Retrofit Micro Turbojet Engine AERO-16 Berbasis Turbocharge HOLSET HX-35

Abstract

Gas turbine engine is a type of engine that performs internal combustion. The engine works by converting thermal energy into mechanical energy, where the thermal energy is generated from the combustion chamber and the mechanical energy is generated from the turbine rotation. This research discusses in detail the manufacturing process of the Micro Turbojet Engine Aero-16. Before manufacturing, a literature study is carried out and information gathering about what data needs to be prepared as a benchmark for manufacturing. The Micro Turbojet Engine Aero-16 has the main components in the form of a compressor, combustion chamber and turbine. The engine requires other components such as a compressor shroud, flange housing, housing, stator tube and exhaust nozzle. The manufacturing of components is used to produce a perfect micro turbojet engine duty cycle. After the manufacturing process is complete, measurements between the design blue print and the components of the manufacturing results have been carried out. There are dimensional differences in some components with the design blue print, due to the lack of available manufacturing tools. From this research, the Micro Turbojet Engine Aero- 16 has been successfully realized, and it is hoped that it will produce useful specifications and features to facilitate learning about the gas turbine engine working system on an airplane