Rajni Verma, Dr. Rajesh Kumar Saluja
optimization process; hybrid-electric propulsion system; sustainability; aviation industry
This research work focuses on the design and optimization of a hybrid-electric propulsion system for a small general aviation aircraft, Hyperion. The study aims to estimate aerodynamic data, performance parameters, and optimize the propulsion system to achieve maximum efficiency.The concept of hybrid-electric propulsion is introduced, highlighting its advantages over traditional propulsion systems. The estimated aerodynamic data and performance parameters are used to determine the optimal design of Hyperion, which includes a combination of electric and internal combustion engines.The Hyperion program is then discussed, which involves the implementation of the hybrid-electric propulsion system and testing of the aircraft. The results of the optimization process show that the hybrid-electric propulsion system significantly improves the aircraft's fuel efficiency and reduces its emissions.In conclusion, this study demonstrates the potential of hybrid-electric propulsion systems in general aviation aircraft. The implementation of such systems could lead to significant improvements in fuel efficiency and environmental sustainability in the aviation industry.
Article Details
Unique Paper ID: 160280

Publication Volume & Issue: Volume 10, Issue 1

Page(s): 87 - 96
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