Invention Grant
US08418470B2 Gas turbine combustor bulkhead panel 有权
燃气轮机燃油舱壁板

Gas turbine combustor bulkhead panel
Abstract:
A section panel assembly for a bulkhead of a gas turbine combustor includes a section panel defining a rear or cold side and defining a front or hot side. The panel has a circumferential inner edge, a circumferential outer edge and radially extending first and second side edges each extending from the inner edge to the outer edge such that the inner and outer edges subtend a predetermined arc. The panel defines at least one opening extending from the rear side to the front side for receiving cooling air. The rear side includes a central lip extending about a periphery of the opening, and a circumferential rail spaced radially outwardly of and extending about the opening for defining a cavity region including the opening on the rear side of the section panel.
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