Invention Grant
US09441835B2 System and method for fuel and steam injection within a combustor 有权
燃烧器内燃料和蒸汽注入的系统和方法

System and method for fuel and steam injection within a combustor
Abstract:
A system includes a gas turbine combustor configured to combust a fuel and an oxidant, such as O2 and O2 mixtures. The system also includes an aerodynamic peg disposed in the gas turbine combustor. The aerodynamic peg includes a first passage configured to convey a first fluid into the gas turbine combustor and a second passage configured to convey a second fluid into the gas turbine combustor. The first fluid and second fluid are different from one another.
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