Invention Grant
US08425188B2 Diffuser pipe and assembly for gas turbine engine 有权
用于燃气轮机的扩散管和组件

Diffuser pipe and assembly for gas turbine engine
Abstract:
A diffuser pipe (38) of a compressor diffuser assembly (28) for gas turbine engines defines a depressed local area (58) in the pipe wall of an upstream section of the diffuser pipe (38). The depressed local area (58) is bent into the diffuser pipe (38) to reduce the accumulation of fluid boundary layer and improve stall margin of the diffuser pipe (38).
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