TY - JOUR A1 - Häusler, Ines A1 - Schwarze, C. A1 - Umer Bilal, M. A1 - Valencia Ramirez, D. A1 - Hetaba, W. A1 - Darvishi Kamachali, Reza A1 - Skrotzki, Birgit T1 - Precipitation of T1 and theta′ Phase in Al‐4Cu‐1Li‐0.25Mn During Age Hardening: Microstructural Investigation and Phase‐Field Simulation N2 - Experimental and phase field studies of age hardening response of a high purity Al‐4Cu‐1Li‐0.25Mn‐alloy (mass %) during isothermal aging are conducted. In the experiments, two hardening phases are identified: the tetragonal θ′ (Al₂Cu) phase and the hexagonal T1 (Al₂CuLi) phase. Both are plate shaped and of nm size. They are analyzed with respect to the development of their size, number density and volume fraction during aging by applying different analysis techniques in TEM in combination with quantitative microstructural analysis. 3D phase‐field simulations of formation and growth of θ′ phase are performed in which the full interfacial, chemical and elastic energy contributions are taken into account. 2D simulations of T1 phase are also investigated using multi‐component diffusion without elasticity. This is a first step toward a complex phase‐field study of T1 phase in the ternary alloy. The comparison between experimental and simulated data shows similar trends. The still unsaturated volume fraction indicates that the precipitates are in the growth stage and that the coarsening/ripening stage has not yet been reached. KW - Al‐Cu‐Li‐alloy KW - Precipitates KW - Age hardening KW - Volume fraction KW - Number density KW - Microstructure KW - Phase‐field modeling KW - Elasticity KW - Multi‐component diffusion KW - Growth kinetics PY - 2017 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-390473 SN - 1996-1944 VL - 10 IS - 2 SP - Article 117, 1 EP - 21 PB - MDPI CY - Basel, Schweiz AN - OPUS4-39047 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Rockenhäuser, Christian A1 - Rowolt, C. A1 - Milkereit, B. A1 - Darvishi Kamachali, Reza A1 - Kessler, O. A1 - Skrotzki, Birgit T1 - On the long-term aging of S-phase in aluminum alloy 2618A N2 - The aluminum alloy 2618A is applied for engine components such as radial compressor wheels which operate for long time at elevated temperatures. This results in coarsening of the hardening precipitates and degradation in mechanical properties during the long-term operation, which is not taken into account in the current lifetime prediction models due to the lack of quantitative microstructural and mechanical data. To address this issue, a quantitative investigation on the evolution of precipitates during long-term aging at 190 °C for up to 25,000 h was conducted. Detailed transmission electron microscopy (TEM) was combined with Brinell hardness measurements and thorough differential scanning calorimetry (DSC) experiments. The results showthat GPB zones and S-phase Al2CuMg grow up to < 1,000 h during which the GPB zones dissolve and S-phase precipitates form. For longer aging times, only S-phase precipitates coarsen, which can be well described using the Lifshitz–Slyozov Wagner theory of ripening. A thorough understanding of the underlying microstructural processes is a prerequisite to enable the integration of aging behavior into the established lifetime models for components manufactured from alloy 2618A. KW - Long-term aging KW - Transmission electron microscopy (TEM) KW - Differential scanning calorimetry (DSC) KW - Microstructure KW - S-phase KW - Ostwald ripening PY - 2021 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-519899 SN - 0022-2461 VL - 56 IS - 14 SP - 8704 EP - 8716 PB - Springer Nature AN - OPUS4-51989 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Rockenhäuser, Christian A1 - Skrotzki, Birgit T1 - Microstructure evolution in a 2618A aluminium alloy during ageing N2 - The aluminium alloy 2618A is an Al-Cu-Mg alloy which is part of the 2xxx series of age-hardenable alloys. These materials are designed for long-term Operation in transportation and aerospace industries. The desired properties, e.g. creep behavior, hardness, and