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Wave Augmented Diffusers for Centrifugal CompressorsA conceptual device is introduced which would utilize unsteady wave motion to slow and turn flows in the diffuser section of a centrifugal compressor. The envisioned device would substantially reduce the size of conventional centrifugal diffusers by eliminating the relatively large ninety degree bend needed to turn the flow from the radial/tangential to the axial direction. The bend would be replaced by a wall and the flow would instead exit through a series of rotating ports located on a disk, adjacent to the diffuser hub, and fixed to the impeller shaft. The ports would generate both expansion and compression waves which would rapidly transition from the hub/shroud (axial) direction to the radial/tangential direction. The waves would in turn induce radial/tangential and axial flow. This paper presents a detailed description of the device. Simplified cycle analysis and performance results are presented which were obtained using a time accurate, quasi-one-dimensional CFD code with models for turning, port flow conditions, and losses due to wall shear stress. The results indicate that a periodic wave system can be established which yields diffuser performance comparable to a conventional diffuser. Discussion concerning feasibility, accuracy, and integration follow.
Document ID
19980211303
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Paxson, Daniel E.
(NASA Lewis Research Center Cleveland, OH United States)
Skoch, Gary J.
(Army Research Lab. Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1998
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:208480
AIAA Paper 98-3401
NASA/TM-1998-208480
E-11253
Report Number: NAS 1.15:208480
Report Number: AIAA Paper 98-3401
Report Number: NASA/TM-1998-208480
Report Number: E-11253
Meeting Information
Meeting: Propulsion
Location: Cleveland, OH
Country: United States
Start Date: July 12, 1998
End Date: July 15, 1998
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
PROJECT: RTOP 523-26-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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