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US08438855B2 Slotted compressor diffuser and related method 有权
开槽压缩机扩散器及相关方法

Slotted compressor diffuser and related method
Abstract:
A compressor diffuser for a gas turbine includes: a compressor diffuser having an upstream end and a downstream end, the downstream end defined by a peripheral annular edge, the annular edge formed with a plurality of substantially axially-oriented slots extending from an opening at the downstream edge in an upstream direction.
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