Generative Design of a Gas Turbine Combustor Using Invertible Neural Networks

arXiv cs.AI / 4/28/2026

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Key Points

  • The paper addresses the challenge of redesigning gas turbine combustors to enable 100% hydrogen (H2) premix combustion while maintaining stability and preventing flashback, alongside low NOx emissions requirements.
  • It proposes using generative AI to reduce the otherwise large engineering effort needed across a wide power range (from 4 MW to 600 MW) and to transfer design knowledge between engine classes.
  • The authors train an Invertible Neural Network (INN) on a geometry-parameterized database of combustor designs, using simulated performance labels.
  • By running the INN in its inverse mode, the method generates multiple combustor design proposals that satisfy user-specified performance targets.

Abstract

The need to burn 100% H2 in high efficient gas turbines featuring low NOx combustion in premix mode require 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.