Methods and systems to facilitate reducing NOx emissions in combustion systems

摘要

A gas turbine combustor system is provided. The gas turbine combustor system includes a combustion liner (50) including a center axis, an outer wall, a first end (56,62,80), and a second end (60,82), the outer wall is orientated substantially parallel to the center axis, a transition piece (52) coupled to the liner second end, the transition piece including an outer wall, and a plurality of lean-direct injectors (64) spaced axially along at least one of the liner outer wall and the transition piece outer wall.