Axial Flow Gas Turbine
(TD-016)
  • Investigation of behavior and operation of jet engine.
  • Determination of engine thrust.
  • Calculation efficiency of engine.
  • Max. thrust : 80N.
  • Fuel used kero/diesel.
  • Exhaust Temperature: 700°C.
  • Fuel consumption: 270 g/min.
  • Axial Flow Gas Turbine (TD - 016)
  • Hard copy user manual

In this gas turbine jet engine training system, trainees will get familiarized with the working principle and operation behavior of such systems. Trainees will also get in touch with the structure of gas turbine jet engines and the function of each component.

                                     
  • The Trainer allows the trainees to investigate the behavior and operation of axial gas turbine.
  • The axial flow gas turbine is fixed firmly to enable accurate measurement of thurst produced by the turbine.
  • The axial flow gas turbine is supplied with sensors in key point to measure effective parameters such as pressure, temperature and speed.
  • The trainer has digital displayes to display the measured parameters and switches to control the axial flow turbine.
  • The axial flow gas turbine is provided with an easy and simple ignition system based on glow plug .
  • The axial flow gas turbine is provided with tough and transparent cover to make the device completely safe.