TY - CONF A1 - Madia, Mauro T1 - Analytische Beschreibung von Rissarrest, Kurz- und Langrisswachstum in Schweißverbindungen T2 - DVS-Congress 2015 CY - Nürnberg DA - 2015-09-14 PY - 2015 AN - OPUS4-33499 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - Fatigue Strength of Aerospace Parts Repaired by Cold Spray N2 - Aerospace components are safety critical parts, which are often replaced when found defective after the fabrication process or after periodic inspection in-service. Cold spray repair is a promising and cost-saving alternative to replacing worn parts. Depositing materials in decent quality fill machined damage volumes can enhance the performance of refurbished parts and extend their working life. Furthermore, repair represents a resource-efficient and green process in a world targeting at decarbonization of many industrial sectors. Component repair consists of a defined sequence of operations. First, damage is removed by machining, then new material is applied by cold spray on the machined substrate. Usually, the original functional shape of the component is restored by machining. Post-spraying heat treatments can be applied where required. Despite the advantages, cold spray repair still suffers from major limitations which prevent its application in safety relevant parts. The main challenges are posed by the poor adhesion strength, the porosity inherent in the manufacturing process, the reduced ductility and the presence of residual stresses. This work presents recent results obtained in the frame of the cluster project CORE devoted to the development of automatized repair of aerospace parts by cold spray. The investigations consider high-strength aluminum alloys typically used in structural applications in the aerospace industry. As the fatigue properties are crucial to the safe application of repaired components, and given the presence of process-induced defects, a damage tolerant framework is peculiarly suitable for the structural integrity assessment of repaired commponents and give an indication of the permissible defects to optimize the parameters of the cold spray process. Several high cycle fatigue and fatigue crack propagation tests have been performed to compare the fatigue performance of base and repaired materials. The mechanical tests are corroborated by fractographic and microstructural investigations. T2 - ICAM2024 CY - Atlanta, GA, USA DA - 28.10.2024 KW - Cold Spray KW - Aerospace KW - Repair KW - Structural Integrity KW - Fatigue Strength PY - 2024 AN - OPUS4-61539 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - Ermittlung der Wöhlerkurve von Schweißverbindungen mittels bruchmechanischer Methoden N2 - IBESS steht für „Integrale Bruchmechanische Ermittlung der Schwingfestigkeit von Schweißverbindungen“ und ist das Ergebnis eines DFG-AiF-Clusters, an dem acht Partner beteiligt waren. Kernstück ist eine analytische Methode zur bruchmechanischen Beschreibung der Rissausbreitung unter Schwingbelastung, die im IBESS-Teilprojekt A3 entwickelt wurde. Da man es im Bereich der Schwingfes-tigkeit mit kurzen Rissen zu tun hat, auf die die etablierten Methoden der Langrissbruchmechanik nicht anwendbar sind, wurden Lösungen entwickelt, die es erlauben, sowohl die rissnahen Plastizitätsverhältnisse als auch die mit wachsendem Riss graduell zunehmenden Rissschließeffekte quantitativ zu beschreiben. Unter Einbeziehung der sogenannten „zyklischen R-Kurve“, deren experimentelle Methodik ebenfalls im Rahmen des Projekts weiterentwickelt wurde, ist es zudem möglich, Ausgangsrissgrößen vorherzusagen, die auf Dauerfestigkeitsniveau gerade so noch arretieren würden. Dies erlaubt umgekehrt eine Abschätzung der Dauerfestigkeit an den Schweißverbindungen sowie die statistisch basierte, analytische Vorhersagen des Zeitfestigkeitsastes der Wöhlerkurve. In diesem Aufsatz wird die Methodik vorgestellt und ihre Validierung an einem ausgewählten Beispiel diskutiert. T2 - DVM-Arbeitskreis Bruchmechanik und Bauteilsicherheit CY - Freiburg/Breisgau, Germany DA - 16.02.2016 KW - Ermüdungsrissausbreitung KW - Schwingfestigkeit KW - Schweißverbindungen PY - 2016 AN - OPUS4-37953 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - Fracture mechanics-based determination of the fatigue strength of weldments N2 - The 21st century brought new and complex technological challenges, which need to be solved. Of primary importance is the global energy transition that pushes forward the research and innovation in order to achieve the goal of replacing the existing non-renewable energy sources with new renewable and efficient ones, with positive effects on the world climate. In many countries worldwide mid- and long-term goals have been set out in order to reduce the greenhouse gas emissions. Germany, among others, intends to reduce the emissions by 