40750 2017 eng 80 81 conferenceobject SpbPU Publisher St. Petersburg, Russia 0 -- -- -- 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. Proceedings Creep 2017 978-5-7422-5799-8 Creep 2017 St. Petersburg, Russia 19.07.2017 21.07.2017 Christian Rockenhäuser Sina Schriever Birgit Skrotzki eng uncontrolled Creep eng uncontrolled Microstructure eng uncontrolled Coarsening eng uncontrolled TEM Ingenieurwissenschaften und zugeordnete Tätigkeiten Datei im Netzwerk der BAM verfügbar ("Closed Access") Graue Literatur