(57) ABSTRACT A fuel injector in a combustor apparatus of a gas turbine engine. An outer
wall of the injector defines an interior Vol ume in which an intermediate wall is disposed. A …

A system includes a multi-tube fuel nozzle including a fuel nozzle head that includes an
outer wall surrounding a chamber. The outer wall includes a downstream wall portion …

(57) ABSTRACT A method is provided for fuel injection in a sequential com bustion system
comprising a first combustion chamber and downstream thereof a second combustion …

(57) ABSTRACT A burner for a combustion chamber of a turbine, with an injection device for
the introduction of at least one gaseous and/or liquid fuel into the burner is proposed. The …

A burner tip having a converging portion with a multiplicity of ports. The ports are sized and
positioned so that a substantially constant ratio is maintained between any selected cross …

The disclosure relates to a burner Such as for a secondary combustion chamber of a gas
turbine with sequential com bustion having a first and a second combustion chamber, with …

A burner, such as for a secondary combustion chamber of a gas turbine with sequential
combustion having first and second combustion chambers, includes an injection device for …

The lance of a burner includes a body that defines a first duct with first nozzles for injecting a
liquid fuel and a second duct with second nozzles for injecting a gaseous fuel. Outlets of the …

388 A. 338. s 1 eer et al. International Search Report (PCT/ISA/210) issued on Jan. 20,
2011, 2009, 0081048 A1 3, 2009 B. tal by the European Patent Office as the International …

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 …