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The Project of a GTE-65 Power-Generating Gas-Turbine Unit

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Abstract

The thermal scheme and thermodynamic parameters of the GTE-65 unit are validated. The general design makeup of the unit and its main constituent parts, including the compressor, combustion chamber, and turbine are described.

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References

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  2. A. S. Lebedev and N. O. Simin, Substantiating the Choice of Parameters for the Thermal Scheme of a GTE-65 Medium-Capacity Gas-Turbine Unit and the Characteristics of Its Main Parts, Tyazh. Mashinostr., No. 7, 2–7 (2007).

  3. A. S. Lebedev, I. S. Varlamov, and M. V. Roslyakov, The GTE-65 Medium-Capacity Power-Generating Gas Turbine Unit: Design and Manufacture, Elektr. Stn., No. 1, 19–22 (2007).

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  7. S. Lebedev and N. O. Simin, A Strategy of Designing the Service Life of the New GTE-180 Power-Generating Gas-Turbine Unit, Teploenergetika, No. 11, 9–13 (2004) [Therm. Eng., No. 11 (2004).

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Authors and Affiliations

  1. Leningrad Metal Works (LMZ), OAO Silovye Mashiny, Sverdlovskaya nab. 18, St. Petersburg, 195009, Russia

    A. S. Lebedev & N. O. Simin

  2. Central Boiler-Turbine Institute Research and Production Association (NPO TsKTI), ul. Atamanskaya 3/6, St. Petersburg, 191167, Russia

    Yu. K. Petrenya & V. E. Mikhailov

Authors
  1. A. S. Lebedev
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  2. N. O. Simin
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  3. Yu. K. Petrenya
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  4. V. E. Mikhailov
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Lebedev, A.S., Simin, N.O., Petrenya, Y.K. et al. The Project of a GTE-65 Power-Generating Gas-Turbine Unit. Therm. Eng. 55, 54–61 (2008). https://doi.org/10.1134/S0040601508010126

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  • DOI: https://doi.org/10.1134/S0040601508010126

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