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22240

Experimental Study of the Effect of Blade Configurations on the Performance of Centrifugal Pumps

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Last updated: 24 Dec 2024

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Abstract

In the present paper, the effect of change the blade configurations of the centrifugal pump impeller on its performance has been investigated. The pump under investigation has been designed and manufactured to be able to change its blades configurations in a way that the performance of the pump could be measured. The blades configurations have been tested
for conventional blades, as well as split to two and three parts. The split blades were tested for clockwise and anti-clock-wise shifting. The experimental test rig has been carried out and the pump performances, (speed- head- flow rate- power and efficiency) have been measured for conventional impeller blades configuration, as well as for eight iterations of different impeller configurations according to the blades arrangement for different rotational speed ranged from 700 to 1450 rpm. The main blade configuration parameters are the splitting angle (forward or backward) and splitting
diameter. The results showed that, for the same pump rotational speed, the pump head, efficiency and design flow rate, may increase or decrease by 12 to 16 %, compared to the basic impeller configuration.

DOI

10.21608/asat.2013.22240

Authors

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A.

Last Name

Sadek

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Affiliation

Egyptian Armed Forces, Egypt.

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First Name

I.

Last Name

Saleh

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Affiliation

Egyptian Armed Forces, Egypt.

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Orcid

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First Name

R.

Last Name

Nassif

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Affiliation

Ain Shams University, Egypt.

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First Name

E.

Last Name

Mouris

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Affiliation

Ain Shams University, Egypt.

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Volume

15

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013

Related Issue

4183

Issue Date

2013-05-01

Receive Date

2018-12-18

Publish Date

2013-05-01

Page Start

1

Page End

12

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_22240.html

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https://asat.journals.ekb.eg/service?article_code=22240

Order

102

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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

Experimental Study of the Effect of Blade Configurations on the Performance of Centrifugal Pumps

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Article

Created At

22 Jan 2023