Abstract
Recent advances in the simulation of the quench, cold-work and machining processes for large aluminum forgings are opening the way for a new paradigm in the design, manufacture and sustainment of aircraft structures. The use of large forgings permits the unitization of smaller parts (brackets, fittings, lugs, etc.) with primary structural components like spars and bulkheads. This is being done in order to reduce part count, which in turn leads to significant reductions in manufacturing cost. Unitization can also translate into weight reduction / avoidance when comparing against built-up structure, but it raises a number of issues for structural durability and damage tolerance, notably reduced repair / replace capability and reduced crack arrest capability. The viability of the unitization concept is dependent not only on the availability of material systems that retain their mechanical properties in very thick sections, but also on the designer’s ability to retain durability and damage tolerance, and to understand and mitigate the effects of residual stresses.
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© 2015 TMS (The Minerals, Metals & Materials Society)
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Dutton, R., Kobryn, P., Ball, D., Castle, J., James, M., Yavari, P. (2015). From Integrated Computational Materials Engineering to Integrated Computational Structural Engineering. In: Poole, W., et al. Proceedings of the 3rd World Congress on Integrated Computational Materials Engineering (ICME 2015). Springer, Cham. https://doi.org/10.1007/978-3-319-48170-8_12
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DOI: https://doi.org/10.1007/978-3-319-48170-8_12
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-48612-3
Online ISBN: 978-3-319-48170-8
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