Sequential combustion constitutes a major technological step-change for gas turbines
applications. This design provides higher operational flexibility, lower emissions, and higher …

A combustion module for a combustor of a gas turbine includes an annular fuel distribution
manifold disposed at an upstream end of the combustion module. The fuel distribution …

6,374,594 B1 4/2002 Kraft et al. 2011 0146284 A1 6, 2011 Morimoto 6,442,946 B1 9, 2002
Kraft 2011 O247314 A1 10, 2011 Chila 6.450, 762 B1 9, 2002 Munshi 2011/0304.104 A1 …

A spine is proven to be subjected to a follower load which is a compressive load of
physiologic magnitude acting on the whole spine. The path of the follower load …

(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 …

A cooled fuel injector system of a combustor section of a gas turbine engine is provided. At
least a part of the fuel injector system is exposed to core gas flow traveling through the …

A hot gas path duct or unibody liner for a gas turbine includes a main body having a forward
end and an aft end. The main body defines a cross-sectional flow area and an axial flow …

A combustion liner for a gas turbine combustor includes an annular main body having a
forward end axially separated from an aft end, and a transitional intersection defined …

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 …

It has been observed that tension twins (TTs) are triggered in rolled polycrystalline
magnesium alloys under tensile loading applied along the rolling direction (RD) or the …