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AGILE™ Software

Multidisciplinary Optimization (MDO)

Automated Optimization Capabilities Powered by iSIGHT
in the AGILE™ Engineering Design System

Concepts NREC offers several options for automated optimization capabilities in the AGILE™ Engineering Design System® for turbomachinery. Two levels of stress and vibration capabilities can be added to STRESSPREP™ to allow optimization of impeller mechanical properties such as stress and vibration. An additional optimization level has been added to the combination of CCAD® and Pushbutton CFD® to allow optimization of CFD predicted fluid dynamic performance. When combined, these aero/hydraulic and mechanical optimization options allow true Multidisciplinary Optimization (MDO) capabilities in the AGILE™ Engineering Design System. These optimization packages are built upon iSIGHT technology from Engineous Software, Inc.

Optimize Impeller Shape
The new “S” optimization packages are optional add-ons to STRESSPREP that allow the designer to optimize an impeller shape using stress levels, displacements, temperatures, and vibration frequencies as design targets or constraints. Design variables that the optimizer can work with are any of the geometrical parameters that can be adjusted within the STRESSPREP user interface such as backface shape, bore shape, and blade fillets. In addition, if CCAD is part of the design system, the blade and flow path shapes controlled by CCAD can be optimized together with the impeller geometry controlled by STRESSPREP.

On the fluid dynamic side our existing iSIGHT EASy!™ Level 1 (E1) optional add-on to CCAD package is complimented with one additional level. The Level 2 capability requires both CCAD and Pushbutton CFD and allows optimization based on CFD predicted results such as overall efficiency and pressure rise.

True MDO System
When any of the “E” packages is combined with an “S” package, a true MDO system is created. The table on the reverse side summarizes all available options. The MDO packages offered by Concepts NREC represent the world’s first out-of-the-box MDO system for turbomachinery design. All of the complicated stitching together of programs and optimization algorithms has been seamlessly packaged by Concepts NREC and Engineous Software. However, creating an effective MDO system is not simply a matter of hooking together the appropriate codes in an optimization loop. To unleash the real power of MDO, an organization’s design rules and practices must be captured and translated into optimization goals and constraints. Concepts NREC has been working with customers in the area of optimization since 1998 and will be happy to assist any organization to create effective MDO procedures.

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Peak stress was reduced from 66 ksi to 58 ksi in Step One. Step Two shows additional improvement from 58 ksi to 42 ksi.

MDO Step One

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Before: Peak stress 66 ksi at blade root and bore.

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After Step One: Peak stress 58 ksi in bore, blades in great shape < 30 ksi.
MDO Step Two

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Before: Peak stress 58 ksi in bore, blades in great shape < 30 ksi.

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After Step Two: 42 ksi.

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Backface design comparing geometry before and after optimization.

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Turbocharger impeller geometry before and after optimization.

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