风力发电机叶片的雾凇覆冰数值模拟

为了解风力发电机叶片覆冰情况,以某型300 kW风力发电机叶片为研究对象,根据切片-重构的思想,将叶片划分为有限个截面,基于叶片覆冰的物理过程,采用边界元法对风力发电机叶片的空气流场进行计算;采用拉格朗日法分析计算水滴在叶片表面的碰撞过程;通过迭代计算和冰形重构模拟覆冰增长过程,从而建立风力发电机叶片三维雾凇覆冰增长模...     

Numerical investigation on bowed blades of Iarge meridional expansion Turbine

To improve the performance of the Turbofan engine,several measures should be considered during design process.Such measures,relating to aerodynamic characteristic design,include the maximum enthalpy per stage,the shortest axial length,the minimum blade rows and the highest efficient in design and off design condition.To satisfy theses design characters,the meridian geometry of the engine will he excurvature at a high degree transition part between HP and LP turbines.The study is to investigate the effect of blade bowing on flow loss at blade tip and root of the type of turbine.Such turbine,tending towards separation,with severe secondary flow at the tip and strong radial flow at exit,was simulated by the 3D N-S solver Numerea,and there were several different stacking line bowing schemes in all.The results show that tip negative bowing and root positive bowing is able to weaken radial flow,consequently reduce the flow loss at the tip and root.     

Numerical investigation on bowed blades of large meridional expansion Turbine

To improve the performance of the Turbofan engine,several measures should be considered during design process.Such measures,relating to aerodynamic characteristic design,include the maximum enthalpy per stage,the shortest axial length,the minimum blade rows and the highest efficient in design and off design condition.To satisfy theses design characters,the meridian geometry of the engine will be excurvature at a high degree transition part between HP and LP turbines.The study is to investigate the effect of blade bowing on flow loss at blade tip and root of the type of turbine.Such turbine,tending towards separation,with severe secondary flow at the tip and strong radial flow at exit,was simulated by the 3D N-S solver Numerca,and there were several different stacking line bowing schemes in all.The results show that tip negative bowing and root positive bowing is able to weaken radial flow,consequently reduce the flow loss at the tip and root.     

A comparative analysis of 3D flow fields between straight and bowed blades in a steam turbine

A commercial Navier-Stokes flow solver has been employed for simulating steady subsonic flow characteristics and analyzing the comparative features of flow fields between straight and bowed blades applied to the stator of a high pressure steam turbine, For comparison, we have studied the effeets of bowed blades on the wakes of stator trailing edge and horse shoe vortex in the rotor. It was found that the position of wakes for bowed blades is shifted toward the blade suction side. Also, we have discussed and compared the entropy generation and energy loss caused by dissipation mechanism within the boundary layers on the hub and shroud; and temperature gradient in lneridional plane.     

16MN钢坯剪切机刀片的堆焊修复研究

分析了１６ＭＮ剪切机刀片的载载体，破坏形式，阐述了其刀片修复的基本思路，并给出了经修复后刀片的显微组织特点，修复刀片经现场使用后表明，其使用寿命可达原刀片寿命２倍以上。     

双层反转垂直轴风力机的流场特性数值模拟

针对由垂直轴风力机运行过程中的动态失速问题所导致的功率系数较低的问题,提出双层反转构型的垂直轴风力机. 通过在传统垂直轴风力机内侧设置反转向辅助叶片的方式,改善垂直轴风力机流场,从而提高其功率系数. 将该风力机与传统垂直轴风力机进行计算流体动力学数值模拟对比分析,研究不同叶尖速比情况下两者流场特性的差异以及双层风力机内外层风轮起始运转相位差的影响. 通过计算得到的内层辅助叶片的时均扭矩系数为正,不需要额外功率输入. 外层叶片的扭矩系数结果表明,采用这种构型会降低叶片上游区域扭矩系数的峰值,同时大幅提高下游区域扭矩系数,从而实现时均发电效率的提高. 对流场中涡系结构进行分析,结果表明,功率系数提升的原因是内层辅助叶片的反向旋转抑制了主叶片的动态失速. 特别是当叶尖速比为1.85时,在初始相位差为90°的对比算例中,与传统垂直轴风力机相比,新构型下的叶片时均扭矩系数提高了43.92 %.     

