MATCH-MODE METHOD AND ITS NUMERICAL SIMULATION FOR ROTOR-STATOR INTERACTION SOURCE MODES AND PROPAGATION MODES IN AN ANNULAR DUCT WITH MULTI-TREATMENTS

The suppressing design of the engine nacelle in an aircraft can benefit from the development of the prediction system for the sound fields in engine ducts which includes the prediction of the source generation and that of sound propagation in ducts. First, the acoustic match mode principle between the source modes of rotor stator interaction noise and the propagation modes is presented in this paper. Second, by utilizing this principle, the theoretical prediction method for rotor stator interaction noise generation and its propagation and attenuation in an annular duct with multi treatments is developed. That means that the prediction of sound propagation and attenuation in the segmented ducts might no longer completely depend on the in duct mode measurements, and the investigation on the sound propagation and attenuation in ducts can be accomplished not only by acoustic mode measurement, but also by making use of the source prediction to determine the source modes excited by rotor stator interaction. The effects of fan speed, blade/vane numbers, axial spacing between rotor and stator on the in duct sound attenuation and generated sound power level before and after ducts (also including the sound power level of blade passing frequency and its harmonics at the inlet of ducts) have been numerically calculated by using this prediction method. The reliability of this prediction method is verified by reasonable agreement between the predicted results with measured results in references. By analyzing the results of calculating cases, some reference criteria are provided for the engineering design of the suppressing engine nacelle.

抽水蓄能机组动静干涉与相位共振诱发振动故障机理及抑制方法研究

动静干涉与相位共振故障直接影响抽水蓄能电站水泵水轮机安全与稳定运行。本文以某水泵水轮机为对象,系统研究了由动静干涉产生的水力激振模式,并对其进行相位共振风险评估。通过实例计算分析了张河湾与黑麋峰抽水蓄能水泵水轮机由动静干涉引起厂房振动影响因素。同时,通过统计国内部分抽水蓄能电站水力参数,计算了动静干涉水力激振模式与相位共振风险系数RF,并提出相应预控措施。为其他大型抽水蓄能电站的振动问题提供参考,并为即将大规模建设的抽蓄电站安全稳定性提供积极借鉴意义。

长短叶片转轮动静干涉引起的水力激振模态数值分析

本文以5个长叶片和5个短叶片转轮(活动导叶数为16)为例,通过数值计算,分析了长短叶片转轮的动静干涉引起的水力激振模态问题。结果表明,长短叶片转轮动静干涉引起的水力激振模态比较复杂。在无叶区,水力激振模态“节径”数为相应倍频数,如5倍转频对应5“节径”等;在双叶栅区,激振力模态既有长(短)叶片数的特征(如15倍转频的模态的节径数为1),又有叶片总数的特征(如20倍转频的节径数为4,且模态旋转方向与转轮旋转方向相同)。本文的研究为长短叶片转轮的水泵水轮机的结构避振提供了新的方向。

宁海抽水蓄能电站机组相位共振风险评估

通过研究诱发相位共振的相关因素,消除抽水蓄能电站机组相位共振,提高抽蓄机组的运行稳定性,利用归纳分析法,从基础模型选择及模型试验对比结果、无叶区宽度比较、不同转轮叶片数与活动导叶数配比的水压脉动频率及优缺点、相位共振风险因子分析及业绩比较等几方面评估了宁海抽水蓄能电站机组由于动静干涉引起的相位共振风险。研究结果表明:宁海抽水蓄能电站基础模型选择合适,优化后模型各项稳定性指标优于基础模型;无叶区D_(0)/D_(1)=1.23属于国内抽蓄电站较高水平;10+16的转轮叶片数与活动导叶数配比合理,水压脉动频率较低;较低波速下相位共振风险因子高于国内工程经验值,但低于国外工程统计值。研究成果说明宁海抽水蓄能电站机组水力开发选型合理先进,发生相位共振风险较低,评估过程可为后续新建抽水蓄能电站评估提供一定参考和借鉴。

Numerical simulation of unsteady interaction of centrifugal impeller with its diffuser using Lagrangian discrete vortex method

In this study, an advanced Lagrangian vortex- boundary element method is applied to simulate the unsteady impeller-diffuser interactions in a diffuser pump not only for design but also for off-design considerations. In velocity calculations based on the Biot-Savart law we do not have to grid large portions of the flow field and the calculation points are concentrated in the regions where vorticity is present. Lagrangian representation of the evolving vorticity field is well suited to moving boundaries. An integral pressure equation shows that the pressure distribution can be estimated directly from the instantaneous velocity and vorticity field. The numerical results are compared with the experimental data and the comparisons show that the method used in this study can provide us insight into the complicated unsteady impeller-diffuser interaction phenomena in a diffuser pump.

