| Issue |
MATEC Web Conf.
Volume 393, 2024
2nd International Conference on Sustainable Technologies and Advances in Automation, Aerospace and Robotics (STAAAR-2023)
|
|
|---|---|---|
| Article Number | 03001 | |
| Number of page(s) | 7 | |
| Section | Advancements in Aerothermal Analysis | |
| DOI | https://doi.org/10.1051/matecconf/202439303001 | |
| Published online | 13 March 2024 | |
Steady state design and thermal characteristics of a gas turbine blade with lateral holes using finite element analysis
1 Department of Mechanical and Automation Engineering, Agni College of Technology, Chennai, Tamilnadu 600 130, Bharat (India)
2 Centre for Additive Manufacturing, Chennai Institute of Technology, Malayambakkam, Tamil Nadu 600069, Bharat (India)
3 Department of Mechanical Engineering, Government College of Engineering, Bargur, Tamilnadu 635104, Bharat (India)
* Corresponding author: naamphd@gmail.com
Turbine blades are the separate components that make up the turbine section of a steam or gas turbine. The blades must transform the high-temperature, high-pressure gas that the combustor produces into energy. In gas turbines, the turbine blades are usually the limiting element. As gas temperatures rise, the amount of heat that reaches the blades will also grow dramatically, leading to their thermal failure. Because gas turbine blades must function in extremely high temperatures, cooling is crucial. After FEA simulation was conducted and radial perforations of 6, 9, and 12 were constructed to allow high-velocity cooling air to pass through, the cooling of the gas turbine blades was improved.
Key words: Gas Turbine Blade / Creo / Ansys / Thermal Analysis / FEA / and Lateral Holes1
© The Authors, published by EDP Sciences, 2024
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