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Low-Emission Operation of Aeroderivative Gas-Turbine Combustor over a Wide Range of Ambient Conditions

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Power Technology and Engineering Aims and scope

The capabilities of controlling a low-emission combustor (LEC) over a wide range of ambient conditions are analyzed. The LES is intended for a GTU-16P gas turbine that is a derivative of the PS-90A aircraft engine by the UEC Aviadvigatel company. The LEC is of premix swirl stabilized type based on GTE-110 prototype. Its burner consists of pilot and main burners. The main burner has two fuel supply channels that allow controlling the quality of the air-fuel mixture. The low-emission operation range of the LEC can be extended to 70% load at negative ambient temperatures by bleeding air to the compressor inlet.

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References

  1. A. D. Nugumanov, A. M. Sipatov, and V. A. Nazukin, “Using the international experience of controlling gas-turbine engines (GTE) with low-emission combustor (LEC) based on output power and in ambient temperature range in creating an LEC for ODK-Aviadvigatel GTE,” Vestn. PGIPU Aérokosm. Tekhn., No. 50, 139 – 147 (2017).

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Authors and Affiliations

  1. JSC “All-Russia Thermal Engineering Institute”, Moscow, Russia

    L. A. Bulysova, A. G. Tumanovskii, M. N. Gutnik & V. D. Vasil’ev

  2. UEC Aviadvigatel, Perm, Russia

    A. M. Sipatov & A. D. Nugumanov

Authors
  1. L. A. Bulysova
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  2. A. G. Tumanovskii
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  3. M. N. Gutnik
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  4. V. D. Vasil’ev
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  5. A. M. Sipatov
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  6. A. D. Nugumanov
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Corresponding author

Correspondence to L. A. Bulysova.

Additional information

Translated from Élektricheskie Stantsii, No. 12, December 2019, pp. 20 – 22.

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Bulysova, L.A., Tumanovskii, A.G., Gutnik, M.N. et al. Low-Emission Operation of Aeroderivative Gas-Turbine Combustor over a Wide Range of Ambient Conditions. Power Technol Eng 54, 93–95 (2020). https://doi.org/10.1007/s10749-020-01173-3

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  • DOI: https://doi.org/10.1007/s10749-020-01173-3

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