首页>
外国专利>
Gas Turbine Premixer with Cratered Fuel Injection Sites
Gas Turbine Premixer with Cratered Fuel Injection Sites
展开▼
机译:燃气轮机预混器,带有弯曲的燃油喷射点
展开▼
页面导航
摘要
著录项
相似文献
摘要
A premixer for a gas turbine combustor includes a swirler including a plurality of turning vanes that impart swirl velocity to airflow through the premixer, and at least one fuel injection site enabling fuel to mix with the airflow in the premixer. The fuel injection site terminates in a cratered hole. The cratered hole increases mixing efficiency and increases flashback/flameholding resistance.
展开▼