CONCEPTUAL DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER FOR A 65 KW MICRO GAS TURBINE

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AKHLAGHI M.; MOBASHER AMINI A.; JAZAYERI MOGHADDAS SH.; AZIZI Y.

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Journal: FLUID MECHANICS AND AERODYNAMICS JOURNAL Year:2015 | Volume:4 | Issue:1 (15) Page(s): 1-16

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Title

CONCEPTUAL DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER FOR A 65 KW MICRO GAS TURBINE

Author(s)

AKHLAGHI M. | MOBASHER AMINI A. | JAZAYERI MOGHADDAS SH. | AZIZI Y. | Issue Writer Certificate

Keywords

MICRO TURBINEQ2

MICRO COMPRESSORQ2

CENTRIFUGAL COMPRESSORQ2

DIFFUSION RATIOQ2

SLIP FACTORQ2

Abstract

The aim of this study is designing the impeller of a CENTRIFUGAL COMPRESSOR in order to supply pressure ratio for a 65 kW micro gas turbine. First, the primary thermodynamic analysis has been conducted for the considered cycle using a home made code. Herein, the compressor pressure ratio was considered to be 4. The obtained thermal efficiency was 25.64%. Then, the design of MICRO COMPRESSOR in 90,000 rpm rotational speed was conducted and its dimensions were extracted. The designed MICRO COMPRESSOR has 9 main blades and 9 splitter blades. The outer diameter of the compressor impeller was 95.5 mm. Then, the three-dimensional geometry of the compressor impeller was extracted. Finally, to validate the designed impeller, CCD software was used and CFD analysis has been conducted on generated geometry, using CFX.

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APA: Copy

AKHLAGHI, M., MOBASHER AMINI, A., JAZAYERI MOGHADDAS, SH., & AZIZI, Y.. (2015). CONCEPTUAL DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER FOR A 65 KW MICRO GAS TURBINE. FLUID MECHANICS AND AERODYNAMICS JOURNAL, 4(1 (15)), 1-16. SID. https://sid.ir/paper/245501/en

Vancouver: Copy

AKHLAGHI M., MOBASHER AMINI A., JAZAYERI MOGHADDAS SH., AZIZI Y.. CONCEPTUAL DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER FOR A 65 KW MICRO GAS TURBINE. FLUID MECHANICS AND AERODYNAMICS JOURNAL[Internet]. 2015;4(1 (15)):1-16. Available from: https://sid.ir/paper/245501/en

IEEE: Copy

M. AKHLAGHI, A. MOBASHER AMINI, SH. JAZAYERI MOGHADDAS, and Y. AZIZI, “CONCEPTUAL DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER FOR A 65 KW MICRO GAS TURBINE,” FLUID MECHANICS AND AERODYNAMICS JOURNAL, vol. 4, no. 1 (15), pp. 1–16, 2015, [Online]. Available: https://sid.ir/paper/245501/en

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