Method of injecting combustion reactants into a combustor
摘要
A combustion device used in gas turbine engines that produces propulsion or rotates a shaft for power generation includes an annular combustor with a system of fuel and air inlet passages and nozzles that results in a flameless combustor, such that there is not an anchored flame as in typical gas turbine combustors. The fuel and air inlets are placed at various longitudinal locations and circumferentially spaced, and take on several different configurations where some nozzles inject only air and others inject a rich fuel-air mixture. The combustion device provides an optimal mixing of fuel and air as well as creates an environment for combustion that reduces pollutant emissions reducing the need for costly pollution control devices, and enhances ignition and flame stability, reduces piloting issues and improves vibration reduction.
申请公布号
EP2748531(A1)
申请公布日期
2014.07.02
申请号
EP20110871279
申请日期
2011.08.22
申请人
TOQAN, MAJED;GREGORY, BRENT ALLAN;REGELE, JONATHAN DAVID;YAMANE, RYAN SADAO
发明人
TOQAN, MAJED;GREGORY, BRENT ALLAN;REGELE, JONATHAN DAVID;YAMANE, RYAN SADAO