Design for sustainability requires decision-makers to simultaneously consider the economic, ecological, and social consequences of their products and production processes for a broad range of stakeholders. While some choices may mutually benefit the three sustainability categories, there are often tradeoffs where improving one objective comes at a cost to another. Previous studies have shown that geometric tolerance decisions can affect all three sustainability criteria and create tradeoffs, particularly when they are made in conjunction with other design decisions. This paper presents a framework for analyzing product design decisions through a multi-objective optimization approach to sustainable design, tailored to the application of an aircraft engine turbine component. Models are constructed for production and maintenance costs, ecological impacts from manufacturing and use, and social impacts from neighborhood noise and delays caused by reliability-based maintenance events. Using advanced computational simulation and optimization, tradeoffs are shown and sustainable decision-making strategies are discussed.
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ASME 2013 International Mechanical Engineering Congress and Exposition
November 15–21, 2013
San Diego, California, USA
Conference Sponsors:
- ASME
ISBN:
978-0-7918-5641-3
PROCEEDINGS PAPER
Sustainability-Driven Tolerancing and Design Optimization of an Aircraft Engine Component
Steven Hoffenson,
Steven Hoffenson
Chalmers University of Technology, Gothenburg, Sweden
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Anders Forslund,
Anders Forslund
Chalmers University of Technology, Gothenburg, Sweden
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Rikard Söderberg
Rikard Söderberg
Chalmers University of Technology, Gothenburg, Sweden
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Steven Hoffenson
Chalmers University of Technology, Gothenburg, Sweden
Anders Forslund
Chalmers University of Technology, Gothenburg, Sweden
Rikard Söderberg
Chalmers University of Technology, Gothenburg, Sweden
Paper No:
IMECE2013-63520, V012T13A056; 9 pages
Published Online:
April 2, 2014
Citation
Hoffenson, S, Forslund, A, & Söderberg, R. "Sustainability-Driven Tolerancing and Design Optimization of an Aircraft Engine Component." Proceedings of the ASME 2013 International Mechanical Engineering Congress and Exposition. Volume 12: Systems and Design. San Diego, California, USA. November 15–21, 2013. V012T13A056. ASME. https://doi.org/10.1115/IMECE2013-63520
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