A Method for the Suppression of Rotating Cavitation by an Accumulator at the Inlet of an Inducer

Author:

FUJII Akira1,MIZUNO Shinichi2,HORIGUCHI Hironori3,TSUJIMOTO Yoshinobu3

Affiliation:

1. ANSYS Japan K. K.

2. Nagasaki Shipyard and Machinery Works, Mitsubishi Heavy Industry, Ltd.

3. Graduate School of Engineering Science, Osaka University

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering

Reference19 articles.

1. (1) Osborn, W. M., Lewis Jr., G. W., and Heidelberg, L. J., Effect of Several Porous Casing Treatment on Stall Limit and on Overall Performance of an Axial- Flow Compressor Rotor, NASA Technical Note, D-6537 (1971), pp. 1-47.

2. (2) Moore, R. D., Kovich, G., and Blade, R. J., Effect of Casing Treatment on Overall and Blade-Element Performance of a Compressor Rotor, NASA Technical Note, D-6538 (1971), pp. 1-65.

3. (3) Kurokawa, J., An Innovative Device to Suppress Performance-Curve Instability in a Mixed Flow Pump by Use of J-Groove, Transactions of the Japan Society of Mechanical Engineers, Series B, Vol. 66, No. 642(2000), pp. 460-467.

4. (4) Miyake, Y., Noji, I., Nishikawa, Y., and Murata, S., The Characteristics of the Air-Separator of an Axial Flow Fan, Transactions of the Japan Society of Mechanical Engineers, Series B, Vol. 50, No. 460(1984), pp. 2960-2967.

5. (5) Sloteman, D. P. et al, Control of Backflow at the Inlets of Centrifugal Pumps and Inducers, Proceedings of the First International Pump Symposium, (1984), pp. 9-22.

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