Design and Analysis of Composite Propeller Blade for Aircraft |
Author(s): |
| K. Ashok , Lingayas Institute of Management and Technology; Kola Bhanu Krishna, Lingayas Institute of Management and Technology; Saidu Venkanna Babu, Lingayas Institute of Management and Technology; Bolla Rajesh Kumar, Lingayas Institute of Management and Technology; Avula Vamsi Krishna, Lingayas Institute of Management and Technology |
Keywords: |
| Propeller Blade, Aircraft R14.5 |
Abstract |
|
In this project, the work basically deals with the modelling and analysis of the propeller blade of an aircraft for its strength. A propeller blade is complex 3D model geometry. This requires high end modelling CAD software is used for generating the blade model in CATIA V5 R20. This paper consists of brief details about Fiber Reinforced Plastic materials and the advantages of using composite propeller over the conventional metallic propeller blade. This project focus on the metal and composite strength analysis of the propeller blade carried out by using the finite element analysis. By using ANSYS software static and modal analysis were carried out for isotropic material and also we are conducted linear layer analysis using orthotropic materials. In this work two different types of propeller i.e. Aluminium6061 and 7075, E-glass and carbon fibre, were studied using FEA techniques. |
Other Details |
|
Paper ID: IJSRDV10I40413 Published in: Volume : 10, Issue : 4 Publication Date: 01/07/2022 Page(s): 206-225 |
Article Preview |
|
|
|
|
