Invention Grant
US08166767B2 Gas turbine combustor exit duct and hp vane interface 有权
燃气轮机燃烧器出口管和hp叶片接口

Gas turbine combustor exit duct and hp vane interface
Abstract:
An assembly for a gas turbine engine includes a combustor and a vane assembly disposed downstream thereof. A portion of an outer platform of the vane assembly defines an axial sliding joint connection with the combustor, and includes a plurality of depressions located in an outer circumferential surface thereof opposite the combustor. The depressions are disposed in regions of expected higher thermal growth about the circumference of the outer platform such that thermal growth of the entire outer platform is substantially uniform circumferentially therearound.
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