author_facet Sarnecki, Jarosław
Białecki, Tomasz
Gawron, Bartosz
Głąb, Jadwiga
Kamiński, Jarosław
Kulczycki, Andrzej
Romanyk, Katarzyna
Sarnecki, Jarosław
Białecki, Tomasz
Gawron, Bartosz
Głąb, Jadwiga
Kamiński, Jarosław
Kulczycki, Andrzej
Romanyk, Katarzyna
author Sarnecki, Jarosław
Białecki, Tomasz
Gawron, Bartosz
Głąb, Jadwiga
Kamiński, Jarosław
Kulczycki, Andrzej
Romanyk, Katarzyna
spellingShingle Sarnecki, Jarosław
Białecki, Tomasz
Gawron, Bartosz
Głąb, Jadwiga
Kamiński, Jarosław
Kulczycki, Andrzej
Romanyk, Katarzyna
Polish Maritime Research
Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
Mechanical Engineering
Ocean Engineering
author_sort sarnecki, jarosław
spelling Sarnecki, Jarosław Białecki, Tomasz Gawron, Bartosz Głąb, Jadwiga Kamiński, Jarosław Kulczycki, Andrzej Romanyk, Katarzyna 2083-7429 Walter de Gruyter GmbH Mechanical Engineering Ocean Engineering http://dx.doi.org/10.2478/pomr-2019-0008 <jats:title>Abstract</jats:title> <jats:p>This article concerns the issue of thermal degradation process of fuels, important from the perspective of the operation of turbine engines, especially in the context of new fuels/bio-fuels and their implementation. The studies of the kerosene-based jet fuel (Jet A-1) and its blends with synthetic components manufactured according to HEFA and ATJ technology, were presented. Both technologies are currently approved by ASTM D7566 to produce components to be added to turbine fuels. Test rig investigations were carried out according to specific methodology which reflects the phenomena taking place in fuel systems of turbine engines. The mechanism of thermal degradation process was assessed on the basis of test results for selected properties, IR spectroscopy and calculation of activation energy. The results show that with the increase of the applied temperature there is an increment of the content of solid contaminants, water and acid for all tested fuels. Thermal degradation process is different for conventional jet fuel when compared to blends, but also semi-synthetic fuels distinguished by different thermal stability depending on a given manufacturing technology.</jats:p> Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications Polish Maritime Research
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title Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_unstemmed Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_full Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_fullStr Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_full_unstemmed Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_short Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_sort thermal degradation process of semi-synthetic fuels for gas turbine engines in non-aeronautical applications
topic Mechanical Engineering
Ocean Engineering
url http://dx.doi.org/10.2478/pomr-2019-0008
publishDate 2019
physical 65-71
description <jats:title>Abstract</jats:title> <jats:p>This article concerns the issue of thermal degradation process of fuels, important from the perspective of the operation of turbine engines, especially in the context of new fuels/bio-fuels and their implementation. The studies of the kerosene-based jet fuel (Jet A-1) and its blends with synthetic components manufactured according to HEFA and ATJ technology, were presented. Both technologies are currently approved by ASTM D7566 to produce components to be added to turbine fuels. Test rig investigations were carried out according to specific methodology which reflects the phenomena taking place in fuel systems of turbine engines. The mechanism of thermal degradation process was assessed on the basis of test results for selected properties, IR spectroscopy and calculation of activation energy. The results show that with the increase of the applied temperature there is an increment of the content of solid contaminants, water and acid for all tested fuels. Thermal degradation process is different for conventional jet fuel when compared to blends, but also semi-synthetic fuels distinguished by different thermal stability depending on a given manufacturing technology.</jats:p>
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author Sarnecki, Jarosław, Białecki, Tomasz, Gawron, Bartosz, Głąb, Jadwiga, Kamiński, Jarosław, Kulczycki, Andrzej, Romanyk, Katarzyna
author_facet Sarnecki, Jarosław, Białecki, Tomasz, Gawron, Bartosz, Głąb, Jadwiga, Kamiński, Jarosław, Kulczycki, Andrzej, Romanyk, Katarzyna, Sarnecki, Jarosław, Białecki, Tomasz, Gawron, Bartosz, Głąb, Jadwiga, Kamiński, Jarosław, Kulczycki, Andrzej, Romanyk, Katarzyna
author_sort sarnecki, jarosław
container_issue 1
container_start_page 65
container_title Polish Maritime Research
container_volume 26
description <jats:title>Abstract</jats:title> <jats:p>This article concerns the issue of thermal degradation process of fuels, important from the perspective of the operation of turbine engines, especially in the context of new fuels/bio-fuels and their implementation. The studies of the kerosene-based jet fuel (Jet A-1) and its blends with synthetic components manufactured according to HEFA and ATJ technology, were presented. Both technologies are currently approved by ASTM D7566 to produce components to be added to turbine fuels. Test rig investigations were carried out according to specific methodology which reflects the phenomena taking place in fuel systems of turbine engines. The mechanism of thermal degradation process was assessed on the basis of test results for selected properties, IR spectroscopy and calculation of activation energy. The results show that with the increase of the applied temperature there is an increment of the content of solid contaminants, water and acid for all tested fuels. Thermal degradation process is different for conventional jet fuel when compared to blends, but also semi-synthetic fuels distinguished by different thermal stability depending on a given manufacturing technology.</jats:p>
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spelling Sarnecki, Jarosław Białecki, Tomasz Gawron, Bartosz Głąb, Jadwiga Kamiński, Jarosław Kulczycki, Andrzej Romanyk, Katarzyna 2083-7429 Walter de Gruyter GmbH Mechanical Engineering Ocean Engineering http://dx.doi.org/10.2478/pomr-2019-0008 <jats:title>Abstract</jats:title> <jats:p>This article concerns the issue of thermal degradation process of fuels, important from the perspective of the operation of turbine engines, especially in the context of new fuels/bio-fuels and their implementation. The studies of the kerosene-based jet fuel (Jet A-1) and its blends with synthetic components manufactured according to HEFA and ATJ technology, were presented. Both technologies are currently approved by ASTM D7566 to produce components to be added to turbine fuels. Test rig investigations were carried out according to specific methodology which reflects the phenomena taking place in fuel systems of turbine engines. The mechanism of thermal degradation process was assessed on the basis of test results for selected properties, IR spectroscopy and calculation of activation energy. The results show that with the increase of the applied temperature there is an increment of the content of solid contaminants, water and acid for all tested fuels. Thermal degradation process is different for conventional jet fuel when compared to blends, but also semi-synthetic fuels distinguished by different thermal stability depending on a given manufacturing technology.</jats:p> Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications Polish Maritime Research
spellingShingle Sarnecki, Jarosław, Białecki, Tomasz, Gawron, Bartosz, Głąb, Jadwiga, Kamiński, Jarosław, Kulczycki, Andrzej, Romanyk, Katarzyna, Polish Maritime Research, Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications, Mechanical Engineering, Ocean Engineering
title Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_full Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_fullStr Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_full_unstemmed Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_short Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
title_sort thermal degradation process of semi-synthetic fuels for gas turbine engines in non-aeronautical applications
title_unstemmed Thermal Degradation Process of Semi-Synthetic Fuels for Gas Turbine Engines in Non-Aeronautical Applications
topic Mechanical Engineering, Ocean Engineering
url http://dx.doi.org/10.2478/pomr-2019-0008