The present application belongs to the technical field of
aviation turbine engine, and discloses an intercooling regenerative water enhanced
turbofan engine, which comprises a
Brayton cycle and a supercritical
water vapor Rankine cycle in a main flow path, the two cycles are closely related, and are coupled by increasing a
steam turbine, a steam generator and a condenser. The
steam turbine does work to supply a high-pressure compressor, and
liquid water appears at the
steam turbine outlet, the
liquid water is injected into the high-low pressure compressor for intercooling, the
intermediate temperature of the compressor is reduced, the
power consumption of the compressor is reduced, the unit working medium thrust is improved, the
intercooler is saved, and the application is facilitated, the low-temperature steam at the steam
turbine outlet can be injected into the low-pressure
turbine inlet for cooling, and the
cold air amount can be effectively reduced and the unit working medium thrust can be improved. The present application effectively overcomes the high
temperature difference and large loss of the steam generator, compared with the conventional
aviation engine, the
total efficiency of the engine can be greatly improved, the fuel consumption rate and the
pollutant emission are reduced.