Invention Grant
US08500399B2 Method and apparatus for enhancing compressor performance 有权
提高压缩机性能的方法和装置

Method and apparatus for enhancing compressor performance
Abstract:
The present invention provides a non-axisymmetric flow member disposed in a duct of a gas turbine engine. The flow member narrows the area aft of a vane to reduce the cross sectional area through which a wake from the vane traverses.
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