Turbine Impeller Blade Using Advanced Surface Modeling

Abstract

The Turbine Impeller Blade Using Advanced Surface Modeling project focuses on the design and development of a turbine impeller blade using advanced computer-aided surface modeling techniques. Turbine blades are critical components in power generation and energy conversion systems, where their geometry directly influences aerodynamic performance, efficiency, and structural reliability. Therefore, accurate and smooth blade modeling is essential for achieving the required performance. In this project, a detailed 3D turbine impeller blade is developed using advanced surface modeling techniques. Important parameters such as blade profile, twist, thickness, leading edge, trailing edge, blade angle, and span are considered during the design process. Surface modeling techniques are used to create smooth and continuous blade surfaces with accurate geometric transitions. The developed blade model can be evaluated using CAD-based analysis and computational simulation to study its aerodynamic and geometric characteristics. The model can be examined for surface continuity, blade shape, flow direction, and potential regions of performance loss. Different blade profiles and design parameters can also be modified and compared to obtain an improved blade configuration. The main objective of this project is to demonstrate how advanced surface modeling can be used to create an accurate and optimized turbine impeller blade. The approach reduces design complexity and provides greater flexibility compared with conventional solid modeling methods. The developed model can serve as a foundation for further CFD analysis, structural analysis, manufacturing, and performance optimization of turbine blade systems.