自带冠叶片碰撞减振研究

建立自带冠叶片碰撞减振的力学模型和数学模型,用理论方法和试验方法研究碰撞减振效果与叶片结构参数之间的关系.研究结果表明,自带冠叶片碰撞减振具有很好的减振效果,其动应力水平与叶片负荷的关系很小,适合于中短叶片.并提出自带冠叶片的设计方法和可靠性准则,考虑非线性的影响.     

汽轮机叶片振动非接触测量技术综述

介绍了汽轮机旋转叶片振动非接触测量技术的研究现状,比较了用于汽轮机叶片非接触测量的各种方法。非接触测量方法可以实现对整级中的所有叶片进行在线监测,具有接触测量方法不可比拟的优势。     

风力机翼型及叶片气动性能数值模拟

采用FLUENT数值计算方法模拟了NACA4412、NACA4418、FX60-126和NREL-S809四种常用风力机翼型和单位长度平板叶片以及单位长度实际叶片.通过数值计算所得4种翼型的升阻力系数曲线与实验数据的对比,验证了计算模型和计算方法的准确性,在此基础上分析了翼型和平板叶片随攻角变化的流场分布规律以及实际叶片的三维气动特性,数值模拟结果显示三维平板叶片在失速攻角附近气流展向流动较明显,三维实际叶片旋转时气流展向流动产生了三维涡体,更准确地反映了实际叶片的气动特性.     

空气冷却涡轮叶片气热耦合数值计算

借助CFX-TASC flow程序的气热耦合数值模拟技术分析了文献[1]实验研究的径向冷却高压涡轮叶片,计算结果与实验数据比较吻合,与绝热壁面条件的结果比较,叶片外表面的等熵马赫数增加.     

基于UG的叶片专用数控加工软件

为了提高叶片零件设计及加工效率,开发出一套基于图形化编程技术的叶片专用数控加工软件.针对专用数控加工软件开发周期长、工作量大的特点,提出了在UG软件CAD/CAM模块基础上使用UG/OpenAPI函数开发叶片专用数控加工软件的方法.开发的叶片专用数控加工软件以数据库为核心,分为叶片CAD和叶片CAM两个部分.在叶片CAD模块中实现了叶片零件三维参数化设计.在叶片CAM模块中解决了叶片零件加工刀具轨迹生成及数控加工代码生成问题.数控加工软件的开发实现了叶片从设计到加工的无缝集成.对提高叶片设计、加工质量和效率及降低叶片生产制造成本有着十分重要的意义.     

汽轮机叶片1Cr13钢表面微弧修复的工艺研究

研究3H-ES-6型金属表面强化修复机修复汽轮机叶片1Cr13钢过程中工艺参数对修复效果的影响,并将修复后的试样用200 MAT金相显微镜观察.研究结果表明:用直径2.5mm的ZEA132电极修复叶片1Cr13钢时采用1000 r/min的电极棒自身转速、10 mm/s的电极移动横向速度、电极头10～40 mm的横向摆幅、68 V的修复电压、640 W的功率和300 Hz的频率能取得最佳的修复效果.     

非惯性系下旋转柔性叶片的动力学分析

旋转柔性叶片是汽轮机关键零部件,针对叶片振动损伤问题,考虑经历大范围运动的柔性叶片刚性运动与弹性变形运动之间的相互耦合,应用哈密顿原理建立了旋转柔性叶片非线性动力学控制方程.考虑旋转离心惯性力的影响以及轴向变形与横向变形之间的耦合,基于假设模态法对方程进行离散,研究了不同转速下梁端部位移的响应.研究结果表明,刚性旋转运动对柔性叶片端部位移的响应具有明显的影响,并且由于离心力的存在,出现了动力刚化现象,文中所用方法及数值仿真结果可用于研究旋转柔性叶片的振动失效问题.     

