The multi-heat addition turbine engine

Abstract

A study was made of multiheat addition turbine engines (MHATE) which incorporate multiple burners and turbines. The types of engines studied were a MHATE two-spool duct burning turbo fan and a single-spool turbojet. A conventional duct burning turbofan and a TBE turbojet were studied for comparison. Comparisons of the thrust and specific fuel consumption of the engines were made for maximum burner temperatures of 2400 F and 2900 F. The results of the study show that the MHATE engines with maximum burner temperatures of 2400 F obtain the same thrust and specific fuel consumption as the conventional engines having maximum burner temperatures of 2900 F. This would have the potential for significant reductions in harmful emissions of NO(x). When the MHATE and conventional engines have the same maximum burner temperatures, the MHATE engines achieve 15 to 50 percent more thrust.