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 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 …

An air-shielded fuel injection assembly for use in a combustion chamber of a turbine
assembly. The air-shielded fuel injection assembly generally includes a fuel manifold …

(57) ABSTRACT A pilot nozzle, a gas turbine combustor and a gas turbine are provided with
a nozzle main body having a fuel passage, a cover ring arranged at an outside of a front end …

A combustor arrangement for a gas turbine includes a first burner, a first combustion
chamber, a mixer for admixing a dilution gas to the gases leaving the first combustion …

Embodiments of the present disclosure provide an apparatus including: a first injector
located on a surface of a turbine nozzle of a turbine stage positioned downstream of a …

(57) ABSTRACT A gas turbine combustion chamber includes a fuel nozzle with a cylindrical
nozzle tube, in which a fluid flows, and a convexly formed nozzle cover, which is arranged …

(57) ABSTRACT A lance of a gas turbine burner includes an inner duct having inner
nozzles; an annular outer duct encircling the inner duct and having outer nozzles; and a …

Embodiments of the present disclosure provide an apparatus comprising: a reaction
chamber positioned between a first turbine stage of a power generation system and a …

US10544736B2 - Combustion chamber for adjusting a mixture of air and fuel flowing into
the combustion chamber and a method thereof - Google Patents US10544736B2 …