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Introduction:

Hybrid electric propulsion systems have emerged as a promising technology for reducing carbon emissions and improving the efficiency of aircraft operations. The integration of electric propulsion systems into traditional gas turbine engines has the potential to significantly decrease fuel consumption and emissions, while also enhancing the overall performance of aircraft. This thesis aims to explore the design, implementation, and impact of hybrid electric propulsion systems for aircraft.

Chapter 1: Introduction
1.1 Introduction
1.2 Background of study
1.3 Problem Statement
1.4 Objective of Study
1.5 Limitation of Study
1.6 Scope of Study
1.7 Significance of Study
1.8 Structure of the Thesis
1.9 Definition of Terms

Chapter 2: Literature Review
2.1 Introduction to Hybrid Electric Propulsion Systems
2.2 Evolution of Hybrid Electric Propulsion Systems
2.3 Benefits of Hybrid Electric Propulsion Systems
2.4 Challenges of Hybrid Electric Propulsion Systems
2.5 Existing Hybrid Electric Aircraft Projects
2.6 Comparison of Hybrid Electric and Conventional Aircraft
2.7 Environmental Impact of Hybrid Electric Propulsion Systems
2.8 Regulatory Framework for Hybrid Electric Aircraft
2.9 Future Trends in Hybrid Electric Propulsion Systems
2.10 Conclusion

Chapter 3: System Design and Methodology
3.1 Introduction to System Design
3.2 Components of Hybrid Electric Propulsion Systems
3.3 Integration of Electric and Gasoline Propulsion Systems
3.4 Design Considerations for Hybrid Electric Aircraft
3.5 Simulation and Modeling of Hybrid Electric Propulsion Systems
3.6 Performance Analysis of Hybrid Electric Propulsion Systems
3.7 Cost Analysis of Hybrid Electric Propulsion Systems
3.8 Methodology for System Optimization

Chapter 4: System Implementation
4.1 Introduction to System Implementation
4.2 Selection of Components for Hybrid Electric Propulsion Systems
4.3 Integration of Components
4.4 Testing and Validation of Hybrid Electric Propulsion Systems
4.5 System Performance Evaluation
4.6 Challenges Faced during Implementation
4.7 Lessons Learned
4.8 Future Directions for System Implementation

Chapter 5: Conclusion and Summary
5.1 Recap of Key Findings
5.2 Implications of Research
5.3 Recommendations for Future Research
5.4 Conclusion

Thesis Overview:

Hybrid electric propulsion systems for aircraft have gained significant interest in recent years due to their potential to reduce emissions and improve fuel efficiency. This thesis provides a comprehensive examination of the design, implementation, and impact of hybrid electric propulsion systems for aircraft.

The literature review explores the evolution of hybrid electric propulsion systems, the benefits and challenges associated with these systems, existing hybrid electric aircraft projects, and the regulatory framework for hybrid electric aircraft. Additionally, the literature review examines the environmental impact of hybrid electric propulsion systems and future trends in this technology.

The system design and methodology chapter delves into the components of hybrid electric propulsion systems, the integration of electric and gasoline propulsion systems, design considerations for hybrid electric aircraft, simulation and modeling techniques, performance analysis, cost analysis, and optimization methodologies.

The system implementation chapter focuses on the selection of components, integration of components, testing and validation processes, performance evaluation, challenges faced during implementation, lessons learned, and future directions for system implementation.

Overall, this thesis provides valuable insights into the design, implementation, and impact of hybrid electric propulsion systems for aircraft, highlighting the potential benefits of this technology and offering recommendations for future research in this field.

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