TY - CONF A1 - Zerbst, Uwe T1 - Defects as a root cause for fatigue failure of metallic components N2 - The Topic of the presentationis a discussion on defects which can cause failure in cyclically loaded metallic components. Although also touching Features such as material defects such as pores or micro-shrinkages, etc. and geometric defects such as surface roughness and secondary notches (which are not considered in the design process) which origin in manufacturing, and others the presentation concentrates on non-metallic inclusions. It is prefaced by an introduction to the life cycle of a fatigue crack from initiation up to fracture. Special emphasis is put on the fact that only cracks which are not arrested during one of their distinct Propagation stages can grow to a critical size. T2 - VIII. International Conference on Engineering Failure Analysis CY - Budapest, Ungarn DA - 08.06.2018 KW - Metallic components KW - Material defects KW - Micro-shrinkages PY - 2018 AN - OPUS4-46875 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Grundmann, Jana A1 - Bodermann, Bernd A1 - Ermilova, Elena A1 - Weise, Matthias A1 - Hertwig, Andreas A1 - Klapetek, Petr A1 - Rafighdoost, Jila A1 - Pereira, Silvania F. T1 - Optical and tactile measurements on SiC sample defects N2 - Abstract. In power electronics, compound semiconductors with large bandgaps, like silicon carbide (SiC), are increasingly being used as material instead of silicon. They have a lot of advantages over silicon but are also intolerant of nanoscale material defects, so that a defect inspection with high accuracy is needed. The different defect types on SiC samples are measured with various measurement methods, including optical and tactile methods. The defect types investigated include carrots, particles, polytype inclusions and threading dislocations, and they are analysed with imaging ellipsometry, coherent Fourier scatterometry (CFS), white light interference microscopy (WLIM) and atomic force microscopy (AFM). These different measurement methods are used to investigate which method is most sensitive for which type of defect to be able to use the measurement methods more effectively. It is important to be able to identify the defects to classify them as critical or non-critical for the functionality of the end product. Once these investigations have been completed, the measurement systems can be optimally distributed to the relevant defects in further work to realize a hybrid analysis of the defects. In addition to the identification and classification of defects, such a future hybrid analysis could also include characterizations, e.g. further evaluation of ellipsometric data by using numerical simulations. KW - Compound semiconductors KW - Hybrid metrology KW - Material defects KW - Spectroscopic ellipsometry KW - Scanning probe microscopy KW - White-light interference microscopy PY - 2024 UR - https://nbn-resolving.org/urn:nbn:de:kobv:b43-601220 DO - https://doi.org/10.5194/jsss-13-109-2024 SN - 2194-878X VL - 13 IS - 1 SP - 109 EP - 121 PB - Copernicus Publ. CY - Göttingen AN - OPUS4-60122 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Duarte, Larissa T1 - Application of the cyclic R-curve analysis to determine the Kitagawa-Takahashi Diagram N2 - The fatigue limit of metallic materials corresponds to the maximum stress below which all microcracks that were originally able to grow still arrest. In technical alloys, microcracks are normally initiated at material defects. As a result, the fatigue limit of these materials is a function of the defect size. The Kitagawa-Takahashi Diagram (KT-diagram) provides a useful description of this dependency. However, the established methods for its determination are associated with great uncertainties, especially in the technically interesting region corresponding to the short crack regime. In addition, the effect of crack closure and the influence of local stresses are not considered. For this reason, short crack models offer a better alternative for estimating KT-diagrams. In this work, a methodology is presented that incorporates the determination of the fatigue limit based on crack arrest (cyclic R-curve analysis). The crack driving force is determined by FE simulations, while the increase in material resistance with cyclic crack propagation in the region of physically short cracks is described experimentally by the cyclic R-curve. To validate the procedure, fatigue limit tests based on the staircase method are carried out on smooth and notched specimens with 3 different notch sizes. Furthermore, tests are carried out on a low-alloyed steel with two different heat treatments for considering different strengths. The experimental results are compared with the simulations and the possible differences are discussed. T2 - 5th International Symposium on Fatigue Design and Material Defects CY - Trento, Italy DA - 14.05.2025 KW - Fatigue limit KW - Material defects KW - Kitagawa-Takahashi Diagram KW - Cyclic R-curve analysis PY - 2025 AN - OPUS4-63144 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Bär, Jürgen T1 - Determination of the Kitagawa-Takahashi Diagram using DC Potential Drop Measurements N2 - The Kitagawa-Takahashi Diagram is an important tool for describing the fatigue limit of components containing defects. The models used for its description differ, particularly in the transition region corresponding to the short crack regime. Therefore, for a reliable statement about the fatigue limit in this area, an experimental validation of the curve is necessary. However, the standardized stair-case method requires a large number of samples and has a long test duration. In this work, a method is presented that allows a simpler and faster validation of the Kitagawa-Takahashi Diagram in the region of short cracks. Notches with a defined width and depth were manufactured in flat samples of a low-alloyed steel with two different heat treatments using an engraving laser. This method allows to produce very sharp notches without plastic deformation and with only a slight thermal influence on the surrounding material. The samples prepared in this way were fatigued with block wise increasing loads until failure. Cracks are detected by means of a direct current potential drop method. The length of the loading block (number of cycles) is determined by the measured potential drop. This procedure enables a reliable and precise determination of the limit stress for the respective notch size with a low experimental effort and time consumption. T2 - 5th International Symposium on Fatigue Design and Material Defects CY - Trento, Italy DA - 14.05.2025 KW - Fatigue limit KW - Material defects KW - Kitagawa-Takahashi Diagram KW - DC Potential Drop PY - 2025 AN - OPUS4-63145 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Zerbst, Uwe A1 - Klinger, Christian T1 - Material defects as cause for the fatigue failure of metallic components N2 - The paper provides an overview on material defects which may serve as fatigue crack initiation sites and can cause final fatigue failure of a component. These comprise nonmetallic inclusions in Steel and aluminum alloys, cavities such as pores, micro-shrinkages and un-welded regions in cast, sinter and additively manufactured alloys, graphite nodules, shrinkages and other items in modular cast iron, regions of defective microstructure, microcracks and secondary notches such as undercuts and surface roughness. Besides their origin, the effect and mechanisms on fatigue crack initiation and propagation are discussed. The considerations are proceeded and accompanied by a Brief discussion of some Basic aspects such as the stages of crack propagation along their length scale, the overcoming of crack arrest and the question when a secondary notch can be treated as a crack. KW - Material defects KW - Fatigue strength and life KW - Non-metallic inclusions KW - Pores KW - Shrinkages KW - Graphite modules KW - Surface roughness PY - 2019 DO - https://doi.org/10.1016/j.ijfatigue.2019.06.024 SN - 0142-1123 SN - 1879-3452 VL - 127 SP - 312 EP - 323 PB - Elsevier AN - OPUS4-49127 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER -