Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece
View Patent ↗A gas turbine combustor including a fuel nozzle for injecting mixed gas of fuel and air, a cylindrical liner for burning and reacting the mixed gas of fuel and air in a combustion chamber, a transition piece which is a flow path for leading combustion gas generated in the liner to turbine blades, and a transition piece flow sleeve for wrapping an outside surface of the transition piece, wherein a plurality of air introduction holes for introducing air into the transition piece flow sleeve are formed in regions of the transition piece flow sleeve excluding regions which are corner portions of the transition piece flow sleeve in a sectional direction thereof.
1. A gas turbine combustor comprising a fuel nozzle for injecting mixed gas of fuel and air, a cylindrical liner for burning and reacting the mixed gas of fuel and air in a combustion chamber, a transition piece which is a flow path for leading combustion gas generated in the liner to turbine blades, and a transition piece flow sleeve for wrapping an outside surface of the transition piece,
wherein a plurality of first air introduction holes are formed in regions which are corner portions of the transition piece flow sleeve in a sectional direction thereof, a plurality of second air introduction holes are formed in regions of the transition piece flow sleeve excluding the regions which are the corner portions of the transition piece flow sleeve, and
a diameter of the first air introduction holes formed in the regions of the corner portions of the section of the transition piece flow sleeve is made smaller than a diameter of the second air introduction holes formed in the regions of the transition piece flow sleeve excluding the regions of the corner portions.
2. The gas turbine combustor according to claim 1 , wherein:
the corner portions of the section of the transition piece flow sleeve are regions of radii of curvature, among regions of radii of curvature for specifying a form of an outside surface portion of the transition piece flow sleeve by regions of a plurality of radii of curvature of the outside surface portion of the transition piece flow sleeve, when a value of each of the radii of curvature for respectively specifying the form of the outside surface portion of the transition piece flow sleeve is smaller than values of the radii of curvature for respectively specifying the forms of a upper side and a lower side of the outside surface portion of the transition piece flow sleeve.