DESIGN AND ANALYSIS OF AIRCRAFT JET ENGINE TURBINE BLADE USING ANSYS WORKBENCH

Abstract

This paper summarizes the design and analysis of Aircraft Jet Engine Turbine Blade, Catia is
used for design and analysis is done using Ansys Workbench for model generated by applying boundary
condition; this paper also includes specific post processing and life assessment of blade. We take an
opportunity to present this report on “Design and Analysis of Aircraft Jet Engine Turbine Blade” and
put before readers some useful information regarding this project. Drawn by list of priorities progress in
the design and structural analysis of Aircraft Jet Engine Turbine Blade is reviewed and presented for
generating huge performance. This project is motivated by the key role of blades in the performance of
jet engine turbine. The fundamentals of the associated physics are emphasized. Recent developments and
advancements have led to an increase and improvement in blade aerodynamics, stability and reliability.
This article is intended as a high-level review of design of the blade environment and current state of
structural design to aid further research in developing new and innovative blade technologies.