SYSTEM HAVING A FUEL NOZZLE AND METHOD

摘要

A gas turbine system 10 include a first body including a central passage 160 extending from a mixing region to a central outlet at a first downstream end portion of the first body, a fuel outlet in the mixing region 96, an oxidant outlet in the mixing region, and an outer passage including a first passage extending in a downstream direction toward the first downstream end portion and a second passage extending in an upstream direction from the first downstream end portion into the mixing region.