泵喷定子襟翼作动对转子非定常力抑制方法数值研究

[目的]转子非定常力是泵喷推进器轴系振动的主要激励源,其产生机理和抑制机理受转−定子干扰流动的影响,需研究其抑制方法。[方法]在泵喷推进器定子后缘引入襟翼结构,利用襟翼作动产生二次流动,改变转子入流条件,调控转−定子干扰流动,达到抑制转子非定常力的目的。以具有前置定子襟翼的Suboff全附体艇后泵喷推进器为研究对象,采用基于SST k–ω湍流模型的URANS方法和动网格技术建立可实现定子襟翼作动的数值模型。针对转子非定常力转子叶频分量的抑制,给出定子襟翼作动规律的表达式。[结果]结果显示,在襟翼作动最优控制下,泵喷的水动力性能变化不超过1%,转子轴向非定常力在转子叶频处下降了83.35%,单个转子叶片轴向非定常力在转子叶频处降低了81.80%;襟翼作动对定子尾迹与转子入流速度的调控是抑制转子非定常力的机理。[结论]研究表明,最优控制下的定子襟翼作动能够在保持水动力性能的同时使转子非定常力特征线谱得到显著抑制,可为泵喷推进器的叶频等线谱控制提供一种新的思路。

叶片出口梯形切割对离心泵蜗壳流激噪声影响的研究

为探究叶片出口梯形切割对离心泵蜗壳流激噪声的影响,以一台比转速为66的单级单吸离心泵为对象,通过定义切割宽度系数δ与径向高度系数γ,设计了9种切割方案。基于RNG k-ε湍流模型对离心泵进行全三维非定常数值模拟,在此基础上采用边界元法(boundary element method,BEM)计算内场噪声,采用结构有限元法(finite element method,FEM)耦合声学边界元方法计算外场流激噪声;分析不同切割方案下离心泵水力特性和噪声幅射特性,经试验方法验证数值计算的准确性。研究表明:动静干涉是离心泵蜗壳流激噪声产生的主要原因,合理的叶片出口梯形切割能使离心泵水力性能基本稳定的同时有效降低动静干涉强度及蜗壳流激噪声水平;声学性能最优切割方案,叶频处的进、出口监测点声压级分别下降13%和7.5%,外场噪声监测点声压级下降2.4%。

满负荷工况下水泵水轮机动静干涉效应研究

动静干涉引起的压力脉动主要是叶片通过频率及其倍频。这些频率的压力脉动在无叶区、活动导叶和固定导叶以及流道上游传播和反射,极大地影响机组的安全稳定运行。本文基于可压缩计算方法,获得某高水头水泵水轮机满负荷工况下1倍和2倍叶片通过频率压力脉动,通过分析其幅值和相位的分布特征,探索了压力脉动传播特性。

Laser Measurements in High Speed Compressors for Rotor-Stator Interaction Analysis

This paper deals with the experimental quantification of the unsteady effects of the interactions between rotor and stator rows in high speed compressors. Due to the fact that the levels of the periodic fluctuations arising from the unsteady interaction may be low compared with the random fluctuations arising from the measurement uncertainties, it is crucial to minimize the errors inherent to the used technique. The first part of the paper concentrates on technical details relative to the experimental process. The second part is devoted to the data post-processing. Two tools for analysing the rotor-stator interactions are presented. The first tool is based on a decomposition of the flow field which was initially introduced to solve numerical problems when attempting to calculate the flow field in a multi-row configuration. The second tool is based on a spectral analysis of the signal, that qualifies the interaction in a sense of circumferential spinning lobes. Experimental results obtained within both an axial and a centrifugal high speed compressors are used to illustrate the data processing. In both cases, the effects of the unsteady interaction are quantified.

Experimental Analysis of the Rotor Stator Interaction Within a High Pressure Centrifugal Compressor

An analysis of the experimental results obtained by laser two focus anemometry in the rotor-stator inter-row region of a high-speed high-pressure centrifugal compressor is presented with the aim of quantifying the unsteady effects of the rotor-stator interaction. Two complementary methods are used. First, the results are analyzed in terms of the time-averaging procedure developed by Adamczyk. The purely time dependent correlations of the velocity components are quantified. They show that the unsteady interaction is mainly due to the splitter wake-vane interaction. Then, it is shown that the rotor-stator interaction produces spatial harmonics which are identified as spinning modes by means of Fourier series.

Numerical Simulation of Sand Erosion Phenomena in Rotor/Stator Interaction of Compressor

沙侵蚀是侵犯到一面墙的稳固的粒子引起严重机械损坏到墙表面的现象。这现象是典型煤气粒子的二阶段的狂暴的流动和流动地，粒子轨道和墙变丑与对方一起交往的一个多物理问题。在另一方面，在微粒环境操作的飞机引擎由于沙侵蚀受到表演和一生恶化。特别，飞机引擎的压缩机严重地被损坏。压缩机的流动地强烈有三个维、不稳定的性质。以便由于沙侵蚀估计恶化，为一台压缩机的沙侵蚀模拟在转子定子相互作用的考虑下面被要求。在现在的学习，我们把我们的三维的沙侵蚀预言代码用于一台单个阶段轴流压缩机。我们数字地在压缩机调查流动领域，粒子轨道，和侵蚀的墙形状的变化，到在压缩机澄清沙侵蚀的效果。

