Authors: Kamlesh Bachka, Mukund Kavekar, Aniket Akhade
Abstract: This paper borders around analysis of compressor blade. The Impeller blade is a rotating part which imparts highly pressurized air. Impeller blade is critical part of turbocharger which has shown increasing growth of failure damaging assembly. It deals with Static and thermal analysis of Impeller blade which is made up of INCONEL N06230 to estimate its performance. The causes of failure for blade have also been found out. The investigation has been done using Soild Works 2012 and ANSYS 10.0 software. Solid Works 2012 is used for modeling of compressor blade and analysis has been done by ANSYS10.0 software. An attempt has been made to investigate the effect of induced stresses, pressure and temperature on the Impeller blade. A structural analysis has been carried out to investigate the stresses and displacements of the Impeller blade. A thermal analysis has been carried out to investigate the thermal gradient and thermal stress.
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