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22364

Reduction of Radial Thrust by Using Triple-Volute Casing Centrifugal Pump

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Last updated: 04 Jan 2025

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Abstract

Radial thrust in a single volute centrifugal pump, which is a result of pressure variation in the volute casing, is investigated in order to avoid failures caused by this thrust force. Two ideas are introduced to avoid or to minimize this thrust force, the first is a double volute, and the second is a triple volute. A complete centrifugal pump design was manufactured. The volute was designed such that partition vanes could be added to change the number of volutes. Experiments were performed on single, double, triple volutes centrifugal pump at 500, 800, and 900 rpm for each case. The performances of the three pumps as seen on a non-dimensional plot, are nearly the same in the three casing types (Single, double and triple volutes). However, the values of the efficiency reveal an improvement associated with the presence of the volute(s)
On the other hand, the use of multiple volutes reduced the radial thrust force. These reductions were pronounced as the departure from the BEP was increased. At shut off for instance, the radial thrusts for the double volutes and triple volutes were reduced by 55% and 70%, respectively, below the thrust of a single volute pump.

DOI

10.21608/asat.2018.22364

Keywords

Radial thrust, double volute, triple volute, Centrifugal Pump, Pressure distribution

Authors

First Name

E.

Last Name

Mina

MiddleName

M.

Affiliation

Ass. Prof., Mech. Power Eng. Dept., Faculty of Eng., Ain Shams University, Cairo, Egypt.

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First Name

R.

Last Name

Abdelmessih

MiddleName

N.

Affiliation

Prof., Mech. Power Eng. Dept., Faculty of Eng., Ain Shams University, Cairo, Egypt.

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City

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Orcid

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First Name

M.

Last Name

Matbouly

MiddleName

E.

Affiliation

Rotating Equipment Eng., Engineering for Petroleum and Process Industries (Enppi), Cairo, Egypt.

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Volume

17

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 – April 11 - 13, 2017

Related Issue

4266

Issue Date

2017-04-01

Receive Date

2018-12-19

Publish Date

2017-04-01

Page Start

1

Page End

13

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_22364.html

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https://asat.journals.ekb.eg/service?article_code=22364

Order

4

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Reduction of Radial Thrust by Using Triple-Volute Casing Centrifugal Pump

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Article

Created At

22 Jan 2023