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Article
Affiliation(s)

1. Department of Mechanical Engineering, Jolfa International Branch, Islamic Azad University, Jolfa 54417-34335, Iran
2. Department of Mechanical and Aerospace Engineering, Science and Research Branch, Islamic Azad University, Semnan 35135-179, Iran
3. Design Department, Oil Turbo-Compressor Equipment, Tehran 11548-38415, Iran

ABSTRACT

Considering the essential and influential role of centrifugal compressors in a wide range of industries makes most of engineers research and study on design and optimization of centrifugal compressors. Centrifugal compressors are the key to part of oil, gas and petrochemical industries as well as gas pipeline transports. Since complete 3D design of the compressor consumes a considerable amount of time, most of active companies in the field, are profoundly interested in obtaining a design outline before taking any further steps in designing the entire machine. In this paper, a numerical algorithm, named ACDA (adapted compressor design algorithm) for fast and accurate preliminary design of centrifugal compressor is presented. The design procedure is obtained under real gas behavior, using an appropriate equation of state. Starting from impeller inlet, the procedure is continued on by resulting in numerical calculation for other sections including impeller exit, volute and exit diffuser. Clearly, in any step suitable correction factors are employed in order to conclude in precise numerical results. Finally, the achieved design result is compared with available reference data.

KEYWORDS

Process centrifugal compressor, adapted design algorithm, real gas.

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