Published Paper Details:

The design of the turbine blade was delicate. The experimental test of turbine blade structure is delicate and more precious process. In this present work, a detailed design of turbine blade structure modeling done by using CATIA V5 R20 software. The static stress analysis is carried out to find the stresses of the turbine blade structure for different paraphernalia. The stresses are estimated with the help of ANSYS structural analysis software. One of the important structural factors of the aircraft is turbine blade which controls the machine. The turbine blade, which is mounted in the turbine section of the aircraft spurt machine. The material used in the Turbine blade is nickel predicated superalloy, which as high- strength admixture and high strength- to- weight rate and excellent fatigue resistance. The use of emulsion paraphernalia in the spurt machine of aircraft is getting further common, the sedulity demand for predicting and minimizing the product and conservation cost is rising. Still, the selection for the design and associated manufacturing process in the early design stage is so far largely experience and knowledge predicated and partly a political decision which creates a high cost. There is, therefore, a need to develop an approach for the optimal design of turbine blade structure subject to design conditions, paraphernalia, manufacturing process, and bearing in mind the cost constraints in the early stages of development. In order to gain a high-strength material, trials were made to make the turbine blade as light as possible as well as with a high structural strength These tasks are considered in the order and manner in which the inventor must handle them. Within these task areas, the critical aspects of the structural, performance, and physical boundary conditions that the structure design must satisfy are presented and the detailed procedure for modeling the turbine blade structure is also presented. The model is also exported into the analysis software to conduct the analysis. The analysis on the turbine blade model is conducted representing that the model when an advanced material analogous as titanium alloy and Inconel 625 is considered including nickel and chromium to check the strength. The idea is to give high-strength material that can perform in the turbine section where high temperature is there and high forces are acting on the turbine blade.