Optimization Design Of Axial Flow Compressor

January 2020
Vol-6, Issue-1
Paper ID: 11314
ISSN: 2395-4396
Downloads: 0

Abstract & Details

Research Area
Production Engineering
Keywords
Optimized Design Axial flow Compressor Blade 3D Solid Works CFD Analysis
Abstract
An axial compressor is a pressure producing machine. It is a rotating, airfoil-based compressor in which the working fluid principally flows parallel to the axis of rotation. This is in contrast with other rotating compressors such as centrifugal compressors, axi-centrifugal compressors and mixed-flow compressors where the air may enter axially but will have a significant radial component on exit. The energy level of air or gas flowing through it is increased by the action of the rotor blades which exert torque on the fluid which is supplied by an electric motor or a steam or a gas turbine. In this thesis, an axial flow compressor is designed and modeled in 3D modeling software SOLIDWORKS. The present design has 30blades, in this thesis it is replaced with 10 blades. The present used material is Alloy Steel; it is replaced with chromium alloy and Tungsten alloy. Structural analysis is done on the compressor models to verify the strength of the compressor. CFD analysis is done to verify the flow of air. The stress values are less for Tungsten alloy than the respective yield stress values for Chromium steel and Alloy steel. The stress value is less for Tungsten alloy than Chromium steel and Alloy steel, so using Tungsten alloy is better. By using 10blades the stresses are increasing, but are within the limits. CFD analysis is done to verify the flow of air. The outlet velocity is increasing for 10 blades; pressure is more for 30 blades. So it concluded that using Tungsten alloy and 10 blades is better for compressor blade.

Author Information

# Name Institute / Affiliation
1 Abdul Jalil Taleb Ahmed Otaifah Bhagwant University
2 Sagar Sharma Bhagwant University
3 Devesh Kumar Singh Bhagwant University
4 Riyadh Redhwan Abdullah Haidar Bhagwant University
5 YADRAM SINGH Bhagwant University

How to Cite

Use the following formats to cite this article in your research.

APA Style
Otaifah, Abdul Jalil Taleb Ahmed, Sharma, Sagar, Singh, Devesh Kumar, Haidar, Riyadh Redhwan Abdullah, & SINGH, YADRAM (2020). Optimization Design Of Axial Flow Compressor. International Journal of Advance Research and Innovative Ideas In Education, 6(1), 547-556.
MLA Style
Otaifah, Abdul Jalil Taleb Ahmed, et al. "Optimization Design Of Axial Flow Compressor." International Journal of Advance Research and Innovative Ideas In Education, vol. 6, no. 1, 2020, pp. 547-556.
IEEE Style
Abdul Jalil Taleb Ahmed Otaifah, Sagar Sharma, Devesh Kumar Singh, Riyadh Redhwan Abdullah Haidar, and YADRAM SINGH, "Optimization Design Of Axial Flow Compressor," International Journal of Advance Research and Innovative Ideas In Education, vol. 6, no. 1, pp. 547-556, 2020.
Vancouver Style
Otaifah Abdul Jalil Taleb Ahmed, Sharma Sagar, Singh Devesh Kumar, Haidar Riyadh Redhwan Abdullah, SINGH YADRAM. Optimization Design Of Axial Flow Compressor. International Journal of Advance Research and Innovative Ideas In Education. 2020;6(1):547-556.
Harvard Style
Otaifah, Abdul Jalil Taleb Ahmed, Sharma, Sagar, Singh, Devesh Kumar, Haidar, Riyadh Redhwan Abdullah, & SINGH, YADRAM (2020) 'Optimization Design Of Axial Flow Compressor', International Journal of Advance Research and Innovative Ideas In Education, 6(1), pp. 547-556.
Chicago Style
Otaifah, Abdul Jalil Taleb Ahmed, et al. "Optimization Design Of Axial Flow Compressor." International Journal of Advance Research and Innovative Ideas In Education 6, no. 1 (2020): 547-556.
Turabian Style
Otaifah, Abdul Jalil Taleb Ahmed, et al. "Optimization Design Of Axial Flow Compressor." International Journal of Advance Research and Innovative Ideas In Education 6, no. 1 (2020): 547-556.

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