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New Diagram and Equation for Thermodynamic Calculations for Gas Turbines FREE

[+] Author Affiliations
B. Herrmann

Lahmeyer International GmbH, Frankfurt/Main, West Germany

Paper No. 84-GT-275, pp. V005T16A013; 6 pages
doi:10.1115/84-GT-275
From:
  • ASME 1984 International Gas Turbine Conference and Exhibit
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; Process Industries; Technology Resources
  • Amsterdam, The Netherlands, June 4–7, 1984
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7950-4
  • Copyright © 1984 by ASME

abstract

On basis of ISO-Standard 2314, the German Standard Organisation (DIN) has prepared the German Standard DIN 4341, which deals with acceptance tests for gas turbines. Sample calculations have been included.

In connection with the development of the sample calculations a new diagram for thermodynamic properties of air and products of combustion was developed on basis of

-humid air as per ISO standard 2314

-standard gaseous fuel

-standard liquid fuel

This diagram allows exact calculation of performance data.

Further, a simplified but relatively acurate formula is presented for calculating the turbine inlet temperature on basis of

-compressor pressure ratio

-exhaust gas temperature

-thermal efficiency

Development and limitation of this formula is presented.

Copyright © 1984 by ASME
Topics: Gas turbines
This article is only available in the PDF format.

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