Jet Engine Test Rig

Order Code: 14132

Category: Thermodynamics Lab

Introduction: Jet engines are gas turbines which generate thrust. Jet engines are used on aircraft for propulsion due to their low weight and high performance.This trainer investigates the behaviour during operation of a jet engine. It includes the f...



SPECIFICATION

Introduction: Jet engines are gas turbines which generate thrust. Jet engines are used on aircraft for propulsion due to their low weight and high performance.This trainer investigates the behaviour during operation of a jet engine. It includes the following components: jet engine (with compressor, annular combustion chamber, turbine, and propelling nozzle), fuel system, starter and ignition system, and measurement and control equipment. The gas turbine works as an open cyclic process, with the ambient air being drawn out and fed back in

Specifications:

  1. Jet engine max. thrust: 80N at 120000min-1 speed range 35000…120000min-1
  2. fuel consumption: max. 22L/h (full load)exhaust gas temperature: 610°C sound level at 1m distance: max. 130dB(A)
  3. Fuel: kerosene or petroleum + turbine oil
  4. Starting system: electric starter 1 tank for fuel: 5L
  5. Measuring ranges differential pressure: 0…150 bar pressure: 0…2,5bar (combustion chamber)temperature: 2x 0…1200°C / 1x 0…400°C speed: 0…120000min-1 consumption: 0…25L/h (fuel)force: 0…±200N.

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