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contributor authorKrueger, Patrick
contributor authorGottschalk, Hanno
contributor authorWerdelmann, Bastian
contributor authorKrebs, Werner
date accessioned2025-04-21T09:57:43Z
date available2025-04-21T09:57:43Z
date copyright9/13/2024 12:00:00 AM
date issued2024
identifier issn0742-4795
identifier othergtp_147_01_011007.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4305200
description abstractThe need to burn 100% H2 in high efficient gas turbines featuring low NOx combustion in premix mode requires the complete redesign of the combustion system to ensure stable operation without any flashback. Since all engine frames featuring a power range from 4 MW up to 600 MW are affected, a huge design effort is expected. To reduce this effort, especially to transfer knowledge between the different engine classes, generative design methods using latest AI technology will provide promising potential. In this work, this challenge is approached utilizing the current advances in generative artificial intelligence. We train an invertible neural network (INN) on an expandable database of geometrically parameterized combustor designs with simulated performance labels. Utilizing the INN in its inverse direction, multiple design proposals are generated, which fulfill specified performance labels.
publisherThe American Society of Mechanical Engineers (ASME)
titleGenerative Design of a Gas Turbine Combustor Using Invertible Neural Networks
typeJournal Paper
journal volume147
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4066294
journal fristpage11007-1
journal lastpage11007-13
page13
treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 001
contenttypeFulltext


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