Integration of Fluidic Nozzles in the New Low Emission Dual Fuel Combustion System for MGT Gas Turbines

Fluidic oscillators have proven their capabilities and advantages in terms of the generation oscillating jets without moving parts for many years, mainly experimental studies. In this paper, design, development, integration fluidic atomizers into liquid-fuel system dual-fuel low NOX Advanced Can Combustion (ACC) MAN Gas Turbines (MGT) are presented. The two-stage comprises a pressure-swirl nozzle as pilot stage an assembly four main premixed nozzles, based on technology. design features briefly presented, whereas focus lies functionality layout nozzles. complete integration, validation, verification innovative injection unit final fast fuel-switchovers, complexity, high reliability, dry emissions operation.