Review of Structural and Thermal Analysis of Gas Turbine Blade

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ISSN: 2278-0149 (Online)
Short Title: Int. J. Mech. Eng. Robot. Res.
Frequency: Bimonthly
DOI: 10.18178/ijmerr
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Prof Richard (Chunhui) Yang

Professor of School of Engineering, Design and Built Environment, Western Sydney University, Australia. His research interests cover Industry 4.0, Additive Manufacturing, Advanced Engineering Materials and Structures (Metals and Composites), Multi-scale Modelling of Materials and Structures, Metal Forming and Metal Surface Treatment.

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Home > Articles > All Issues > 2014 > Volume 3, No. 2, April 2014 >

G D Ujade1 and M B Bhambere2

1.Advance Manufacturing & Mech. System Design, SSGMCE, Shegaon, India.
2.Mechanical Engineering Department, SSGMCE, Shegaon, India.

Abstract— The gas turbine obtains its power by utilizing the energy of burnt gases and the air which is at high temperature and pressure by expanding through the several rings of fixed and moving blades. Since the turbine blades are working at high temperature and pressure there are extreme stresses developed on turbine blades. The first centrifugal stresses act on the blade due to high angular speeds, and second is thermal stresses that arise due to temperature gradient within the blade material. The present paper is review of various analyses done on turbine blades and there are various factors affects on turbine blade. This paper will be helpful for those who are working in the area of power plants.

Index Terms— Turbine blade, Thermal analysis, FEM

Cite: G D Ujade and M B Bhambere, " Review of Structural and Thermal Analysis of Gas Turbine Blade," International Journal of Mechanical Engineering and Robotics Research, Vol. 3, No. 2, pp. 347-352, April 2014.