Noise reduction and surge margin improvement using tapered diffuser vane in a centrifugal compressor

Improvement of surge margin and reduction of interaction tone noise radiated from a centrifugal compressor with a vaned diffuser is discussed from experiments and CFD analyses. Two types of one-side tapered diffuser vanes, which are shroud- and hub-side tapered vanes, were used in the experiments. The height of the leading edge of the tapered vanes varied from 100% to 10%. Both types of tapered vanes are effective for the reduction of the inter- action tone noise radiated from the compressor, because of the smaller interaction area between impel- ler-discharge flow and diffuser vane surface. Especially, the hub-side tapered diffuser vane suppresses the evolution of the leading-edge vortex, which causes reverse-flow in the diffuser passage. Furthermore, the hub-side tapered diffuser vane, which has an optimized diffuser leading edge shape, can improve the compressor pressure-rise characteristics at low-flow operation and can enlarge the surge margin.     

Influence of the wakes of rotating spokes on the performance of a turbine exhaust diffuser

The design of turbine exhaust diffusers is still commonly based upon conservative design charts which do not consider the influence of the components installed upstream such as the last turbine stage.Based on investigations with different spoke wheels which approximate the blade wakes of the last turbine stage,the influence of a rotating bladed disc on the flow in a exhaust diffuser is presented.The pressure recovery for an annual diffuser with 15° half cone angle and the 5 mm spoke wheel used in the model test is very high and nearly independent on the rotational speed and the corresponding Strouhal number.For a 20° annual diffuser,the pressure recovery increases with Strouhal number     

带轴径向扩压器低压排汽缸几何参数的选择

以大量系列试验数据和数值计算为基础,分析了轴径向扩压器及低压排汽缸各种几何参数对排汽缸气动性能的影响,并在此基础上提出了带轴径向扩压器低压排汽缸几何参数选择的范围。     

设计工况下离心压气机内部动静部件耦合非定常流动的数值模拟

以设计工况下离心压气机内部动静部件耦合的非定常流场为研究对象,采用ＰＩＳＯ算法求解了包含绝对速度与相对速度的、统一形式的运动方程组。计算结果与试验测量结果比较,说明计算结果是可靠的;计算结果同时说明,只有采用非定常算法,才有可能较好地描述动静部件耦合的流场。     

大型水泵轴向后导叶叶片出口角对出水流道性能的影响

对低扬程大型泵站单管出水流道 ,水泵出口存在最优旋流 ,使水力损失最小 ,可以通过后导叶叶片出口角设计满足出流最优旋流要求。为此 ,提出了已建泵站和新建泵站泵后导叶—出水流道整体水力设计两种物理模型 ,目的是使流道水力损失最小。提出了平分分析法试验求解物理模型的方法和后导叶设计方法     

离心压缩机无叶扩压器的改进新方法

研究了某高压比离心压缩机无叶扩压器的性能,提出在无叶扩压器轮盘侧加装一定高度机翼型导叶的改进方法。结果表明,这种扩压器可以改善其内部流动,提高自身的压力恢复系数和效率,从而改善离心压缩机的整级性能。     

改进型N300MW机组高压调节汽门故障处理

针对大坝发电有限责任公司#2汽轮机运行中#4高压调节汽门扩散器松动的问题,对松动原因进行了分析,并通过机组检修进行了处理,提出了此类问题的处理方案,确保了机组的安全运行。     

用IFA300热膜风速仪测量双舌形挡板VGT无叶喷嘴出口流场的研究

本文给出了用ＩＦＡ３００ 热膜（ 热线） 风速仪Ｘ 形探针测量双舌形挡板变截面涡轮蜗壳无叶喷嘴出口速度场的方法,分析了挡板开度对无叶喷嘴出口气流参数的影响。     

多级离心压缩机无叶扩压器内气动性能的数值研究

对某多级离心压缩机的气动性能进行了整级CFD数值模拟,重点研究并比较了级间与级后无叶扩压器内的气动特点。计算方法基于Jameson格式,湍流模型选择Spalart-Allmaras模型。结果表明,在多级离心压缩机中,无叶扩压器的性能对整个机组的总体性能影响很大。级间与级后无叶扩压器内的能量损失都很高,但后者以摩擦损失为主,而前者由于受其下游弯道的影响,流动发生分离,因而其能量损失来源于摩擦与分离的共同作用。     

紫外辐射计的波长定标及不确定度分析

限于常规汞灯谱线法波长定标的局限性,构建了紫外辐射计波长定标装置,研究了紫外辐射计波长定标的物理过程和测量链,并对紫外辐射计中臭氧十二个吸收波长进行了光谱定标,通过对定标影响量的分析和计算,得到定标影响量的测量不确定度和波长定标合成标准不确定度,其中波长定标合成标准不确定度为0.026nm,同时通过光学CAD分析和实验验证紫外辐射计的光谱带宽可以达到1.0nm.应用自行构建的紫外波长定标装置较好地完成了紫外辐射计臭氧吸收谱线的定标工作,满足了臭氧反演所需的波长精度要求和光谱带宽要求.