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As humanity contemplates manned missions to Mars, strategies need to be developed for the design and operation of hospitable environments to safely work in space for years. The supply of spare parts for repair and replacement of lost equipment will be one key need, but in-space manufacturing remains the only option for a timely supply. With high flexibility in design and the ability to manufacture ready-to-use components directly from a computeraided model, additive manufacturing (AM) technologies appear extremely attractive. For the manufacturing of metal parts, laser-beam melting is the most widely used AM process. However, the handling of metal powders in the absence of gravity is one prerequisite for its successful application in space. A gas flow throughout the powder bed is successfully applied to compensate for missing gravitational forces in microgravity experiments. This so-called gas-flow-assisted powder deposition is based on a porous Building platform acting as a filter for the fixation of metal particles in a gas flow driven by a pressure difference maintained by a vacuum pump.
The safe fatigue design of metallic components fabricated by additive manufacturing (AM) is still a largely unsolved problem. This is primarily due to (a) a significant inhomogeneity of the material properties across the component; (b) defects such as porosity and lack of fusion as well as pronounced surface roughness of the asuilt components; and (c) residual stresses, which are very often present in the as‐built parts and need to be removed by post‐fabrication treatments. Such morphological and microstructural features are very different than in conventionally manufactured parts and play a much bigger role in determining the fatigue life. The above problems require specific solutions with respect to the identification of the critical (failure) sites in AM fabricated components. Moreover, the generation of representative test specimens characterized by similar temperature cycles needs to be guaranteed if one wants to reproducibly identify the critical sites and establish fatigue assessment methods taking into account the effect of defects on crack initiation and early propagation. The latter requires fracture mechanics‐based approaches which, unlike common methodologies, cover the specific characteristics of so‐called short fatigue cracks. This paper provides a discussion of all these aspects with special focus on components manufactured by laser powder bed fusion (L‐PBF). It shows how to adapt existing solutions, identifies fields where there are still gaps, and discusses proposals for potential improvement of the damage tolerance design of L‐PBF components
This article is an outcome of a workshop on Fatigue of Additive Manufactured Metallic Components jointly organized by the Federal Institute for Materials Research and Testing (BAM) Berlin, Germany and the National Institute of Standards and Technology (NIST) Boulder, CO, U.S.A. The aim of the workshop was a comprehensive discussion of the specific aspects of additively manufactured (AM) components in regard to failure under cyclic loading. Undoubtedly, a better understanding and the further development of approaches for damage tolerant component design of AM parts are among the most significant challenges currently facing the use of these new technologies.
This article presents a thorough overview of the workshop discussions. It aims to provide a review of the parameters affecting the damage tolerance of AM parts with special emphasis on the process parameters intrinsic to the AM technologies, the resulting defects and residual stresses. Based on these aspects, concepts for damage tolerant component design for AM are reviewed and critically discussed.
The control of friction and wear is a major concern in many industrial applications. A promising method for tailored surface modification is the so-called laser implantation technique. This method combines surface texturing and material optimization in one processing step by a localized dispersing of hard ceramic particles using pulsed laser radiation. Wear resistant, protruding micrometric features (implants) with defined geometry can be created in a deterministic pattern where needed on highly stressed surfaces, i.e., on forming or cutting tools.
However, in order to maintain the implants over the tool’s lifetime, a suitable selection of hard ceramic particles is a prerequisite. They must provide a defect-free metal matrix composite with a high share of homogeneously distributed particles and, especially, high implant hardness. In this study, TiN, TiC, and TiB2 hard particles were compared as implant materials for the first time. By a systematic variation of pulse power and pulse duration, their dispersing behavior and influence on the material properties of AISI D2 tool steel were investigated.
