Radial Diffuser Vane for Centrifugal Compressors
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United States of America Patent
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Issued Date -
Aug 29, 2013
app pub date -
Aug 12, 2010
filing date -
Aug 12, 2010
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Abstract
A turbo machine comprising a rotor assembly comprising at least one impeller, a bearing connected to the rotor assembly, wherein the bearing is configured to rotatably support the rotor assembly, and a stator comprising at least one diffuser connected to an exit portion of the at least one impeller, wherein the at least one diffuser comprises a plurality of diffuser vanes, wherein at least one of the plurality of diffuser vanes comprising a camber line defined by a function comprising an inflection point.
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