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Coupled Optimization of Compressor Blade Roots and Rotor Grooves for Industrial Gas-Turbines

  • Substituting an intuitive human design search by an automated design process for compressor blade roots and rotor grooves driven by numerical optimization. The design of industrial gas turbines is a highly complex task where the engineer typically run a lot of design cases intuitively and manually in order to find only acceptable design solution which is usually a time consuming procedure. Research project funded by Alstom, Switzerland. The research shows the benefit of applying optimization methods to an industrial design process.

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Metadaten
Author: Roman Schörner, Dieter BestleGND
URL:http://www.epsmso.gr/all_conf_index/index.html
ISBN:978-960-98941-9-7
Title of the source (English):5th IC-SCCE International Conference: From Scientific Computing to Computational Engineering
Document Type:Conference Proceeding
Language:English
Year of publication:2012
Tag:optimization, FE analysis, compressor blade root, rotor groove, gas turbine
Faculty/Chair:Fakultät 3 Maschinenbau, Elektro- und Energiesysteme / FG Technische Mechanik und Fahrzeugdynamik
Institution name at the time of publication:Fakultät für Maschinenbau, Elektrotechnik und Wirtschaftsingenieurwesen (eBTU) / LS Technische Mechanik und Fahrzeugdynamik
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