Although all powder materials had grain sizes smaller than 10 μm, it was possible to disperse them by pulsed laser radiation and to obtain defect-free protruding implants. The highest share of dispersed particles (∼64%) was observed for TiB2. By scanning electron microscopy and energy dispersive x-ray spectroscopy, it was also shown that a significant share of the preplaced particles was dissolved by the laser beam and precipitated as nanometer sized particles within the matrix during solidification. These in situ formed particles have a decisive influence on the material properties. While the TiN and TiC implants have shown maximum hardness values of 750 and 850 HV1, the TiB2 implants have shown the highest hardness values with more than 1600 HV1. By x-ray diffraction, it was possible to ascribe the lower hardness values of TiC and TiN implants to high amounts of retained austenite in the metal matrix. By implanting TiB2, the formation of retained austenite was successfully suppressed due to the in situ formation of TiC particles, which was proven by electron backscatter diffraction.
In conclusion, all the implant materials are basically suitable for laser implantation on AISI D2 tool steel. However, TiB2 has shown
the most promising results.
The control of friction and wear is a major concern in many industrial applications. A promising method for a tailored surface modification is the so-called laser implantation technique. This method combines surface texturing and material optimization in one processing step by a localized dispersing of hard ceramic particles using pulsed laser radiation. Wear resistant, protruding micrometric features (implants) with defined geometry can be created in deterministic pattern where needed on highly stressed surfaces, i.e. on forming or cutting tools. However, in order to maintain the implants over the tool’s lifetime, a suitable selection of hard ceramic particles is a prerequisite. They must provide a defect-free Metal Matrix Composite with a high share of homogeneously distributed particles and especially a high implant hardness.
In this study TiN, TiC and TiB2 hard particles were compared as implant materials for the first time. By a systematic variation of the pulse power and pulse duration, their dispersing behavior and influence on the material properties of AISI D2 tool steel was investigated. Although all powder materials had grain sizes smaller than 10 µm, it was possible to disperse them by pulsed laser radiation and to obtain defect-free protruding implants. The highest share of dispersed particles (~64 %) was observed for TiB2. By scanning electron microscopy and energy dispersive X-ray spectroscopy, it was also shown that a significant share of the pre-placed particles was dissolved by the laser beam and precipitated as nanometer sized particles within the matrix during solidification. These in-situ formed particles have a decisive influence on the material properties. While the TiN and TiC implants have shown maximum hardness values of 750 HV1 and 850 HV1, the TiB2 implants have shown the highest hardness values with more than 1600 HV1. By X-ray diffraction, it was possible to ascribe the lower hardness values of TiC and TiN implants to high amounts of retained austenite in the metal matrix. By implanting TiB2, the formation of retained austenite was successfully suppressed due to the in-situ formation of TiC particles, which was proven by electron backscatter diffraction. In conclusion, all the implant materials are basically suitable for laser implantation on AISI D2 tool steel. However, TiB2 has shown the most promising results.
The potential of lowered surface features as well as the application of wear resistant coatings have been known for many years to improve the tribological behavior of forming tools. More recent studies also discuss the capability of protruded microfeatures for adjusting the tribological behavior between contacting surfaces. The demand for a high wear resistance of such structures as well as their economical and reliable production, however, often limits the industrial application. The laser implantation process can overcome these limitations. In contrast to conventional cw-laser dispersing processes, where the formation of uniform metal matrix composite layers is intended, this surface engineering technique aims to improve the tribological behavior of contacting surfaces by a localized dispersing of pre-placed hard ceramic particles. This enables the formation of deterministic textures composed of separated wear resistant dome- or ring-shaped microstructures (implants).
Since TaC shows very promising material properties for improving the wear resistance of tools exposed to severe operating conditions, this paper analyzes its suitability for pulsed laser implantation on X38CrMoV5-3 tool steel for the first time. In the experiments, the influence of the particles and the laser parameters (pulse power, pulse duration and focal diameter) on the material properties of the localized dispersed zones was studied by optical microscopy, scanning electron microscopy, energy dispersive X-ray spectroscopy and X-ray diffraction. The composite´s (micro-) hardness was measured and calculated by using a rule of mixture. Additionally, the influence of the laser parameters and the TaC particles on the geometrical properties of the implants was studied by optical microscopy and white light interferometry.
