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Working Model of Turbojet Engine

                Yashwant A P1, Tanushree Kale2, Nikita Mane3, Purva Rupavate4& Gaurav Bankar5

1234Pune Institute of Aviation Technology Affiliated to Savitribai Phule Pune University, INDIA

1E-mail: yashwantpurwant.puneit@gmail.com

2E-mail: tanushreekale.puneiat@gmail.com

3E-mail: nikitamane.puneiat@gmail.com

4E-mail: purvarupavate.puneiat@gmail.com

5E-mail: gauravbankar@puneiat.edu.in

Abstract – The project made to show the working model of Turbojet Engine. The turbojet engine operates on the Brayton cycle and features four primary stages: air intake, compression, combustion, and exhaust. The turbo-jet engine is for high speeds. The working model shows how atmospheric air is taken in and compressed using a multi-stage axial or centrifugal compressor. The compressed air then enters the combustion chamber, where it mixes with fuel and undergoes ignition, producing high-energy exhaust gases. These gases rapidly expand through a turbine, extracting mechanical energy to drive the compressor and producing thrust as they accelerate through a nozzle to generate forward propulsion. This model serves as an educational tool, illustrating critical concepts such as the conversion of chemical energy into kinetic energy.

Key Words: Turbojet Engine, Air Intake, Compression, Combustion, Exhaust, Centrifugal Compressor,

Chemical Energy, Kinetic Energy.