Version 1
: Received: 29 November 2023 / Approved: 29 November 2023 / Online: 29 November 2023 (11:08:52 CET)
How to cite:
Kumar Jha, N.; Malve, B.S.; Gawde, R.V. Design and Optimization of Combustion Chamber for Gas Turbine Engine. Preprints2023, 2023111853. https://doi.org/10.20944/preprints202311.1853.v1
Kumar Jha, N.; Malve, B.S.; Gawde, R.V. Design and Optimization of Combustion Chamber for Gas Turbine Engine. Preprints 2023, 2023111853. https://doi.org/10.20944/preprints202311.1853.v1
Kumar Jha, N.; Malve, B.S.; Gawde, R.V. Design and Optimization of Combustion Chamber for Gas Turbine Engine. Preprints2023, 2023111853. https://doi.org/10.20944/preprints202311.1853.v1
APA Style
Kumar Jha, N., Malve, B.S., & Gawde, R.V. (2023). Design and Optimization of Combustion Chamber for Gas Turbine Engine. Preprints. https://doi.org/10.20944/preprints202311.1853.v1
Chicago/Turabian Style
Kumar Jha, N., Bhakti Sachin Malve and Rohit Vinod Gawde. 2023 "Design and Optimization of Combustion Chamber for Gas Turbine Engine" Preprints. https://doi.org/10.20944/preprints202311.1853.v1
Abstract
Gas turbine engines are widely used in various industries such as aviation, power generation, and marine propulsion due to their high efficiency and reliability. The combustion chamber of a gas turbine engine design contains a number of elements, including as the chamber's size and form, the fuel injection system, the ignition system, and the cooling system and it plays a critical role in the performance and efficiency of the engine. This research discusses the fabrication of a combustion chamber model for a gas turbine engine. The aim of this research is to develop a combustion chamber that is cost-effective, easily available, and can be fabricated in less time. The research covers the different types of combustion chambers used in gas turbine engines and compares their advantages and disadvantages. It then selects the best type of combustion chamber for the gas turbine engine based on its cost, availability, and fabrication time, Efficiency and high power to fuel ratio. The report also describes the fabrication process involved, including the techniques and materials used, along with safety precautions and environmental protection measures. Lastly, the research suggests future improvements and potential applications for the fabricated combustion chamber model.
Keywords
Aviation; Marine propulsion; Combustion chamber; high power to fuel ratio; Gas turbine engines
Subject
Engineering, Aerospace Engineering
Copyright:
This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