The results showed that defect-free implants with hardness values of ~900 HV1 can be obtained at the focal spot, since a localized dispersing of the TaC particles is possible using a pulsed millisecond laser. However, in dependence of the laser intensity, also a partial dissolution of the initial particles occurs. This leads to the precipitation of new dendritic TaC nanoparticles and to varying contents of retained austenite in the matrix. Both effects have a strong influence on the implant hardness and must be considert by the rule of mixture. Regarding the geometrical response it was pointed out that protruded microfeatures with heights up to 10 µm can be created. In comparison to laser remelted zones, the implanted zones showed significantly altered weld pool profiles due to the influence of the particles on the melt convection. A transition of the implant shape from predominantly dome-shaped to predominantly ring-shaped was observed for intensities >1.7∙106 W/cm2 due to the onset of the keyhole effect.
The laser implantation–named technique aims to address the tribological problems frequently seen on tool surfaces during hot stamping. It is based on the creation of elevated dome- or ring-shaped hard structures on the surface of tool steels by a localized dispersing of hard particles. Therefore, a combination of the two distinct approaches that are normally used in surface Technology for optimizing friction and wear, i.e., surface texturing and surface material optimization, are realized in one processing step. In experimental studies, a localized dispersing of TiB2 particles in the surface layer of the hot work tool steel X38CrMoV5-3 was considered and compared with punctual laser–remelted textures. The structures (micro-) hardness was measured at top- and cross-sections. With the aid of a scanning electron microscope, energy dispersive X-ray spectroscopy and X-ray diffraction the interaction between the hard particles and the substrate material were studied. From the results, an optimal parameter range was identified for laser implantation. To the investigation’s end, the implant geometry was measured by optical microscopy and White light microscopy. Furthermore, a mathematic model was introduced, which allows a prediction of the implant geometry as a response to the laser parameters. It was shown that the implantation of TiB2 particles leads to a significant hardness increase up to 1600 HV1 due to the dispersion of initial particles and an in situ precipitation of new titanium-rich phases. It was possible to create defect-free dome- and ring-shaped microstructures on the surfaces. It was also shown that the implants geometry highly depends on the applied laser parameters. The applied central composite design shows a good agreement with the experimental results.
Die Laserimplantation erlaubt die Herstellung verschleißbeständiger, erhabener Mikrostrukturen (Implants) auf Stahloberflächen durch ein diskontinuierliches Dispergieren von keramischen Partikeln mittels gepulster Laserstrahlung. Durch die flexible Anordnung separierter Implants zu komplexen Mustern erlaubt das Verfahren eine gezielte Oberflächenstrukturierung zur Beeinflussung des Reibungs- und Verschleißverhaltens. Insbesondere erwies sich Titandiborid (TiB2) als Implantationsmaterial für geeig-net, da eine Manipulation der Implantgeometrie in einem breiten Bereich vorgenommen werden konnte, ohne dass Materialdefekte wie Risse oder Poren auftraten.
Ziel der Untersuchungen war es, den Einfluss implantierter TiB2-Partikel auf die Materialeigenschaften von X153CrMoV12 zu ermitteln. Hierfür wurden im Rahmen der Arbeit die Laserparameter (Pulsleistung und -dauer) in einem breiten Parameterfeld variiert und vergleichende Untersuchungen an TiB2 implan-tierten Zonen sowie an punktuell umschmelzstrukturierten Zonen durchgeführt. Die Ergebnisse zeigen, dass eine reine Umschmelzstrukturierung zu einer deutlichen Reduktion der Oberflächenhärte aufgrund erhöhter Restaustenitgehalte (γR) führt. Im Gegensatz dazu führt das Laserimplantieren von TiB2-Partikeln zu einer deutlichen Härtesteigerung in den kuppel- oder ringförmigen Implants. Härtewerte von bis zu 1800 HV1 resultieren aus dispergierten TiB2-Primärpartikeln sowie in-situ ausgeschiedenen Se-kundärphasen, durch die der Restaustenitanteil zudem deutlich reduziert wird.
