A conception of a two-combustor turbofan engine is the main scope of this paper. At the beginning, the problems
of turbofan engines development are briefly discussed as a background of this work. In this part the turbofan engines
innovation activities are presented. It is mentioned the engine’s innovations consists of many aspects but some
important ones are: lowering of production operation cost, maintenance, reduction of noise and exhaust gases
emission while engine reliability should stay on the same level or event increase. Next, the conception of turbofan
engine with two combustors is presented in this context. Some positive aspects for environment, production and
maintenance of such engine are discussed. Then the thermodynamic cycle of two-combustor engine is presented and
analysed. On this basis, the engine numerical model is prepared. Next, some information about the model
simplifications and calculations done to determine performance of the engine is presented. Then the results of the
simulation calculations of the engine performance are presented and discussed. The relationship of engine thrust and
specific fuel consumption vs. engine flight conditions are shown. Based on the results there were discussed the
advantages and disadvantages of two combustors engine as an airplane propulsion are specified. The conclusions are
formulated and presented in the last part of the paper.
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