Unsteady Rotor-Stator Interaction in High Speed Compressor and Turbine Stages

片排相互作用能改变时间平均数流动因此具有为空气动力学的设计分析的兴趣。而在低亚声的 turbomachines 以内的结果在文学是相当众多的，有少得多的工作，在高速度盒子以内给片排相互作用的结果。二个盒子在这份报纸被联系。首先，效果一到来在一台接近音速的压缩机的转子流动地上醒来被分析。片排相互作用证明了关于全部的压力比率，但是否定考虑积极损失。第二个盒子使一台接近音速的汽轮机担心。特别强调被放在对在平均经过方程系统包括的确定的关联的评价上。关键词不稳定的气体动力学 - 转子定子相互作用 - 确定的压力 CLC 数字

Numerical Simulation of Rotor-stator Interactions in a Transonic Compressor Stage

A numerical method is developed for the simulation of rotor\|stator interactions in a compessor or turbine stage. This method solves quasi\|three\|dimensional Navier\|Stokes equations by an implicit high\|resolution finite volume approach.A fully conservative method is designed to compute the inviscid and viscous fluxes at the interface of rotor and stator grids. Numerical results of rotor\|stator interactions in a transonic compressor stage are presented. The mechanism of rotor\|stator interactions in this compressor stage is discussed in terms of the computational results.

Modal Decomposition for the Analysis of the Rotor-stator Interactions in Multi-stage Compressors

A modal analysis method of the rotor-stator interactions in multistage compressors has been developed by LMFA.This method,based on a double modal decomposition of the flow over space and time,has been applied to nu-merical and experimental results of the high-speed 3?-stage compressor CREATE based at LMFA,Lyon-France.It reveals the presence of a very strong rotor-stator interaction which completely drives the flow at casing behind all the rotors.This modal analysis method applied to an unsteady RANS simulation permits to calculate the en-ergy of the rotor-stator interactions and to plot energetic meridian maps to explain experimental results and to analyze the interaction in the whole machine.

An Extraction of the Dominant Rotor-Stator Interaction Modes by the Use of Proper Orthogonal Decomposition (POD)

合适的直角的分解方法在转子定子以内被用于即时速度地一台高速度的高压的离心的压缩机的内部排的区域。处理数据来自实验和数字模拟。与 Fourier 变换比较， POD 为两块起始的地给最好的形式的近似，以在要考虑的模式的任何给定的数字上表示的精力：到速度地的活动范围 98% 全部的精力，邮政部门模式的要求的数字比 Fourier 泛音的数字低多达九倍。单个邮政部门模式被给并且证明不稳定的转子定子相互作用已经是在第一个模式的现在。关键词转子定子相互作用 - 合适的直角的分解 -

动静干涉下高压涡轮外环非定常气膜冷却性能分析

为了探索航空发动机高压涡轮外环非定常气膜冷却性能的影响因素及其作用规律,对叶片高速旋转作用下某航空发动机高压涡轮外环的非定常气膜冷却过程进行了3维数值模拟。应用滑移网格技术实现了涡轮叶片与涡轮外环壁面之间的相对运动以及转子与静子之间干涉作用的模拟;分析了叶片的旋转作用、吹风比、气膜射流方向、气膜轴向射流角度等因素对高压涡轮外环非定常气膜冷却性能的影响规律。结果表明:在高吹风比下应防止叶片前缘上游气膜孔冷却裕度不足现象的发生;逆向排布的气膜孔更适合在高吹风比下使用;当气膜入射角由45°减小为30°时,外环面平均气膜冷却效率时均值增大18.54%,显著提高了涡轮外环冷却的冷气利用效率。

抽水蓄能电站水泵水轮机的动静干涉与振动分析

针对抽水蓄能电站水泵水轮机运行过程中出现的振动问题,从产生共振的条件出发,分析了转轮叶片和活动导叶形成的叶栅组合的动静干涉机理。根据转轮对水力激振模式的动态响应,研究了不同叶栅组合方式对水力激振力的影响。建立流固耦合数学模型,对转轮、活动导叶、顶盖及底环等过流部件的动态特性进行了有限元分析,以7/20的叶栅组合为例,阐述了流体激发结构共振的可能性。为了避免过流部件发生共振以及由此产生的疲劳裂纹或断裂等事故,提出了最佳叶栅组合的选择原则、降低无叶区压力脉动的方法以及提高结构固有频率和降低局部应力集中系数的具体措施。

高速泵内三维非定常动静干扰流动计算

利用三维Navier-Stokes方程和RNG湍流模型,并在转动部件与静止部件间采用滑移网格技术建立交互界面,对高速泵内多级动静干扰引起的三维非定常湍流进行了计算,得到了旋转叶轮与固定导叶间的流体的紊流特征。