Turbojet Engine

For the 2016-17 year, one of YUAA’s projects will be to research, design, build, test and optimize a small centrifugal flow turbojet engine capable of a sustained combustion, complete with built-in starters, sensors, fuel supply system and thrust measuring equipment. YUAA has never built a turbojet engine before, so both the team leader Kevin Liang ’19 and YUAA members are very excited to move ahead with the project.

Old-style airplane engines are piston-propeller internal combustion engines that, while able to provide sufficient thrust for low speed, low altitude cruising, fail to support ever-increasing demand on airplane’s performance. Such a demand for engines with higher thrust to weight ratio and less structural complexity was eventually met with the arrival of jet engines.

The very first generation of jet engines (and the simplest of which) is the turbojet, in which air is forced through a series of axial or centrifugal flow compressor stages to gain enough pressure and temperature before being mixed with fuel and ignited. The heated flow of high pressure exhaust will then go through stages of turbines (which could be thought of as the compressor blades reversed) to extract a fraction of the energy to drive the compressors before being ejected rearward to produce thrust. In this way, the turbojet can produce very high thrust at very low resistance, bulk weight, and high rpm.

For the past two months, members have been working on designing and constructing the engine. Since this project is both challenging and new to YUAA, Turbojet members will learn skills and gain experience that will prove invaluable for not only YUAA, but the wider aerospace community as well.