A swirler including an annular housing with limiting walls. At least two vanes are arranged in
the annular housing including the sidewalls of the swirler. The leading edge area of each …

8,028,529 B2 10/2011 8,069,676 B2 12/2011 8,176.739 B2 5, 2012 8, 177,547 B2 5, 2012
2002fOO11070 A1 1, 2002 2005. O13. 0089 A1 6, 2005 2005/026861.6 A1 12/2005 …

(57) ABSTRACT A fuel lance is disclosed for injecting a gaseous and/or liquid fuel mixed
with air into an axial hot gas flow flowing through a sequential combustor of a gas turbine …

The present invention relation to a burner for a combustion chamber of a gas turbine with a
mixing and injection device. The mixing and injection device includes a limiting wall that …

A burner head for a burner defines a burner longitudinal axis along which the burner
extends. The burner head includes a base body and at least one oxidant duct defining a …

The present invention generally relates to a sequential combustor for a gas turbine having
second and/or subse quent stages of a re-heat, sequential or axially-staged com bustion …

Disclosed is a fuel injector device having a body with a leading edge and a trailing edge and
defining a streamwise direction from the leading edge to the trailing edge, the fuel injector …

(57) ABSTRACT A burner for a combustion chamber of a gas turbine with a mixing and
injection device, which includes a limiting wall that defines a gas-flow channel and at least …

(57) ABSTRACT A method is disclosed for controlling fuel injection in a reheat combustor of
a gas turbine combustor assembly including a combustor casing defining a gas flow channel …

US20140053569A1 - Method for mixing a dilution air in a sequential combustion system of
a gas turbine - Google Patents US20140053569A1 - Method for mixing a dilution air in a …