In einer Vielzahl technischer Anwendungen spielt die Aufrechterhaltung eines definierten Reibungs- und Verschleißverhaltens zwischen bewegten Oberflächen für die Sicherheit und Funktionalität eine entscheidende Rolle. Die Oberflächentechnik versucht durch geeignete Verfahren die Randschichten zu ertüchtigen, um Reibung und Verschleiß zu kontrollieren. Eine Verbesserung der Materialeigenschaften kann durch flächige Beschichtungen erreicht werden. Zusätzlich ermöglichen Oberflächenstrukturierungen breite Möglichkeiten zur Beeinflussung des Schmierungszustandes bzw. der Kontaktbedingungen. Neben Negativstrukturen bieten ebenfalls erhabene Mikrostrukturen großes Potenzial zur Beeinflussung des tribologischen Verhaltens. Ihr Einsatz ist aber aufgrund der besonderen Verschleißproblematik erhabener Strukturen momentan limitiert, so dass in der Regel zusätzliche verschleißreduzierende Beschichtungen notwendig werden.
In diesem Beitrag wurde das Verfahren der Laserimplantation angewandt, mit dem erhabene und separierte Oberflächenstrukturen hoher Verschleißfestigkeit in einem Fertigungsschritt erzeugbar sind. Das Verfahren basiert auf einem lokalisierten Dispergieren von Hartstoffpartikeln. Hierfür wurde erstmalig ein gepulster Faserlaser mit hoher Strahlqualität zur Erzeugung punkt- und linienförmiger Mikrostrukturen angewandt. Versuche wurden auf dem Kaltarbeitsstahl X153CrMoV12 unter Anwendung von Titandiborid als Hartstoff durchgeführt. Anhand von Härtemessungen konnte gezeigt werden, dass sowohl punkt- als auch linienförmige Strukturen mit Härten über 1000 HV1 und einer feinkörnigen Mikrostruktur mit feinverteilten Hartstoffpartikeln herstellbar sind. Des Weiteren war es möglich, die Implantgeometrien, welche an Querschliffen und durch Weißlichtinterferometeraufnahmen erfasst wurden, durch die Pulsleistung und Pulsdauer zu steuern.
In einer Vielzahl technischer Anwendungen spielt die Aufrechterhaltung eines definierten Reibungs- und Verschleißverhaltens zwischen bewegten Oberflächen für die Sicherheit und Funktionalität eine ent-scheidende Rolle. Die Oberflächentechnik versucht durch geeignete Verfahren die Randschichten zu ertüchtigen, um Reibung und Verschleiß zu kontrollieren. Eine Verbesserung der Materialeigenschaften kann durch flächige Beschichtungen erreicht werden. Zusätzlich ermöglichen Oberflächenstrukturierun-gen breite Möglichkeiten zur Beeinflussung des Schmierungszustandes bzw. der Kontaktbedingungen. Neben Negativstrukturen bieten ebenfalls erhabene Mikrostrukturen großes Potenzial zur Beeinflussung des tribologischen Verhaltens. Ihr Einsatz ist aber aufgrund der besonderen Verschleißproblematik er-habener Strukturen momentan limitiert, so dass in der Regel zusätzliche verschleißreduzierende Be-schichtungen notwendig werden.
In diesem Beitrag wurde das Verfahren der Laserimplantation angewandt, mit dem erhabene und sepa-rierte Oberflächenstrukturen hoher Verschleißfestigkeit in einem Fertigungsschritt erzeugbar sind. Das Verfahren basiert auf einem lokalisierten Dispergieren von Hartstoffpartikeln. Hierfür wurde erstmalig ein gepulster Faserlaser mit hoher Strahlqualität zur Erzeugung punkt- und linienförmiger Mikrostrukturen angewandt. Versuche wurden auf dem Kaltarbeitsstahl X153CrMoV12 unter Anwendung von Titandibo-rid als Hartstoff durchgeführt. Anhand von Härtemessungen konnte gezeigt werden, dass sowohl punkt- als auch linienförmige Strukturen mit Härten über 1000 HV1 und einer feinkörnigen Mikrostruktur mit feinverteilten Hartstoffpartikeln herstellbar sind. Des Weiteren war es möglich, die Implantgeometrien, welche an Querschliffen und durch Weißlichtinterferometeraufnahmen erfasst wurden, durch die Puls-leistung und Pulsdauer zu steuern.