13th Computers in Engineering Conference 1993
DOI: 10.1115/cie1993-0045
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Knowledge-Based Parametric Modeling for Nozzles

Abstract: This paper describes a new, and unique, system for design and analysis of a family of parts with a specific focus on gas turbine nozzles. The system, built on the tenets of knowledge-based engineering (KBE) within an object-oriented framework, supports the notion of scalable products that can be resized through reparametrization. The KBE system for the parametric design of nozzles has been integrated with a Topology and Geometry Utility System (TAGUS) and geometry-based mesh generators (QUADTREE and EXTREME) t… Show more

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“…Reduction of the risk of a drop back to the conceptual phase [25] Capture and reuse the expert experience efficiently [27,31,33,37] Heighten the design efficiency and quality [27,37] Portable web-based development and runtime environments [28] Independence from proprietary CAD systems [28] Automatic caching and dependency tracking for scalable runtime performance of large models [28] Minimal source code volume [28] More efficient, clearer and easier model development and debugging [22,26,28,31,34,35,36] More information on the model (what, why, how) [30] E3S Web of Conferences 334, 05001 (2022) EFC21…”
Section: Benefits Referencementioning
confidence: 99%
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“…Reduction of the risk of a drop back to the conceptual phase [25] Capture and reuse the expert experience efficiently [27,31,33,37] Heighten the design efficiency and quality [27,37] Portable web-based development and runtime environments [28] Independence from proprietary CAD systems [28] Automatic caching and dependency tracking for scalable runtime performance of large models [28] Minimal source code volume [28] More efficient, clearer and easier model development and debugging [22,26,28,31,34,35,36] More information on the model (what, why, how) [30] E3S Web of Conferences 334, 05001 (2022) EFC21…”
Section: Benefits Referencementioning
confidence: 99%
“…Shorten learning curves for novice engineers [22,31] Shorten Design cycle time [22,34,35,36,37] Given the peculiar features of hydrogen combustion, existing gas turbines can be adapted for using hydrogen as a fuel integrating improved burners that are able to work at high temperature. Therefore, one of the major design challenge is related to re-configure existing gas turbines and to integrate new burners/combustor with them.…”
Section: Benefits Referencementioning
confidence: 99%