The invention provides an axial grading
turbofan engine based on
methanol fuel afterburning, and belongs to the technical field of aero-engines. The problems that when an existing
jet fuel with the
high carbon content serves as a
raw material, the carbon emission of a
turbofan engine is high, the overall
NOx is high, and the heat efficiency is difficult to further improve are solved. Through axial grading afterburning, the fuel
utilization rate is increased, thrust is improved, carbon emission is reduced, the performance of the
turbofan engine is improved, distribution of fuel in the axial position is optimized, the fuel amount of a head
combustion area is reduced, meanwhile, the supply amount of the fuel on the two stages can be flexibly adjusted and controlled, a more reasonable air distribution mode is matched, and the
combustion efficiency of the turbofan engine is improved. And the overall
NOx level can be effectively reduced. The performance of the engine is improved by supplying
methanol fuel into the afterburning chamber, the use of
aviation kerosene is reduced through afterburning of
methanol, and meanwhile, the stability of thrust is guaranteed. The method is more environment-friendly and low in storage and
transportation cost, and can utilize the existing fuel infrastructure as a
liquid fuel system.