Development in Geared Turbofan Aeroengine

4th International Conference on Manufacturing, Optimization, Industrial and Material Engineering

Mohd Tobi, A.L.^1 ; Ismail, A.E.^1

Structural Integrity and Monitoring Research Group, Faculty of Mechanical and Manufacturing Engineering, Universiti Tun Hussein Onn Malaysia, Johor, Batu Pahat, Malaysia^1

关键词: Aero-engine;    Aircraft design;    Open rotors;    Pollutant gas;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/131/1/012019/pdf
DOI  :  10.1088/1757-899X/131/1/012019

来源: IOP

【 摘 要 】

This paper looks into the implementation of epicyclic gear system to the aeroengine in order to increase the efficiency of the engine. The improvement made is in the direction of improving fuel consumption, reduction in pollutant gasses and perceived noise. Introduction of epicyclic gear system is capable to achieve bypass ratio of up to 15:1 with the benefits of weight and noise reduction. Radical new aircraft designs and engine installation are being studied to overcome some of the challenges associated with the future geared turbofan and open-rotor engine.