damage tolerance, are controlled by the distribution of fine precipitates formed within the matrix. However, the strength of the material declines du ring exposition to elevated temperatures due to the overageing of the S-phase precipitates (AI2CuMg) and the conversion of the S-phase into the stable equilibrium S-phase. A quantitative model of the overageing process at application relevant temperatures would be desirable for accurate predictions of component lifetime made from the 2618A alloy. T2 - MC 2015 - Microscopy conference CY - Göttingen, Germany DA - 06.09.2015 KW - Aluminium alloys KW - Transmission electron microscopy KW - Microstructure KW - Coarsening PY - 2015 SP - MS4.P078, 150 EP - 151 AN - OPUS4-34304 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Rockenhäuser, Christian A1 - Schriever, Sina A1 - Skrotzki, Birgit ED - Panfilov, Peter ED - Kodzhaspirov, Georgii T1 - Microstructural evolution during creep of Al-alloy 2618A 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. T2 - Creep 2017 CY - St. Petersburg, Russia DA - 19.07.2017 KW - Creep KW - Microstructure KW - Coarsening KW - TEM PY - 2017 SN - 978-5-7422-5799-8 SP - 80 EP - 81 PB - SpbPU Publisher CY - St. Petersburg, Russia AN - OPUS4-40750 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Skrotzki, Birgit A1 - Rockenhäuser, Christian A1 - Schriever, Sina T1 - Microstructural Evolution during Creep of Al-Alloy 2618A 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 was investigated. T2 - Creep 2017 CY - St. Petersburg, Russia DA - 18.06.2017 KW - Creep KW - Microstructure KW - Coarsening KW - TEM PY - 2017 AN - OPUS4-40756 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Skrotzki, Birgit A1 - Koch, B. T1 - Microstructural characterization of the metastable Beta-titanium alloy TIMETAL LCB after fatigue loading N2 - In the present work, the titanium alloy Ti-6.8Mo-4.5Fe-1.5Al (Timetal LCB) was investigated with respect to the microstructural evolution during strain controlled fatigue loading. The alloy was developed to reduce the generally high material costs of β-alloys by substituting expensive beta stabilizers by using a standard Fe-Mo master alloy. One possible application seen in the automotive industry is the substitution os suspension structural parts currently made of steel, suc as suspension springs. These components require a high strength and fatigue resistance. T2 - International conference on electron nanoscopy & XXXII Annual meeting of EMSI CY - Hyderabad, India DA - 2011-07-06 KW - Titanium KW - Fatigue KW - Microstructure KW - Deformation mechanism PY - 2011 SP - 255 EP - 256 AN - OPUS4-24167 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Skrotzki, Birgit A1 - Avila, Luis A1 - Charmi, Amir A1 - Falkenberg, Rainer A1 - Rehmer, Birgit T1 - Mechanical Testing and Simulations on AM Ti6Al4V and 316L N2 - First experimental results are shown on mechanical properties of additively manufactured alloy Ti6Al4V. A modelling and simulation approach is presented to describe the anisotropic behavior of 316L at the macro-scale. T2 - Workshop on Additive Manufacturing: Process, materials, testing, simulation & implants CY - BAM, Berlin, Germany DA - 13.05.2019 KW - AM KW - Mechanical behavior KW - Microstructure KW - Anisotropy KW - Modeling KW - Simulation PY - 2019 AN - OPUS4-48072 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - von Hartrott, P. A1 - Metzger, M. A1 - Rockenhäuser, Christian A1 - Skrotzki, Birgit T1 - Lifetime assessment of aging materials N2 - Materials subjected to high-temperature service conditions will change their microstructure with time. Associated with this aging process is a change of mechanical properties as well as a change of damage mechanisms. Within the scope of the FVV project Aging and Lifetime, Fraunhofer IWM in Freiburg and BAM in Berlin (both Germany) experimentally characterized the widespread high-temperature aluminum alloy EN AW-2618A in different overaging states. Based on the experimental findings, models for numerical lifetime assessment with the