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This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
Article
Single Platform Integration Environment for Turbine Rotor Design and Analysis
Author(s)
Francois Lagloire, Yannick Ouellet, Francois Garnier and Hany Moustapha
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DOI:10.17265/1934-8975/2014.09.010
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ABSTRACT
The present article covers briefly state of the art software interoperability technical solutions and the development of the first module of a new single platform D & A (design & analysis) tool for simulation and prediction of stress and burst behavior of turbine rotating disc a preliminary design stage. This platform singularity requires integration of multiple CAD (computer assisted design) & FEA (finite element analysis) tools processing in batch mode and driven from a SPIE (single platform integration environment). This first module is also to demonstrate, for an axial turbine disc hub axi-symmetric component, feasibility and usefulness of such a platform at preliminary design stage. Expected benefits of the D & A single platform are to improve output accuracy, reduce cycle time, improve process quality and improve resource productivity.
KEYWORDS
Aero-engines, gas turbines, preliminary design, turbines, optimisation
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