Int. Cl.(57) F02G 3/00(2006.01) An improved mixing tube design and fuel nozzle that allows
FO2C I/00(2006.01) for a more uniform and thorough mixing of fuel and air being (52) US Cl …

Primary Examiner Craig Kim (74) Attorney, Agent, or Firm-Dority & Manning, PA (57)
ABSTRACT A system for dissipating fuel egress includes a fuel injector and a fuel supply …

A fuel injector is provided for the radial introduction of a fuel/air mixture to a combustor. The
fuel injector includes a frame having interior sides defining an opening for passage of a first …

A fuel injector for a gas turbine combustor includes side wall fuel injection bodies extending
between opposite end walls. Each side wall fuel injection body defines a fuel plenum and …

A fuel injector is provided for the radial introduction of a liquid fuel/air mixture to a combustor.
The fuel injector includes a body having a frame that defines an inlet portion and an outlet …

A fuel injector is provided for the radial introduction of a fuel/air mixture to a combustor. The
fuel injector includes a frame having interior sides defining an opening for passage of a first …

In a gas turbine combustor having an inner and outer liner defining an annular combustion
chamber, at least an annular scoop ring provided on each inner and outer combustor liner …

A combustor section for a gas turbine engine includes a can combustor with a combustion
chamber. A pilot fuel injection system is in axial communication with the combustion …

A combustor section for a gas turbine engine includes an outer wall assembly and an inner
wall assembly inboard of the outer wall assembly to define an annular combustion chamber …

A combustor comprises an annular combustor chamber formed between the inner and outer
liners, the annular combustor chamber having a central axis. Fuel nozzles are in fluid …