Invention Grant
US08528344B2 Bleed structure for a bleed passage in a gas turbine engine 有权
用于燃气涡轮发动机中的排放通道的排气结构

Bleed structure for a bleed passage in a gas turbine engine
Abstract:
A bleed structure for a bleed passage in a gas turbine engine includes a first wall portion defining a first side of an opening for the passage, and a second wall portion defining a second side, opposite the first side of the opening. The first and second wall portions end at different positions in an extension direction of the opening.
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