一种自动检测铁路车辆轮对踏面擦伤及剥离的新方法．该方法用激光位移传感器获得踏面数据，通过纠偏、插值和运用经典的数据处理的中值滤波和边界搜索等方法对数据进行分析；通过对数据矩阵进行数字化处理，得到了轮对踏面损伤结果．运用VC 和Mat1ab语言编制出通用分析软件，功能包括轮对踏面的二维和三维图形显示、打印踏面擦伤和剥离的损伤尺寸等．     

离心式风机叶片的一体化设计方法

在理解离心式风机叶片的成形机理及形状特点的基础上，借助先进的3D设计软件Pro／Engineer，将翼型风机叶片的建模、运算、绘图以及最后的下料全部由计算机实现一体化设计，最后得到精确的下料图纸，可大大简化传统的设计过程，提高了设计精度。     

Simulation Analysis on Polyurethane Coating of Wind Blade

The distribution regularities of stress and displacement in the interior and on the surface of polyurethane coating are analyzed by the software of finite element analysis with the condition that the polyurethane coating of wind blade is impacted by the sand particle with different velocities and angles. The analysis results indicate that at the same impacting angle, the coating produces plastic yield more easily when the velocity of sand particle is faster and the range of the yield area is connected with the contacting time; plastic deformation wear and cutting wear on the surface of polyurethane coating are concurrent but have different effects;the sand particle impacting the coating can produce large tensile stress on the surface of the coating which causes the coating cracks to occur easily; the shear stress is symmetrically distributed on both side of the contacting point, and the coating at the contacting points lower left and lower right can be easily damaged by the shear.     

无梢涡螺旋桨试验研究

本文根据螺旋桨的升力线理论,分析了螺旋桨叶梢产生梢涡的机理,通过在叶梢处的截面上安装一个与螺旋桨同轴旋转面相切的弧面封板所进行的螺旋桨敞水试验,来验证叶梢安装叶片可使叶梢不产生旋涡,减少叶梢处能量损失,得出了初步的结论。     

基于ANSYS的车辆液力缓速器叶片强度分析及模态分析

基于UG-NX2造型软件平台建立YJ-400型号液力缓速器三维几何模型,并对液力缓速器进行叶片的提取简化,利用ANsYsuG的数据接口将叶片导人ANSYS生成FEA模型,利用计算流体分析软件Fluent对液力缓速器的内流场进行数值模拟,得到叶片表面的液压载荷分布,利用ANSYs的载荷施加模块将工作液液体总压按线性分布施加于FEA模型,进行叶片强度分析求得叶片的变形量和等效应力分布;同时对只施加有位移约束的FEA模型进行前六阶模态分析,求得各阶振型的固有频率和共振时叶片的最大变形量．     

薄壁叶片加工误差分析与预测

薄壁叶片在数控加工中容易变形,影响加工精度,提出了采用柔性变形迭代方法计算叶片铣削过程中的变形量．首先利用正交切削仿真试验确定球头铣刀的铣削力模型,并给出叶片数控加工刀触点计算方法,再将切削力加载到叶片的有限元网格节点上,采用柔性变形迭代方法计算出薄壁叶片的变形量．结果表明,所提出的方法能有效地预测薄壁零件的变形,为叶片加工误差补偿提供了依据．     

非均匀流场中桨叶剖面设计方法

给出了非均匀流场中螺旋桨桨叶剖面的设计方法，提出了保持剖面空泡特征不变的等效运转曲线的思想，并创建了等效运转曲线的确定方法．基于等效运转曲线设计的桨叶剖面能有效地控制空泡范围和空泡类型，得到期望的空泡性能．剖面采用母型剖面方法来设计，进而可确定桨叶弦向环量分布，然后由升力面理论设计三维桨叶的几何形状．通过实例螺旋桨的设计，说明本方法是合理和有效的．     

Research on Dynamic Response Characteristics of 6MW Spar-Type Floating Offshore Wind Turbine

