Optimization and Analysis of an Elite Electric Propulsion System

Abstract

Verbatim from Embry-Riddle Scholarly Commons. Not paraphrased, not summarized.

Abstract- Electric propulsion has a promising system to create new possibilities in this technological era as well as control the harmful gaseous emission. This paper put a vision on several parameters of electric propulsion. The engine’s performance is comparable to the current propulsion devices and provides a lightweight solution to the robust technologies’ dependent on chemical energy sources. There are a plethora of factors which is enhanced by electric propulsion such as, overall efficiency, capabilities, and robustness of future air vehicles as well as mainly overcome from exhaust hazards. Electric propulsion systems have the potential of utilizing the electrically-driven propulsion system which is coupled electrically to power-generating devices. As a result, the electric propulsion system operated with greater flexibility and the synergistic benefits of aero-propulsive coupling and enhance performance in comparison with traditional designs. The experimentally calculated thrust of the engine model is approximately 547.6365, Newton.

Authors

• Singh, Mehakveer Embry-Riddle Aeronautical University
• Yadav, Kapil Embry-Riddle Aeronautical University
• Singh, Satnam Embry-Riddle Aeronautical University
• Chumber, Vikas Embry-Riddle Aeronautical University
• Chavhan, Harikrishna Embry-Riddle Aeronautical University

Keywords

• Electric Propulsion
• Electric Fan Engine
• Harmful Emission
• Thrust.
• Aeronautical Vehicles
• Propulsion and Power
• Systems Engineering and Multidisciplinary Design Optimization