首页>
外国专利>
Gas turbine premixer with radially staged flow passages and method for mixing air and gas in a gas turbine
Gas turbine premixer with radially staged flow passages and method for mixing air and gas in a gas turbine
展开▼
机译:具有径向分段流动通道的燃气轮机预混合器以及在燃气轮机中混合空气和气体的方法
展开▼
页面导航
摘要
著录项
相似文献
摘要
A burner for use in a combustion system of an industrial gas turbine. The burner includes a fuel/air premixer including a splitter vane defining a first, radially inner passage and a second, radially outer passage, the first and second passages each having air flow turning vane portions which impart swirl to the combustion air passing through the premixer. The vane portions in each passage are commonly configured to impart a same swirl direction in each passage. A plurality of splitter vanes may be provided to define three or more annular passages in the premixer.
展开▼