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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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