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dc.contributor.authorKrueger, Patrick
dc.contributor.authorGottschalk, Hanno
dc.contributor.authorWerdelmann, Bastian
dc.contributor.authorKrebs, Werner
dc.date.accessioned2025-04-21T09:57:43Z
dc.date.available2025-04-21T09:57:43Z
dc.date.copyright9/13/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0742-4795
dc.identifier.othergtp_147_01_011007.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4305200
dc.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.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleGenerative Design of a Gas Turbine Combustor Using Invertible Neural Networks
dc.typeJournal Paper
dc.journal.volume147
dc.journal.issue1
dc.journal.titleJournal of Engineering for Gas Turbines and Power
dc.identifier.doi10.1115/1.4066294
dc.journal.fristpage11007-1
dc.journal.lastpage11007-13
dc.page13
dc.treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 001
dc.contenttypeFulltext


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