Vibration response of a waterjet propulsion pump under low-gas-fraction microbubble inflow

This study experimentally investigates the vibration attenuation effect of low-inlet-gas-volume-fraction microbubble inflow in a waterjet propulsion pump. Hydraulic performance and triaxial vibration responses at the inlet, impeller, and outlet were measured under IGVF values of 0–0.5%. The vibration signals were analyzed using root-mean-square values, fast Fourier transform, empirical mode decomposition, and the Hilbert–Huang transform. The results show that microbubble inflow has only a limited influence on the head coefficient and efficiency, while effectively reducing vibration responses at all measuring locations. The impeller region exhibits the highest vibration intensity and the strongest sensitivity to gas entrainment. Frequency-domain analysis indicates that the main spectral peak locations remain nearly unchanged, while the amplitudes of several prominent peaks and the broadband vibration response decrease under microbubble inflow. The EMD and Hilbert marginal energy analyses show that the first two IMF components account for most of the summed IMF energy and that microbubble inflow reduces the vibration signal energy across a broad frequency range. Additional pressure-pulsation measurements and pressure–vibration coherence analysis reveal frequency-dependent changes in selected hydraulic excitation components and their linear relationship with vibration. These results demonstrate vibration attenuation under the tested low-IGVF conditions and characterize the accompanying changes in pressure pulsations.

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Publication Details

Journal
Ocean Engineering
Published
2026-10-07
DOI
https://doi.org/10.1016/j.oceaneng.2026.128632
Primary Topic
Cavitation Phenomena in Pumps
Type
article
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article

Vibration response of a waterjet propulsion pump under low-gas-fraction microbubble inflow

Yongxin Jin, Chao Feng, Zhengchuan Zhang, HaoHao Jiang et al.
Ocean Engineering
Cavitation Phenomena in Pumps
article

Vibration response of a waterjet propulsion pump under low-gas-fraction microbubble inflow

Yongxin Jin, Chao Feng, Zhengchuan Zhang, HaoHao Jiang, Ning Li
article en

Abstract

This study experimentally investigates the vibration attenuation effect of low-inlet-gas-volume-fraction microbubble inflow in a waterjet propulsion pump. Hydraulic performance and triaxial vibration responses at the inlet, impeller, and outlet were measured under IGVF values of 0–0.5%. The vibration signals were analyzed using root-mean-square values, fast Fourier transform, empirical mode decomposition, and the Hilbert–Huang transform. The results show that microbubble inflow has only a limited influence on the head coefficient and efficiency, while effectively reducing vibration responses at all measuring locations. The impeller region exhibits the highest vibration intensity and the strongest sensitivity to gas entrainment. Frequency-domain analysis indicates that the main spectral peak locations remain nearly unchanged, while the amplitudes of several prominent peaks and the broadband vibration response decrease under microbubble inflow. The EMD and Hilbert marginal energy analyses show that the first two IMF components account for most of the summed IMF energy and that microbubble inflow reduces the vibration signal energy across a broad frequency range. Additional pressure-pulsation measurements and pressure–vibration coherence analysis reveal frequency-dependent changes in selected hydraulic excitation components and their linear relationship with vibration. These results demonstrate vibration attenuation under the tested low-IGVF conditions and characterize the accompanying changes in pressure pulsations.

Ocean EngineeringVol. 368
Xihua University (CN), Shanghai Jiao Tong University (CN), Marine Design & Research Institute of China (CN)
Openalex Percentile: Top 22%
Cavitation Phenomena in Pumps
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Vibration response of a waterjet propulsion pump under low-gas-fraction microbubble inflow — Yongxin Jin, Chao Feng, et al. · Ocean Engineering (2026) | TGRS Research Map | TGRS