ET 796 Gas Turbine Jet Engine Didactic Equipment Vocational Training Equipment Thermal Lab Equipment
Small single-shaft gas turbine with thrust measurement using either kerosene or petroleum Features - gas turbine, operated as jet engine - open gas turbine process Learning objectives/experiments - behaviour during operation of a jet engine including start-up procedure - determination of the specific thrust - determination of the specific fuel consumption - determination of lambda (fuel-air ratio) Specification [1] experiments relating to the function and behaviour during operation of a jet engine [2] gas turbine with radial compressor and axial turbine as jet engine [3] single-shaft engine [4] protective grating for the jet engine [5] turbine mounted on moving base with force sensor for thrust measurement [6] electric starter for fully automatic start-up [7] additional remote control for display and control of the jet engine [8] software for data acquisition via USB under Windows 10 Technical data Jet engine - max. thrust: 80N at 120000min-1 - speed range 35000...120000min-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 - 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 230V, 50Hz, 1 phase 230V, 60Hz, 1 phase 120V, 60Hz, 1 phase UL/CSA optional LxWxH: 1230x800x1330mm Weight: approx. 112kg
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