The blade-passing frequency noise, abbreviated to BPF noise, of low specific speed centrifugal blower is analyzed by separating the frequency-response of the transmission passage and the intensity of the noise source. Frequency-response has previously been evaluated by the authors using a one-dimensional linear wave model, and the results have agreed well with the experimental response in a practical range of the blower speed. In the present study, the intensity of the noise source is estimated by introducing the quasi-steady model of the blade wake impingement on the scroll surface. The effective location of the noise source is determined by analyzing the cross-correlation between measured data of the blower suction noise and pressure fluctuation on the scroll surface. Then, the surface density distribution of a dipole noise source is determined from pressure fluctuation expressed in terms of quasi-steady dynamic pressure of the traveling blade wake. Finally, the free-field noise level is predicted by integrating the density spectrum of the noise source over the effective source area. The sound pressure level of the blower suction noise is easily predicted by multiplying the free-field noise level by the frequency-response characteristics of the noise transmission passage.
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ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition
June 13–16, 1994
The Hague, Netherlands
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7883-5
PROCEEDINGS PAPER
Evaluation and Prediction of Blade-Passing Frequency Noise Generated by a Centrifugal Blower
Klyohiro Tajima
Klyohiro Tajima
Waseda University, Tokyo, Japan
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Yutaka Ohta
Waseda University, Tokyo, Japan
Elsuke Outa
Waseda University, Tokyo, Japan
Klyohiro Tajima
Waseda University, Tokyo, Japan
Paper No:
94-GT-334, V001T01A109; 11 pages
Published Online:
February 18, 2015
Citation
Ohta, Y, Outa, E, & Tajima, K. "Evaluation and Prediction of Blade-Passing Frequency Noise Generated by a Centrifugal Blower." Proceedings of the ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. Volume 1: Turbomachinery. The Hague, Netherlands. June 13–16, 1994. V001T01A109. ASME. https://doi.org/10.1115/94-GT-334
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