Constructing a gas turbine combustor reactor model with formalized identification of zones limiting carbon monoxide oxidation

Authors

  • Kutlumukhamedov Artur Ramilevich ПАО "ОДК-УМПО"
  • Skiba Dmitriy Vladimirovich ООО «НПФ «Теплофизика»
  • Bakirov Fedor Gayfullovich Ufa University of Science and Technology

Keywords:

combustion chamber, pollutant emissions, carbon monoxide, three-dimensional modeling, formalized reactor model, modeling criterion, low-temperature zone, flame zone

Abstract

This paper describes the process for constructing a reactor model of a gas turbine engine (GTE) combustion chamber, using 3D modeling results, with a formalized identification of zones limiting carbon monoxide oxidation. The reactor model and calculation results for the combustion chamber of the GTE-10/953 industrial gas turbine are presented, with configurations before and after conversion from aviation kerosene to natural gas. The difference between the calculated and experimental values for carbon monoxide (CO) emissions averaged 13%. doi: 10.54708/19926502_2026_30311335

Author Biographies

Kutlumukhamedov Artur Ramilevich, ПАО "ОДК-УМПО"

Cand. Tech. Sci., Leading design engineer, Design Bureau “Motor”

Skiba Dmitriy Vladimirovich, ООО «НПФ «Теплофизика»

a, Cand. Tech. Sci., Deputy Scientific Director of LLC NPF “Teplofizika”, Assoc. Prof. of the Dept. of Aviation Thermal Engineering and Heat Power Engineering

Bakirov Fedor Gayfullovich, Ufa University of Science and Technology

Doct. Tech. Sci. in thermal, electrical rocket engines and power plants of aircraft, Prof. of the Dept. of Aviation Thermal Engineering and Heat Power Engineering

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Published

2026-07-10

Issue

Vol. 30 No. 3(113) (2026)

Section

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