Invention Grant
US09239166B2 Gas turbine diffuser with flow separator 有权
带流量分离器的燃气轮机扩散器

Gas turbine diffuser with flow separator
Abstract:
A diffuser for use in a gas turbine engine, the diffuser having a first wall, a second wall, and a flow separator. The first and second wall define an annular cavity, with the annular cavity having an inlet. The first and second wall also forming a prediffuser that is proximate the inlet, and a dump region distal the inlet. The flow separator extends from the first wall into the annular cavity.
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