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    Investigation of Ash Deposition Behavior From Biogenic Solid Fuel Under Gas Turbine Conditions With Film Cooling

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:006::page 718
    Author:
    Wunder, Luis
    ,
    Bernhardt, Daniel
    ,
    Beckmann, Michael
    DOI: 10.1115/1.4070348
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. In the current state of technology, gas turbines operate mainly with fossil fuels. In order to achieve a sustainable energy supply with gas turbines, alternative fuels have to be used. In the past, many attempts have been made to use alternative fuels, such as solid biogenic fuels. The main problem with the use of these fuels has been the fouling of the turbine stages during operation. To counteract this problem, the use of film cooling as a protective mechanism to reduce deposits is considered in this work. For this purpose, test blades with film cooling were created and exposed to an increased particle load in a test rig. Synthetically produced ash, which corresponds to the typical components of biogenic utilization, was used as test ash for the deposition tests. The deposits were analyzed by means of a visual inspection paired with a raster electron microscope–energy-dispersive X-ray spectroscopy (REM-EDX) examination. The deposition tests were additionally supported by computational fluid dynamics (CFD) simulations and compared with the particle Stokes number. Overall, film cooling appears to be a suitable means of reducing deposits on a turbine blade. However, the geometric design needs to be modified compared to the classical film cooling setup. In addition, low momentum flux ratios and a delay of the flow seem to be favorable for film cooling as a protective mechanism. The blade deflection angle also plays an important role in the implementation of the new design.
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      Investigation of Ash Deposition Behavior From Biogenic Solid Fuel Under Gas Turbine Conditions With Film Cooling

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    contributor authorWunder, Luis
    contributor authorBernhardt, Daniel
    contributor authorBeckmann, Michael
    date accessioned2026-08-23T07:11:48Z
    date available2026-08-23T07:11:48Z
    date copyright2026/06/01
    date issued2026
    identifier issn0889-504X
    identifier otherturbo-25-1215.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314751
    description abstractAbstract. In the current state of technology, gas turbines operate mainly with fossil fuels. In order to achieve a sustainable energy supply with gas turbines, alternative fuels have to be used. In the past, many attempts have been made to use alternative fuels, such as solid biogenic fuels. The main problem with the use of these fuels has been the fouling of the turbine stages during operation. To counteract this problem, the use of film cooling as a protective mechanism to reduce deposits is considered in this work. For this purpose, test blades with film cooling were created and exposed to an increased particle load in a test rig. Synthetically produced ash, which corresponds to the typical components of biogenic utilization, was used as test ash for the deposition tests. The deposits were analyzed by means of a visual inspection paired with a raster electron microscope–energy-dispersive X-ray spectroscopy (REM-EDX) examination. The deposition tests were additionally supported by computational fluid dynamics (CFD) simulations and compared with the particle Stokes number. Overall, film cooling appears to be a suitable means of reducing deposits on a turbine blade. However, the geometric design needs to be modified compared to the classical film cooling setup. In addition, low momentum flux ratios and a delay of the flow seem to be favorable for film cooling as a protective mechanism. The blade deflection angle also plays an important role in the implementation of the new design.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigation of Ash Deposition Behavior From Biogenic Solid Fuel Under Gas Turbine Conditions With Film Cooling
    typeJournal Paper
    journal volume148
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4070348
    journal fristpage718
    journal lastpage724
    page7
    treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:006
    contenttypeFulltext
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