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

Bulysova, L. A. / Tumanovskii, A. G. / Gutnik, M. N. / Vasil’ev, V. D. / Sipatov, A. M. / Nugumanov, A. D.

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

Bulysova, L. A. / Tumanovskii, A. G. / Gutnik, M. N. / Vasil’ev, V. D. / Sipatov, A. M. / Nugumanov, A. D.

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.

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

Bulysova, L. A. / Tumanovskii, A. G. / Gutnik, M. N. / Vasil’ev, V. D. / Sipatov, A. M. / Nugumanov, A. D.

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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Title:

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

Contributors:

Bulysova, L. A. (author) / Tumanovskii, A. G. (author) / Gutnik, M. N. (author) / Vasil’ev, V. D. (author) / Sipatov, A. M. (author) / Nugumanov, A. D. (author)

Published in:

Power Technology and Engineering ; 54

Publication date:

2020

ISSN:

DOI:

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

Type of media:

Article (Journal)

Type of material:

Electronic Resource

Language:

English

Keywords:

gas turbine , air-fuel mixture , NO , low-emission combustor , combustion stability , air bleeding

Classification:

BKL: 56.30 Wasserbau / 56.30$jWasserbau

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