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Development of Inlet for an Axial Compressor PUBLIC ACCESS

[+] Author Affiliations
R. C. Reisweber

Elliott Company, Jeannette, PA

Paper No. 68-GT-41, pp. V001T01A041; 11 pages
doi:10.1115/68-GT-41
From:
  • ASME 1968 Gas Turbine Conference and Products Show
  • ASME 1968 Gas Turbine Conference and Products Show
  • Washington, DC, USA, March 17–21, 1968
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7987-0
  • Copyright © 1968 by ASME

abstract

In development of an axial-flow boiler supercharger, a test program on the compressor inlet was carried out. Tests were run using a test compressor aerodynamically identical to the first three stages of the supercharger compressor. Prototype compressor inlet was compared to an axial inlet, and also to several modified inlets. While the prototype inlet showed considerably more distortion ahead of the inlet guide vanes than the axial inlet, the inlet guide vanes removed most of the distortion. As a result, overall performance of all inlet configurations was essentially the same.

Copyright © 1968 by ASME
Topics: Compressors
This article is only available in the PDF format.

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