Theoretical analysis and optimization of the performance of a hybrid engine

Analyzing the amount of fuel in the hybrid engine and battery cells helps to optimize the overall performance of the drone. Research has shown that different combinations of the amount in fuel level and battery cells will result in various outputs. This paper aims to determine the mathematical optim...

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Main Author: Ho, Xiu Ting
Other Authors: Chan Wai Lee
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2020
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Online Access:https://hdl.handle.net/10356/138777
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1387772023-03-04T19:51:35Z Theoretical analysis and optimization of the performance of a hybrid engine Ho, Xiu Ting Chan Wai Lee Lyu Chen School of Mechanical and Aerospace Engineering chan.wl@ntu.edu.sg and lyuchen@ntu.edu.sg Engineering::Mechanical engineering::Energy conservation Analyzing the amount of fuel in the hybrid engine and battery cells helps to optimize the overall performance of the drone. Research has shown that different combinations of the amount in fuel level and battery cells will result in various outputs. This paper aims to determine the mathematical optimization of the flight time after collecting all the possible combination outcomes. Building codes with all the assumptions and constraints, the State of Charge (SoC) curve and the available fuel curve demonstrates the relationship between both the hybrid engine and battery cells, and the flight time. In this context, the hybrid engine begins to charge the battery pack when the energy level reaches below a certain value. When the hybrid engine begins to operate, the available fuel curve decreases accordingly. This code also demonstrates that when the load demands a higher power to supply and yet battery cells alone could not support, the hybrid engine automatically provides power to the load. Based on the literature review done on hybrid engine and battery pack, configurations in the entire system of the drone and the internal configuration in battery pack will contribute to a huge difference in the outcome. It is proven that with a lower power load, the drone can fly thrice the amount of flight time as compared to the drone which requires a higher power load. This result indicates that a lower power load has an impact on the total overall flight time. Hence, it is recommended to have a smaller power load in order to save energy consumption of the battery pack and hybrid engine. A future simulation is also advised to be carried out for a parallel hybrid system as a comparison with the series hybrid system. This is to determine which configuration gives the best optimization in terms of endurance. Translating the code to simulation is also another factor to improve effectiveness and visualization Bachelor of Engineering (Mechanical Engineering) 2020-05-12T09:04:18Z 2020-05-12T09:04:18Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/138777 en A196 application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Mechanical engineering::Energy conservation
spellingShingle Engineering::Mechanical engineering::Energy conservation
Ho, Xiu Ting
Theoretical analysis and optimization of the performance of a hybrid engine
description Analyzing the amount of fuel in the hybrid engine and battery cells helps to optimize the overall performance of the drone. Research has shown that different combinations of the amount in fuel level and battery cells will result in various outputs. This paper aims to determine the mathematical optimization of the flight time after collecting all the possible combination outcomes. Building codes with all the assumptions and constraints, the State of Charge (SoC) curve and the available fuel curve demonstrates the relationship between both the hybrid engine and battery cells, and the flight time. In this context, the hybrid engine begins to charge the battery pack when the energy level reaches below a certain value. When the hybrid engine begins to operate, the available fuel curve decreases accordingly. This code also demonstrates that when the load demands a higher power to supply and yet battery cells alone could not support, the hybrid engine automatically provides power to the load. Based on the literature review done on hybrid engine and battery pack, configurations in the entire system of the drone and the internal configuration in battery pack will contribute to a huge difference in the outcome. It is proven that with a lower power load, the drone can fly thrice the amount of flight time as compared to the drone which requires a higher power load. This result indicates that a lower power load has an impact on the total overall flight time. Hence, it is recommended to have a smaller power load in order to save energy consumption of the battery pack and hybrid engine. A future simulation is also advised to be carried out for a parallel hybrid system as a comparison with the series hybrid system. This is to determine which configuration gives the best optimization in terms of endurance. Translating the code to simulation is also another factor to improve effectiveness and visualization
author2 Chan Wai Lee
author_facet Chan Wai Lee
Ho, Xiu Ting
format Final Year Project
author Ho, Xiu Ting
author_sort Ho, Xiu Ting
title Theoretical analysis and optimization of the performance of a hybrid engine
title_short Theoretical analysis and optimization of the performance of a hybrid engine
title_full Theoretical analysis and optimization of the performance of a hybrid engine
title_fullStr Theoretical analysis and optimization of the performance of a hybrid engine
title_full_unstemmed Theoretical analysis and optimization of the performance of a hybrid engine
title_sort theoretical analysis and optimization of the performance of a hybrid engine
publisher Nanyang Technological University
publishDate 2020
url https://hdl.handle.net/10356/138777
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