LAPSE:2023.36105
Published Article
LAPSE:2023.36105
Nozzle Jet Deviation from Bucket Pitch Circle’s Effect on the Stability and Efficiency of Pelton Turbine
Huiming Deng, Ke Song, Fangxiong Deng, Yu Huang, Tao Luo, Yijin Zhou, Bei Qin, Yongzhong Zeng, Zhishun Yu, Jiayang Pang, Xiaobing Liu
June 13, 2023
During the operation of a Pelton turbine, the centerline of the nozzle jet may deviate from the bucket pitch circle due to the low installation and maintenance accuracy, which will reduce the operating efficiency and the stability of the turbine and even cause severe vibrations and damages. Based on the VOF (Volume of Fluid) two-phase flow model and the SST k-ω turbulence model, the flow characteristics of a Pelton turbine were simulated with the nozzle jet deviating from the bucket pitch circle. The pressure pulsation inside the bucket and the force distribution of the runner were obtained, the turbine oscillation and efficiency were measured before and after the jet deviation, and the effects of the radial and axial deviations on the stability and efficiency of the Pelton turbine were analyzed. The results show that both the radial and axial deviations of the jet cause a significant increase in the axial force and the pressure pulsation amplitude of the turbine; the radial and tangential forces on the runner are slightly reduced; the maximum axial force on the runner is increased by 4 times and 2 times, respectively, after the axial and radial deviations within the maximum value allowed by the industry standard; and the efficiency of the turbine is reduced by 0.4% and 0.3%, respectively. The maximum relative amplitude of pressure pulsation in the radial offset case appears in the center of the bucket blade, while the axial offset case causes uneven pressure distribution on both sides of the diverter blade, uneven force on the bucket blade of the runner, and fatigue damage. By comparing the operation of the runner under the two offset cases, we can find that the axial offset of the jet has a greater impact on the stability of the runner than the radial offset, and the unit is more prone to vibration, increasing the risk of the unit lifting.
Keywords
deviation, efficiency, jet, Pelton turbine, stability
Suggested Citation
Deng H, Song K, Deng F, Huang Y, Luo T, Zhou Y, Qin B, Zeng Y, Yu Z, Pang J, Liu X. Nozzle Jet Deviation from Bucket Pitch Circle’s Effect on the Stability and Efficiency of Pelton Turbine. (2023). LAPSE:2023.36105
Author Affiliations
Deng H: Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu 610039, China
Song K: CHN Energy Dadu River Geshizha Hydropower Development Co., Ltd., Danba 626300, China
Deng F: CHN Energy Dadu River Geshizha Hydropower Development Co., Ltd., Danba 626300, China
Huang Y: Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu 610039, China
Luo T: CHN Energy Dadu River Geshizha Hydropower Development Co., Ltd., Danba 626300, China
Zhou Y: Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu 610039, China
Qin B: Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu 610039, China
Zeng Y: Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu 610039, China
Yu Z: Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu 610039, China
Pang J: College of Water Resources and Civil Engineering, China Agricultural University, Beijing 100083, China [ORCID]
Liu X: Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu 610039, China
Journal Name
Processes
Volume
11
Issue
5
First Page
1342
Year
2023
Publication Date
2023-04-26
Published Version
ISSN
2227-9717
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PII: pr11051342, Publication Type: Journal Article
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LAPSE:2023.36105
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doi:10.3390/pr11051342
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Jun 13, 2023
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Jun 13, 2023
 
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Calvin Tsay
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