TY - CONF A1 - Rockenhäuser, Christian A1 - Schriever, Sina A1 - Skrotzki, Birgit A2 - Panfilov, Peter A2 - Kodzhaspirov, Georgii T1 - Microstructural evolution during creep of Al-alloy 2618A T2 - Proceedings Creep 2017 N2 - The aluminum alloy 2618A is an Al-Cu-Mg alloy with additions of Fe and Ni, which was designed for long-term operation at elevated temperature in transportation and aerospace industries. Typical applications include aircraft parts and structures (sheet material) or engine components such as turbo charger centrifugal compressor wheels (forged material). Such components are subjected to prolonged aging during service, (e.g. 50 000 h) at temperatures which are close to their age hardening temperature (ca. 190 °C). The microstructural evolution during creep exposure is studied. PB - SpbPU Publisher CY - St. Petersburg, Russia T2 - Creep 2017 CY - St. Petersburg, Russia DA - 19.07.2017 KW - Creep KW - Microstructure KW - Coarsening KW - TEM PY - 2017 UR - https://opus4.kobv.de/opus4-bam/frontdoor/index/index/docId/40750 AN - OPUS4-40750 SN - 978-5-7422-5799-8 SP - 80 EP - 81 AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany