The analysis of work parameters of a turboprop engine fuelled by various fuels was done in the article. The
turboprop engine model was presented in the beginning. The main feature of this model is description of the flow in
the engine as semi-perfect gas model. By this way, the change of fumes chemical composition influence the gas
properties as heat constant and isentropic index are determined. Next energy balance of a compressor and turbine
was analysed and turbine pressure drop was evaluated. Finally, engine output power was determined. It was done for
selected fuels, which could be applied in the aero engines. The results of analyse were presented in the tables and
charts and discussed. Summary of the test results with the results for contemporary applied fuel allows drawing the
conclusions about the turboprop engine performance change by various fuel application. Main of them refers to the
point that higher combustion heat value of fuel and higher heat constant of fumes cause better engine work conditions
By this way the hydrogen seems to be perspective fuel of future, because its combustion heat value is three times JET
A-1 and by this way it is possible the engine fuel consumption will be lower.
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