Gas Turbine Jet Engine

Gas Turbine Jet Engine .

Specification: Gas Turbine Jet Engine

• Experiments relating to the function and behaviour during operation of a jet engine
• Gas turbine with radial compressor and axial turbine as jet engine
• Single-shaft engine
• Protective grating for the jet engine
• Turbine mounted on moving base with force sensor for thrust measurement
• Electric starter for fully automatic start-up
• Additional remote control for display and control of the jet engine

Technical Data

Jet engine

• Max. thrust: 82N at 117000min-1
• Speed range 35000...117000min-1
• Fuel consumption: max. 22L/h (full load)
• Exhaust gas temperature: 610°C
• Sound level at 1m distance: max. 130dB(A)
• Fuel: kerosene or petroleum + turbine oil
• Starting system: electric starter 
• 1 tank for fuel: 5L

Measuring ranges

• Differential pressure: 0...150mbar
• Combustion chamber pressure: 0...2,5bar
• Temperature: 2x 0...1200°C / 1x 0...400°C
• Speed: 0...120000min-1
• Fuel consumption: 0...25L/h
• Force: 0...+/-200N