Turbine Burners: Performance Improvement and Challenge of Flameholding

摘要

The turbine burner holds promise as a major technological advancement for gas-turbine engines. The thermal-cycle analysis for augmentative combustion in the passages of the turbine on a turbojet or turbofan engine shows the potential for large percentage improvements in engine performance. Various types of compact combustors have been studied and can be used as augmentative combustors between turbine stages.