finite-element method were implemented. KW - Aluminum alloy KW - Aging KW - Microstructure KW - Lifetime prediction KW - Damage PY - 2018 U6 - https://doi.org/10.1007/s38313-018-0084-7 SN - 2192-9114 VL - 79 IS - 10 SP - 64 EP - 68 PB - Springer AN - OPUS4-46065 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Rockenhäuser, Christian A1 - Skrotzki, Birgit A1 - Karlin, J. A1 - Von Hartrott, P. T1 - Lebensdauerberechnung von Aluminium-Radialverdichterrädern unter Berücksichtigung der Werkstoffalterung [Zwischenbericht über das Vorhaben Nr. 1172 (IGF-Nr. 17734)] N2 - Aluminiumlegierungen mit besonders hoher Festigkeit werden vor allem in der Luft- und Raumfahrt sowie der Automobilindustrie eingesetzt. Ein Anwendungsbeispiel im Fahrzeugbereich sind Radialverdichterräder von Abgasturboladern. Der hierfür untersuchte Werkstoff ist die Legierung 2618A. Die hohe Festigkeit wird durch Ausscheidungshärtung erreicht. Es scheiden sich hierbei durch eine entsprechende Wärmebehandlung Al-Cu-Mg-Teilchen in die Aluminium-Matrix aus. Diese Teilchen stellen Hindernisse für die Bewegung von Versetzungen dar und haben im Fall der Legierung 2618A stabförmige Geometrie. Durch Einsatz bei Betriebstemperatur von etwa 160 °C bis 190 °C vergröbern die Teilchen im Verlauf der Einsatzzeit (Ostwaldreifung) und die Festigkeit nimmt ab. Der Zwischenbericht soll einen Überblick über die bisherigen experimentellen und theoretischen Ergebnisse geben. Es konnten Brinell-Härteverläufe nach Auslagerung bei 160 °C, 180 °C und 190 °C bis 8.760 h Auslagerungszeit gemessen werden. Erste TEM (Transmissionselektronenmikroskopie )-Untersuchungen der Mikrostruktur liegen vor. Anhand dieser Untersuchungen wurden erste Simulationen und Berechnungen der AI-Cu-Mg-Teilchengrößenentwicklung (Vergröberung) durchgeführt. Auswirkungen dieser Vergröberung der AlCu-Mg-Teilchen auf die Fließgrenze bei Raumtemperatur wurden berechnet. Weitere Ergebnisse sind Kriechversuche an Proben im Ausgangszustand T61 der Legierung 2618A bei den Temperaturen 160 °C, 180 °C und 190 °C. Um das zyklische visko-plastische Verhalten des Werkstoffes und den Einfluss der Alterung zu untersuchen, wurden LCF-Ermüdungsversuche an verschiedenen Auslagerungszuständen durchgeführt. T2 - Herbsttagung 2015 Turbomaschinen CY - Würzburg, Germany DA - 29.09.2015 KW - Aluminium alloys KW - Transmission electron microscopy KW - Microstructure KW - Coarsening PY - 2015 IS - R573 SP - 37 EP - 69 AN - OPUS4-34480 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Han, Ying A1 - Kruse, Julius A1 - Rosalie, Julian A1 - Radners, J. A1 - von Hartrott, P. A1 - Skrotzki, Birgit T1 - Influence of mean stress and overaging on fatigue life of aluminum alloy EN AW-2618A N2 - Fatigue tests were performed on the forged aluminum alloy EN AW-2618A in the T61 state. Different stress ratios (R = -1, R = 0.1) were selected to study the influence of mean stress on fatigue life. Two overaged states (10 h/230 ◦C, 1000 h/230 ◦C) were also tested to investigate the influence of overaging on fatigue life. Transmission electron microscopy (TEM) was used to characterize the precipitates (S-phase), which are mainly responsible for the strength of the alloy. A fractographic analysis was also performed to determine the failure mode. Overaging reduces the fatigue life compared to the T61 state. The longer the aging time, the lower the fatigue resistance. The reason is the decrease in (yield) strength, which correlates with the radius of the S-phase: the precipitate radius increases by a factor of approximately two for the overaged states compared to the initial state. The analysis of the fracture surfaces showed crack initiation occurs predominantly on the outer surface and is associated with the primary phases. KW - Aluminum alloys KW - Aging KW - Fatigue KW - Microstructure KW - Electron microscopy KW - S-Phase PY - 2023 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-583708 SN - 0921-5093 VL - 886 SP - 1 EP - 10 PB - Elsevier B.V. AN - OPUS4-58370 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER -