Research Article

Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade

Volume: 10 Number: 2 April 30, 2022
TR EN

Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade

Abstract

In this study, the structural and thermal analysis of the final stage compressor rotor blades, which are currently used on-site, is performed by using the ANSYS program. For that reason, a 3D model of the existing compressor blade has been done. Later on, this model was transferred to the ANSYS program and analyzed. In the analysis, the parameters formed in the blade geometry were determined. By creating a design geometry with the selected parameters, the stress of the existing blade under operating conditions was examined. All external parameters in this study were taken from an F-class gas turbine operating under real field conditions. The stresses of the obtained values in different regions on the blade were examined. This study is also a reverse engineering study and the effects of real field conditions on the compressor blades have been analyzed.

Keywords

Supporting Institution

yok

Project Number

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Thanks

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References

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Details

Primary Language

English

Subjects

Engineering

Journal Section

Research Article

Publication Date

April 30, 2022

Submission Date

August 2, 2021

Acceptance Date

February 22, 2022

Published in Issue

Year 2022 Volume: 10 Number: 2

APA
Gerengi, M., & Polat, F. (2022). Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade. Duzce University Journal of Science and Technology, 10(2), 1045-1066. https://doi.org/10.29130/dubited.977192
AMA
1.Gerengi M, Polat F. Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade. DUBİTED. 2022;10(2):1045-1066. doi:10.29130/dubited.977192
Chicago
Gerengi, Mustafa, and Fikret Polat. 2022. “Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade”. Duzce University Journal of Science and Technology 10 (2): 1045-66. https://doi.org/10.29130/dubited.977192.
EndNote
Gerengi M, Polat F (April 1, 2022) Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade. Duzce University Journal of Science and Technology 10 2 1045–1066.
IEEE
[1]M. Gerengi and F. Polat, “Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade”, DUBİTED, vol. 10, no. 2, pp. 1045–1066, Apr. 2022, doi: 10.29130/dubited.977192.
ISNAD
Gerengi, Mustafa - Polat, Fikret. “Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade”. Duzce University Journal of Science and Technology 10/2 (April 1, 2022): 1045-1066. https://doi.org/10.29130/dubited.977192.
JAMA
1.Gerengi M, Polat F. Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade. DUBİTED. 2022;10:1045–1066.
MLA
Gerengi, Mustafa, and Fikret Polat. “Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade”. Duzce University Journal of Science and Technology, vol. 10, no. 2, Apr. 2022, pp. 1045-66, doi:10.29130/dubited.977192.
Vancouver
1.Mustafa Gerengi, Fikret Polat. Structural and Thermal Analysis of F Class Gas Turbine Compressor Blade. DUBİTED. 2022 Apr. 1;10(2):1045-66. doi:10.29130/dubited.977192

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