首页>
外国专利>
SYSTEM AND METHOD OF IMPROVING COMBUSTION STABILITY IN A GAS TURBINE
SYSTEM AND METHOD OF IMPROVING COMBUSTION STABILITY IN A GAS TURBINE
展开▼
机译:改善燃气轮机燃烧稳定性的系统和方法
展开▼
页面导航
摘要
著录项
相似文献
摘要
A combustor for a gas turbine engine having a compressor upstream of the combustor and a turbine downstream of the combustor. The combustor also includes a combustor chamber, an oxy-fuel pilot burner (104) centrally positioned at an end of the combustor chamber, and an air-fuel premix burner configured to at least partially premix air and fuel. The air-fuel premix burner surrounds the oxy-fuel pilot burner (104) in an annular configuration.
展开▼