Invention Grant
US07089742B2 Wall elements for gas turbine engine combustors 有权
燃气轮机发动机燃烧器的壁元件

Wall elements for gas turbine engine combustors
Abstract:
A wall element (29) for a wall structure (21) of a gas turbine engine combustor (15). The wall element (29) comprises a main member (36) with an upstream edge region (30) and a downstream edge region (31). A plurality of heat removal members (38) are provided on the main member (36). The downstream edge (35) of the wall element and/or the downstream facing surface of the heat removal members closest to the downstream edge (35) are provided with a thermally resistant coating.
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