Gas Turbine Jet Engine

Gas Turbine Jet Engine

Product Details:

X

Product Description

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

DIDAC INTERNATIONAL

* Tips on getting accurate quotes. Please include product name, order quantity, usage, special requests if any in your inquiry.



DIDAC INTERNATIONAL All Rights Reserved.(Terms of Use)
Developed and Managed by Infocom Network Ltd.