Invention Application
US20140096529A1 SYSTEM AND METHOD FOR FUEL AND STEAM INJECTION WITHIN A COMBUSTOR 有权
燃料和蒸汽喷射在燃烧器中的系统和方法

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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