80 to 95% within 2050, compared with 1990 levels. The achievement of this goal is aimed to be realized by the development of new and more efficient energy sources, but also by substantial investments in electromobility (the goal is to bring one million electrically driven vehicles onto German streets by 2020). Another important challenge came into play following the global financial crisis, which pushed many industries to reduce their operational and maintenance costs. In particular, the life-cycle management of a component has become of primary importance. In some cases it has been shown that the underestimation or the lack of awareness in ageing of plants led to incidents due to the loss of technical integrity. Other studies demonstrated that the component life of many of the long-life components could be extended up to 50% without compromising safety. The third, not less important, challenge is driven by the development of new technologies and materials. The trends show a large investment in additive manufactured metal components and new metallic materials which have to assure longer in-service life, lightweighting and efficient recycling. This works aims at addressing part of these problems by proposing a fracture mechanics-based analytical procedure for the determination of the fatigue lives of engineering components and particularly of welded joints. In fact, an analytical tool, which is able to simulate the main failure mechanisms of weldments under fatigue loading, brings many advantages: i) drastic reduction of long and expensive experimental tests; ii) optimization of the geometry and production processes (possible weight reduction); iii) better estimate of the safety margins used in the design of the components (life extension without safety issues). The results show that the model can fairly well predict the lives of the welded joints investigated experimentally, irrespective of the geometry and loading conditions. T2 - WMRIF 5th International Workshop for Young Scientists CY - Tsukuba, Japan DA - 08.11.2016 KW - Structural integrity KW - Weldments KW - Fatigue strength PY - 2016 AN - OPUS4-38390 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - Multiple crack initiation and propagation in weldments under fatigue loading N2 - The work aims at addressing the modelling and implementation of criteria for multiple crack propagation, including interaction and coalescence, for a more reliable fracture mechanics-based prediction of stress-life curves for weldments. A large experimental work is presented in which micro-cracks have been made visible by heat-tinting at successive stages of fatigue life of the welded specimens. Here the correlation between the number of initiation sites and the applied stress level has been also investigated. The criteria have been implemented in in-house software, which allows multiple fatigue crack propagation, and validated against selected experimental tests. The results have shown that the modelling of multiple crack propagation and interaction is crucial for the prediction of the fatigue strength of weldments, both in finite and infinite life regime. T2 - FDMD 2017 CY - Lecco, Italy DA - 19.09.2017 KW - Weldments KW - Fatigue strength KW - Multiple crack propagation KW - Short cracks PY - 2017 AN - OPUS4-43857 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - Fatigue strength and fracture mechanics N2 - This invited plenary lecture is aimed at giving a General overview about the assessment of the fatigue strength of metallic components under constant Amplitude loading based on fracture mechanics. A particular Focus is put on the Evaluation of the fatigue crack driving force and material resistance to fatigue crack Propagation in the Regime of physically/mechanically short cracks. The potential of the methodolody is demonstrated on case studies dealing with the fatigue life prediction of welded joints. T2 - SAM-CONAMET 2018 CY - San Carlos de Bariloche, Argentina DA - 01.10.2018 KW - Structural Integrity KW - Fatigue strength KW - Short crack Propagation PY - 2018 AN - OPUS4-46873 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - IBESS Methology for the fracture mechanics-based determination of the fatigue strength of weldments N2 - The presentation provides a brief overview on the results of a German cluster project on the use of fracture mechanics to the determination of the fatigue strength of weldments with fatigue cracks originating at the weld toes. The approach includes (a) a concept for short crack propagation for which the common K concept is not applicable and the crack closure effects are still being gradually build-up, (b) a method for determining fatigue life relevant initial crack sizes as they are needed in any fracture mechanics analysis and (c) multiple cracking and crack