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A Configuration to Improve the Aerodynamics and Scope of Can-Annular Combustors FREE

[+] Author Affiliations
R. C. Adkins, D. Binks

Cranfield Institute of Technology, Cranfield, Bedfordshire, England

Paper No. 83-GT-37, pp. V001T01A017; 7 pages
doi:10.1115/83-GT-37
From:
  • ASME 1983 International Gas Turbine Conference and Exhibit
  • Volume 1: Turbomachinery
  • Phoenix, Arizona, USA, March 27–31, 1983
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7951-1
  • Copyright © 1983 by ASME

abstract

Aerodynamic tests on a novel concept of pre-combustor diffuser, particularly suited to can-annular configurations, are described. These tests show that the new arrangement avoids the unstable flow separations and some of the parasitic pressure losses which can be experienced in more conventional arrangements.

With the benefit of improved flow conditions, it is argued that the can-annular combustor arrangement has many advantages over other configurations, particularly for large engines, and where exhaust gas pollutants must be kept to a minimum.

Copyright © 1983 by ASME
This article is only available in the PDF format.

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