Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine

The problem of reducing the emission of unburned hydrocarbons and carbon monoxide that affect the value of fuel combustion efficiency in the afterburner combustion chamber of a gas turbine engine is considered. An analysis of the causes of hydrocarbon and carbon monoxide formation were carried out a...

Full description

Saved in:
Bibliographic Details
Main Authors: A. V. Zhuk, T. V. Grasko, A. S. Kolesnikov, V. V. Raznoschikov
Format: Article
Language:English
Published: Samara National Research University 2025-06-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/28700/11331
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1850119952901603328
author A. V. Zhuk
T. V. Grasko
A. S. Kolesnikov
V. V. Raznoschikov
author_facet A. V. Zhuk
T. V. Grasko
A. S. Kolesnikov
V. V. Raznoschikov
author_sort A. V. Zhuk
collection DOAJ
description The problem of reducing the emission of unburned hydrocarbons and carbon monoxide that affect the value of fuel combustion efficiency in the afterburner combustion chamber of a gas turbine engine is considered. An analysis of the causes of hydrocarbon and carbon monoxide formation were carried out and ways to reduce them were identified. The chemical and physical process of the combustion of hydrocarbon fuel with the addition of gaseous hydrogen to its composition is considered with an assessment of the emission of unburned hydrocarbons and carbon monoxide. A method for calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine engine with a dual-fuel power supply system is proposed. It is shown that the application of the developed technique makes it possible to estimate the value of the combustion efficiency and maintain its set value by correcting the percentage ratio of hydrogen to kerosene. The technique was tested during an experimental study of the hydrogen-air mixture combustion in the model compartment of the afterburner combustion chamber of a commercial gas turbine engine.
format Article
id doaj-art-e7e73978f6084f568cfe8d29d5f52619
institution OA Journals
issn 2542-0453
2541-7533
language English
publishDate 2025-06-01
publisher Samara National Research University
record_format Article
series Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
spelling doaj-art-e7e73978f6084f568cfe8d29d5f526192025-08-20T02:35:31ZengSamara National Research UniversityВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение2542-04532541-75332025-06-0124213615010.18287/2541-7533-2025-24-2-136-1508969Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engineA. V. Zhuk0T. V. Grasko1A. S. Kolesnikov2V. V. Raznoschikov3Military Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. GagarinMilitary Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. GagarinMilitary Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. GagarinCentral Institute of Aviation MotorsThe problem of reducing the emission of unburned hydrocarbons and carbon monoxide that affect the value of fuel combustion efficiency in the afterburner combustion chamber of a gas turbine engine is considered. An analysis of the causes of hydrocarbon and carbon monoxide formation were carried out and ways to reduce them were identified. The chemical and physical process of the combustion of hydrocarbon fuel with the addition of gaseous hydrogen to its composition is considered with an assessment of the emission of unburned hydrocarbons and carbon monoxide. A method for calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine engine with a dual-fuel power supply system is proposed. It is shown that the application of the developed technique makes it possible to estimate the value of the combustion efficiency and maintain its set value by correcting the percentage ratio of hydrogen to kerosene. The technique was tested during an experimental study of the hydrogen-air mixture combustion in the model compartment of the afterburner combustion chamber of a commercial gas turbine engine.https://journals.ssau.ru/vestnik/article/viewFile/28700/11331aviation fuelspecific fuel consumptionafterburnerhydrogen gasvaporized keroseneemission indices
spellingShingle A. V. Zhuk
T. V. Grasko
A. S. Kolesnikov
V. V. Raznoschikov
Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
aviation fuel
specific fuel consumption
afterburner
hydrogen gas
vaporized kerosene
emission indices
title Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine
title_full Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine
title_fullStr Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine
title_full_unstemmed Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine
title_short Method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine
title_sort method of calculating the fuel combustion efficiency in the afterburner combustion chamber of a gas turbine dual fuel engine
topic aviation fuel
specific fuel consumption
afterburner
hydrogen gas
vaporized kerosene
emission indices
url https://journals.ssau.ru/vestnik/article/viewFile/28700/11331
work_keys_str_mv AT avzhuk methodofcalculatingthefuelcombustionefficiencyintheafterburnercombustionchamberofagasturbinedualfuelengine
AT tvgrasko methodofcalculatingthefuelcombustionefficiencyintheafterburnercombustionchamberofagasturbinedualfuelengine
AT askolesnikov methodofcalculatingthefuelcombustionefficiencyintheafterburnercombustionchamberofagasturbinedualfuelengine
AT vvraznoschikov methodofcalculatingthefuelcombustionefficiencyintheafterburnercombustionchamberofagasturbinedualfuelengine