coalescence at load levels higher than the endurance limit. The analyses are stochastically performed. Both, the endurance limit as defined for 107 loading cycles and the finite life branch of the S-N curve are determined. T2 - ESIS TC1 Workshop on Damage and Damage Tolerance of Welded Structures CY - Prague, Czech Republic DA - 12.04.2018 KW - Structural Integrity KW - Fatigue strength KW - Weldments PY - 2018 AN - OPUS4-46878 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - On the modelling of the fatigue strength of am components N2 - The topic of the presentation consists in some basic considerations on the application of fracture mechanics to fatigue live and strengh prediction of metallic componends manufatured by additive manufacturing. These are based on an approach developed at BAM which comprises elements such as the elastic-plastic modelling of the cyclic crack driving force, a physically meaningfull determination of the initial crack size and multipile crack initiation and propagation due to variations of the local geometry and material charactaristics. Spezial emphasis is put to spezific aspects of materials composed by selectiv laser melting such as surface roughness, porosity and gradiants in the microstructure. N2 - Beschreibung der IBESS-Prozedur zur zukünftigen Anwendung zur Berechnung der Schwingfestigkeit von Schweißverbindungen T2 - Additive Manufracturing Benchmarks 2018 CY - Gaithersburg, Maryland, USA DA - 18.06.2018 KW - Structural Integrity KW - Fartigue Strength KW - Additive Manufacturing PY - 2018 AN - OPUS4-46062 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Zerbst, Uwe A1 - Madia, Mauro A1 - Vormwald, M. T1 - Fatigue strength and fracture mechanics N2 - If fracture mechanics shall be applied to the total lifetime respectively the fatigue limit of components (within the meaning of the S-N curve approach) it has to address four challenges: (a) It has to adequately describe so-called short crack propagation, which cannot be based on the common long crack concepts for principle reasons. Since the crack size is in the order of the plastic zone size, the modelling of short crack propagation cannot be based on the common linear elastic Delta K concept. Instead, an elastic-plastic parameter such as the cyclic J integral has to be applied. A second point is that the crack closure concept has to be modified in that the crack opening stress is not a constant, crack size- independent parameter but shows a transient behaviour with increasing short crack size. (b) It has to provide a meaningful definition of the initial crack dimensions as the starting point for an S-N curve relevant (residual) lifetime analysis. This can be based either on the (statistical) size of material defects which can be treated as cracks or by the size of the crack which would arrest subsequent to early crack propagation, whatever is larger. (c) It has to cope with the problem of multiple cracks for load levels higher than the fatigue limit such as it occurs in many applications in the absence of very large initial defects. (d) This requires consequent statistical treatment taking into account variations in the local geometry of the area where crack initiation has to be expected as well as the scatter in the initial crack size and in the material data used for the analyses. T2 - 2nd International Conference on Structural Integrity CY - Funchal, Madeira, Portugal DA - 04.09.2017 KW - Fatigue strength KW - Fracture mechanics KW - Initial crack size KW - Short crack propagation KW - Multiple crack propagation PY - 2017 AN - OPUS4-42546 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Madia, Mauro T1 - Approximation of the crack driving force for cracks at notches under static and cyclic loading N2 - The work deals with the efficient calculation of the elastic-plastic crack driving force (J-integral for monotonic loading andΔJ-integral under cyclic loading) for short cracks at notches as essential parameter for the reliable static and fatigue assessment of notched structures. The J- or ΔJ-integral is calculated based on analytical solutions for stress intensity factors, estimated by means of well-known weight function solutions in the case of cracks under power-law stress distributions. A plasticity-correction function is applied to the stress intensity factors to obtain the final expression of the crack driving force. The comparison between analytical solutions and finite element calculations in case of cracks at the weld toe in welded joints shows good agreement. T2 - 2nd International Conference on Structural Integrity CY - Funchal, Madeira, Portugal DA - 04.09.2017 KW - Structural integrity KW - Fracture mechanics KW - Crack driving force KW - Notches PY - 2017 AN - OPUS4-42558 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER -