Development of a High Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blads

Abstract

This project proposal is submitted to GATET at GTf :E for funding. The research programme envisages the Development of a high Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blades for Small Gas Turbine Engine". The novelty of the Project is to demonstrate a 2: 1 pressure ratio in single stage fan with tip diameter of 316mm, rotor tip speed of 470 m/s and rotational speed of 28400 rpm