CAE-Driven Design Methodology for Semi- Autonomous Product Development

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1 Chart 1 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > CAE-Driven Design Methodology for Semi- Autonomous Product Development Designing the next generation light weight vehicle structures Dr.-Ing. Sivakumara Krishnamoorthy Dipl.-Ing. Matthias Konzelmann Sameer Chaudhari B.E. Dipl.-Ing. Gundolf Kopp Prof. Dr.-Ing. Horst E. Friedrich

2 Chart 2 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > DLR Overview German national research center for aeronautics and space Development of environmentally-friendly technologies Promote mobility, communication and security employees are working at 32 research institutes and facilities in 9 locations and 7 branch offices. SPACE AERONAUTICS TRANSPORTATION ENERGY

3 Chart 3 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Motivation Global Challenges shortage of ressources climate change Challenges in Mobility reduce fuel consumption reduce emissions adapt concepts for new mobility Challenges for Vehicle Concepts short development time increase economic efficiency CAE-based design methodology for BIW-concepts

4 Chart 4 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Objective CAE-based design methodology Lightweight design Comfort Economy Driving characteristics Safety

5 Chart 5 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Approach Light Weight Structure Topology Optimization Result Design-Space-Model

6 Chart 6 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Optimization Model Units and loads are point masses Static loadcases: Torsion Bending Static loads representing dynamic conditions: Front crash Rear crash Side crash Crash equivalent static loads

7 Chart 7 > CAE-driven design methodology > Matthias Konzelmann > Topology Optimization Result

8 Chart 8 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Approach Light Weight Structure Topology Optimization Result Design-Space-Model

9 Chart 9 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Interpretation of Structural Requirements

10 Chart 10 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Interpretation of Structural Requirements Bending Axial load Torsion

11 Chart 11 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Identifying Shear Locations Optimization algorithm disadvantages shear planes Identification necessary Plane structures are easy to manufacture F F End result Intermediate result

12 Chart 12 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Techno-Economic Criteria Material Space-Frame Monocoque Hybrid Shell Branding/ Image Quantity Cost effectiveness

13 Performance LC 1 LC 2 LC 3 LC x LC 1 LC 2 LC 3 LC x Chart 13 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Interpreting the Results One purpose per loadcase (LC) and member Topology Optimization results contain complex equilibrium No loadcase disregarded Good performance for each loadcase No focus on particular loadcases Initial calculation Final calculation

14 Chart 14 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Example: Side-Rail Very high height to width ratio I-shape already in result Shear structure Width Height

15 Chart 15 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Example: Roof-Structure No information in cross-section Further interpretation: Contour Signed VonMises Bending detected? In this case no Bending

16 Chart 17 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Example: Roof-Structure Cross-section shell structure

17 Chart 18 > 2013 European Altair Technology Conference Torino > Matthias Konzelmann > Example: Roof-Structure Roof structure, reinforced with FRP +/-45

18 Chart 19 > CAE-driven design methodology > Matthias Konzelmann > Decision Making in Design Process

19 Thank you for your attention

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