水在波纹板间结冰过程的数值模拟

在空调新风机组中采用空气一水板式换热器代替翅片管式换热器,可防止我国三北地区由于采暖初期与末期热媒的温度偏低,翅片管式换热器加热0℃以下的空气时易结冰,影响正常工作的现象发生.空气一水波纹板式换热器利用波纹板片之间形成三维复杂流道,流体以较小的流速在其间流动就可形成湍流,湍流的形成带来剧烈的能量掺混可有效防止冰层在波纹表面的形成.利用FLUENT软件Solidification/Melting模型分别模拟了静态水与动态水在波纹板间的三维结冰过程,揭示了波纹板式换热器的波纹板片流道结构形式可有效防止流水结冰现象的发生,为相关产品的开发与优化提供依据.     

蒸汽轮机末级应用海豚型静叶的数值仿真

分别对海豚型叶型和常规设计的蒸汽轮机叶型进行了一级全三维气液两相数值计算,对比发现所设计的海豚型叶型在改善常规叶型流场的气动性能、提高汽轮机轮周效率的同时,可以提高流道内叶片段区域的湿蒸汽干度,改善流道内湿蒸汽的分布。海豚型叶型具有短的扩压段,使激波和附面层干扰区域具有更强的防汽流脱落能力,这样可减少此区域内水膜被高速汽流急剧撕裂成二次水滴的可能。海豚型叶型通道内湿蒸汽湿度沿叶高的分布特点有利于在叶片上表面开设除湿槽,进行高效除湿。     

Numerical simulation of 3D viscous flow field of air cooled turbine blades with coolant mixing

To improve thrust and reduce oil consumption of aero-engines, the temperature at turbine inlet is becoming higher and higher, which leads to heavy thermal load of vanes. To efficiently cool the vanes, the mass of coolant with its maximum gas mass flow exceeding to 20% of main stream, has to be increased. In the pres- ent paper, a two-stage turbine with and without coolant mixing was simulated by CFX-TASCflow. Simulation resuits indicate that the flow field structure with coolant is obviously different from that without coolant, and the former has characteristics of lower-speed main flow, reduced mach number, weaker shock intensity and decreased stage efficiency.     

数值模拟与物质平衡关系理论研究

油藏数值模拟方法在很多情况下都是由传统油藏工程方法推导出来的,阐明了油藏数值模拟法与物质平衡方法之间的关系,通过假设法对传统物质平衡方程、广义物质平衡方程与油藏数值模拟进行理论研究。     

Numerical simulation for sheet metal forming process of 16Mn blade of large concrete-mixer truck

A finite element analysis method was used to simulate the stamping process of the blade of a large concrete-mixer truck. The updated Lagrange method and the elasto-plastic constitutive equation were adopted to solve the large strain and displacement deformation of the blade. A modified Coulomb friction model was used to solve the sliding contact between the blade and the dies. The yon Mises stress distribution in the blade, the spatial displacement variation and the spring-back of the typical node were investigated in the simulation. The yon Mises stress in the blade where the spring-back occurs is lowered from 463.0 MPa to 150.0 MPa before and after the spring-back.A typical node in the blade has a 3.33 mm spring-back in Z direction. The results of the experiments agree well with the simulation. The analysis results are valuable for designing optimal tool dies.     

混合对流作用下小室流场和温度场的数值模拟

建筑空调为人们提供清洁舒适的室内环境。本文在Ｂｌａｙ等人实验研究基础之上 ,采用标准关键词模型和壁面函数法 ,对具有混合对流作用的小室流场和温度场进行数值模拟 ,经与实验值对比发现 ,标准κ-ε模型可以较为准确模拟混合对流作用的流动与传热问题 ,速度值的最大偏差为 0 . 0 43ｍ ｓ,温度最大偏差值为 1 . 1Ｋ ;浮升力对ε方程中源项的影响可以不计     

液力变矩器叶栅绘形的三维模型设计方法

提出在液力变矩器叶栅系统设计中直接建立叶栅系统三维模型，采用一种几何变换方法精确求解液力变矩器叶栅数据，克服以往平面展开近似算法的误差（尤其是轴向抽影图中向心涡轮变矩器其涡轮进口及泵轮出口处其流线切线与轴线几乎平行时，投影计算法误差较大），使设计计算结果更精确，该方法简单易行，可对叶栅系统的空间结构进行更加详细的描述。