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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