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27147

PERFORMANCE OF OIL-INJECTED TWIN-ROTORS SCREW COMPRESSOR

Article

Last updated: 04 Jan 2025

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Abstract

In order to improve the performance of screw compressor, it is important to know, understand, and analysis the different geometrical as well as operating parameters on the compressor performance. Consequently, the present study is concerned with obtaining the characteristics of twin-screw compressor by using a simulation code named SCORPATH. Explanation of the code is presented and discussed. A parametric study was performed to determine the effect of the geometrical and the operating parameters on the performance of screw compressor. The study revealed that the geometrical parameters: clearance gap, number of lobes in the rotors, rotor relative length, and screw wrap angle, have significant effect on the performance of the screw compressor. In addition, built in volume ratio, tip speed, suction and discharge pressures, are the operating parameters which have a great effect on the performance of the twin-screw compressor.

DOI

10.21608/asat.2011.27147

Keywords

Compressor, screw machine, oil-injected

Authors

First Name

KASSAB

Last Name

Z.

MiddleName

S.

Affiliation

Professor, Mechanical Engineering Department, Alexandria University, Egypt.

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City

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Orcid

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First Name

ADAM

Last Name

G.

MiddleName

I.

Affiliation

Lecturer, Mechanical Engineering Department, Alexandria University, Egypt.

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City

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Orcid

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First Name

ELGOHARY

Last Name

A.

MiddleName

H.

Affiliation

Graduate Student, Mechanical Engineering Dept., Alexandria University, Egypt.

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-

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Orcid

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Volume

11

Article Issue

ASAT Conference, 17-19 May 2005

Related Issue

4906

Issue Date

2011-05-01

Receive Date

2019-02-14

Publish Date

2011-05-01

Page Start

199

Page End

219

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_27147.html

Detail API

https://asat.journals.ekb.eg/service?article_code=27147

Order

12

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

PERFORMANCE OF OIL-INJECTED TWIN-ROTORS SCREW COMPRESSOR

Details

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Article

Created At

22 Jan 2023