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The effects of the rotor-stator interaction on unsteady pressure pulsation and radial force in a centrifugal pump 被引量:13
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作者 Issa Chalghoum Sami Elaoud +1 位作者 Hatem Kanfoudi Mohsen Akrout 《Journal of Hydrodynamics》 SCIE EI CSCD 2018年第4期672-681,共10页
An unsteady numerical analysis has been conducted to study the strong interaction between impeller blade and volute tongue of a centrifugal pump. The 3-D-URANS equations were solved with the shear stress transport tur... An unsteady numerical analysis has been conducted to study the strong interaction between impeller blade and volute tongue of a centrifugal pump. The 3-D-URANS equations were solved with the shear stress transport turbulence model for a wide range of flow rates. These unsteady interactions are mostly related to the unsteady radial force due to an imbalance in the pressure field at the impeller periphery. This force represents dynamic load that are one of the most important sources of vibration and hydraulic noise. Based on this phenomenon, this work analyzes and gives a more realistic prediction of the pressure fluctuation and the radial force during steady and unsteady calculation by considering the effect of the change in the pump operating point. Actually, the pressure fluctuations in the impeller and the volute were recorded by mounting nine monitoring points on the impeller and volute casing. The results of the existing analysis has proven that the pressure fluctuation is periodic due to the relative position of impeller blade to volute tongue. The characteristics of the time domain and frequency domain of the pressure pulsation were analyzed under different coupling conditions. Fast Fourier transform was performed to obtain the spectra of pressure pulsation. Besides, the steady and unsteady forces were calculated around the impeller periphery to fully characterize the pump behavior. The obtained pump performance curves were numerically compared with the experimental ones, and the outcome have shown an acceptable agreement between both curves. 展开更多
关键词 Unsteady simulation blade-tongue interaction unsteady pressure distribution blade-passing frequency
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倾斜蜗舌对离心风机降噪影响的试验研究 被引量:31
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作者 赵婷 赵忖 +1 位作者 任刚 师铜墙 《流体机械》 CSCD 北大核心 2012年第3期1-7,共7页
针对T9-19No.4A离心风机,试验研究了倾斜蜗舌和蜗舌的安装位置对风机气动性能和噪声特性的影响,结果表明:随着蜗舌倾角和蜗舌与叶轮间安装间距(以下简称安装间距)的增加风机的噪声下降,蜗舌倾角和安装间距对风机的气动性能则是交互影响... 针对T9-19No.4A离心风机,试验研究了倾斜蜗舌和蜗舌的安装位置对风机气动性能和噪声特性的影响,结果表明:随着蜗舌倾角和蜗舌与叶轮间安装间距(以下简称安装间距)的增加风机的噪声下降,蜗舌倾角和安装间距对风机的气动性能则是交互影响,不具有单一性。本文选取了3种不同的蜗舌倾角和安装间距,组合优化设计了7种倾斜蜗舌进行试验。风机气动性能的测量严格按照国标《GB/T1236-2000工业通风机用标准化风道进行性能试验》执行,噪声的测量按照《GB/T 2888-91风机和罗茨鼓风机噪声测量方法》的要求执行。 展开更多
关键词 离心风机 倾斜蜗舌 安装间距 降噪 气动性能 试验研究
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发动机叶片榫槽仿形涡流传感器的设计
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作者 廖泽彬 张国才 张华 《无损检测》 CAS 2022年第7期1-5,共5页
针对特定的航空发动机涡轮叶片榫槽,设计了同心方形线圈仿形涡流传感器,在不同激励模式与激励频率下,对发动机叶片榫槽开展电磁学仿真检测试验。仿真结果表明,同心方形线圈传感器在激励频率为500 kHz与外线圈激励模式下,除了半径为0.05 ... 针对特定的航空发动机涡轮叶片榫槽,设计了同心方形线圈仿形涡流传感器,在不同激励模式与激励频率下,对发动机叶片榫槽开展电磁学仿真检测试验。仿真结果表明,同心方形线圈传感器在激励频率为500 kHz与外线圈激励模式下,除了半径为0.05 mm,深为0.5 mm的圆形缺陷无法检出外,可以检测出长为1.0 mm,宽为0.2 mm或0.1 mm,深为0.5 mm或1.0 mm的4种纵向缺陷及半径为0.1 mm,深为0.5 mm或1.0 mm和半径为0.05 mm,深为1.0 mm的3种圆形缺陷。 展开更多
关键词 发动机叶片榫槽 仿形涡流传感器 电磁学仿真
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