A 6 MW spar-type floating offshore wind turbine(FOWT) model is put forward and a fully coupled aero-hydro-servo-elastic time domain model is established in the fatigue,aerodynamics,structures and turbulence(FAST) code.Influence rules of wind load and wave load on the characteristics of 6 MW spar-type FOWT are investigated.Firstly,validation of the model is carried out and a satisfactory result is obtained.The maximal deviations of rotor thrust and power between simulation results and reference values are 4.54% and-2.74%,respectively.Then the characteristics,including rotor thrust,rotor power,out-of-plane blade deflection,tower base fore-aft bending moment,and mooring line tension,are researched.The results illustrate that the mean value of dynamic response characteristics is mainly controlled by the wind-induced action.For characteristics of tower base fore-aft bending moment and platform pitch motion,the oscillation is dominated by the wave-induced action during all conditions considered.For characteristics of out-of-plane blade tip deflection and mooring line tension,the oscillation is commanded by combination effect of wave and wind loads when the wind speed is lower than the rated wind speed(hereinafter referred to as below rated wind speed) and is controlled by the wave-induced action when the wind speed is higher than the rated wind speed(hereinafter referred to as above rated wind speed).As to the rotor thrust and power,the oscillation is dominated by the wind induced action at below rated wind speed and by the combination action of wind and wave loads at above rated wind speed.The results should be useful to the detailed design and model basin test of the 6 MW spar-type FOWT.     

叶顶间隙对喷水推进水力性能的影响

分别以设计参数相同的混流式喷水推进泵与轴流式喷水推进泵为对象, 基于剪切应力运输湍流模型、隐式多网格耦合算法与全结构化网格, 对4种不同叶顶间隙的水力性能进行数值模拟, 分析了叶顶间隙对喷水推进水力性能的影响, 研究了叶顶间隙影响程度与喷水推进器类型的关系。研究结果表明: 2种喷水推进泵的扬程、效率均随叶顶间隙增大而减小; 随着叶顶间隙的增大, 混流泵消耗功率先增大后减小, 当叶顶间隙为1.3mm时消耗功率最大, 而轴流泵消耗功率单调减小; 混流泵叶顶间隙变化引起的喷泵效率改变量不受流量影响, 而轴流泵效率变化量随流量增大而增大, 以较大叶顶间隙为基准, 且叶顶间隙变化量相同时, 混流泵效率变化较大, 轴流泵效率变化较小; 混流泵与轴流泵性能存在差异的主要原因是外形结构不同导致间隙涡对叶顶间隙泄流的作用大小不同; 当叶顶间隙由0.7mm增大至1.6mm时, 2种喷水推进器推力效率变化量在1%以内; 随着叶顶间隙的增大, 2种喷水推进器消耗功率的变化趋势与喷水推进泵相同, 且轴流式喷水推进器总推力、功率变化幅值大于混流式, 即混流式喷水推进器对叶顶间隙变化的适应性更好。      

城市快速路网布局规划方法研究——以无锡市为例

针对中国大城市干道网布局主要以环射式为主的现状,从城市空间结构分析出发,提出运用点、线、面要素分析与控制点优化法来研究大城市快速路布局规划,并以无锡市为例进行了案例分析。     

Geometrical design of blade＇s surface and boundary control of Navier-Stokes equations

In this article a new principle of geometric design for blade＇s surface of an impeller is provided. This is an optimal control problem for the boundary geometric shape of flow and the control variable is the surface of the blade. We give a minimal functional depending on the geometry of the blade＇s surface and such that the flow＇s loss achieves minimum. The existence of the solution of the optimal control problem is proved and the Euler-Lagrange equations for the surface of the blade are derived. In addition, under a new curvilinear coordinate system, the flow domain between the two blades becomes a fixed hexahedron, and the surface as a mapping from a bounded domain in R2 into R3 , is explicitly appearing in the objective functional. The Navier-Stokes equations, which include the mapping in their coefficients, can be computed by using operator splitting algorithm. Furthermore, derivatives of the solution of Navier- Stokes equations with respect to the mapping satisfy linearized Navier-Stokes equations which can be solved by using operator splitting algorithms too. Hence, a conjugate gradient method can be used to solve the optimal control problem.