π€ AI Summary
This work proposes an implicit generative framework based on DeepSDF to address the limitations of conventional turbine blade generation methods, which often lack performance awareness, manufacturability guarantees, and geometric continuity. By leveraging signed distance functions (SDFs), the approach achieves high-fidelity geometric reconstruction and constructs an interpretable, near-Gaussian latent space aligned with key aerodynamic and structural parameters, enabling both unconditional synthesis and performance-driven conditional generation. A compact neural network maps engineering performance metrics end-to-end to latent codes, facilitating efficient geometry generation through interpolation and Gaussian sampling. Experimental results demonstrate that the reconstructed surfaces exhibit distance errors within 1% of the bladeβs maximum dimension, achieving high fidelity while maintaining strong generalization to unseen designs.
π Abstract
Generative AI has emerged as a transformative paradigm in engineering design, enabling automated synthesis and reconstruction of complex 3D geometries while preserving feasibility and performance relevance. This paper introduces a domain-specific implicit generative framework for turbine blade geometry using DeepSDF, addressing critical gaps in performance-aware modeling and manufacturable design generation. The proposed method leverages a continuous signed distance function (SDF) representation to reconstruct and generate smooth, watertight geometries with quantified accuracy. It establishes an interpretable, near-Gaussian latent space that aligns with blade-relevant parameters, such as taper and chord ratios, enabling controlled exploration and unconditional synthesis through interpolation and Gaussian sampling. In addition, a compact neural network maps engineering descriptors, such as maximum directional strains, to latent codes, facilitating the generation of performance-informed geometry. The framework achieves high reconstruction fidelity, with surface distance errors concentrated within $1\%$ of the maximum blade dimension, and demonstrates robust generalization to unseen designs. By integrating constraints, objectives, and performance metrics, this approach advances beyond traditional 2D-guided or unconstrained 3D pipelines, offering a practical and interpretable solution for data-driven turbine blade modeling and concept generation.