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...
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| Format: | Article |
| Language: | English |
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Samara National Research University
2025-06-01
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| Series: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
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| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/28700/11331 |
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| 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 |
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