Ingenieurwissenschaften und zugeordnete Tätigkeiten
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Atemluftflaschen aus Faserverbundwerkstoffen werden im Feuerwehrbetrieb hohen thermischen Belastungen ausgesetzt. Der thermisch sichere Bereich dieser Behälter ist jedoch heutzutage noch nicht einschätzbar. Deshalb haben es sich die Bundesanstalt für Materialforschung und -prüfung (BAM) im Austausch mit der Bergischen Universität Wuppertal zur Aufgabe gemacht, die Auswirkungen dieser Betriebslasten zu untersuchen. Die Erkenntnisse dieser Untersuchungsreihe werden genutzt, um einzuschätzen, ob es sicherheitstechnisch notwendig ist, besondere thermische Betriebsbedingungen in normativen Prüfkriterien zu berücksichtigen.
In einem ersten Schritt wurden Typ-III-Atemluftflaschen der Berliner Feuerwehr Umgebungsbedingungen des typischen Belastungsprofils der Brandbekämpfung (130 °C bis 250 °C, 10 Minuten) ausgesetzt, um die Erwärmung des Behältermaterials zu erfassen. Da die Größe der bestrahlten Oberfläche in einem Brandeinsatz nicht bekannt ist, erfolgte zusätzlich eine Variation der Strahlungsexposition. Strömungsprozesse, die in einem Brandeinsatz den Behälter von innen kühlen, wurden in diesem ersten Untersuchungsabschnitt noch nicht betrachtet.
Es konnte gezeigt werden, dass der Aluminium-Liner einer Typ-III-Atemluftflasche einen erheblichen Einfluss auf die Temperaturverteilung im Behältermaterial ausübt. Die hohe Leitfähigkeit des Aluminiums führt bei Verringerung der bestrahlten Behälteroberfläche zu hohen Temperaturgradienten innerhalb der Behälterwand. Die Materialtemperaturen in der Atemluftflasche konnten für das Belastungsprofil der Brandbekämpfung auf ein typisches Temperaturintervall eingegrenzt werden. Die Grenzen liefern Aussagen zur exponierten Behälteroberfläche und liegen zwischen einseitiger und Vollbestrahlung.
Characterization of multiphase metal matrix composites by means of CT and neutron diffraction
(2016)
The present study examines the relationship between the microstructure of multiphase MMC and their damage mechanisms. The matrix AlSi12CuMgNi was combined with 15% vol. Al2O3 (short fibres) and with 7% vol. Al2O3 + 15% vol. SiC (short fibres and whiskers, respectively). The experimental approach encompasses 3D microstructure characterization by means of computed tomography of samples (a) as-received, (b) after heat treatment, and (c) after compression tests at room temperature. The volume fraction of different phases, their distribution, their orientation and the presence of defects and damage are studied.
Influence of addition of SiC whiskers on mechanical properties of composite was investigated. Phase-specific load partition analysis for samples with fibre plane parallel to load was perform by using neutron diffraction measurements during in-situ compression. It shows damage in the Si phase, while Al2O3 short fibres carry load without damage until failure. The computed tomography observations confirm the load partition analysis.
The paper addresses the ‘Determining the influence of preparation and measurement conditions on bonding strength using CAT-Technology’ and the follow points are discussed in more detail: Motivation, CAT – Technology, Influence of bonding area on bonding strength, Influence of storing & measurement temperatures and Influence of substrate thickness and coating support.
An exciting challenge is to create unduloid-reinforcing fibers with tailored dimensions to produce synthetic composites with improved toughness and increased ductility. Continuous carbon fibers, the state-of-the-art reinforcement for structural composites, were modified via controlled laser irradiation to result in expanded outwardly tapered regions, as well as fibers with Q-tip (cotton-bud) end shapes. A pulsed laser treatment was used to introduce damage at the single carbon fiber level, creating expanded regions at predetermined points along the lengths of continuous carbon fibers, while maintaining much of their stiffness. The range of produced shapes was quantified and correlated to single fiber tensile properties. Mapped Raman spectroscopy was used to elucidate the local compositional and structural changes. Irradiation conditions were adjusted to create a swollen weakened region, such that fiber failure occurred in the laser treated Region producing two fiber ends with outwardly tapered ends. Loading the tapered fibers allows for viscoelastic energy dissipation during fiber pull-out by enhanced friction as the fibers plough through a matrix. In these tapered fibers, diameters were locally increased up to 53%, forming outward taper angles of up to 1.8°. The tensile strength and strain to failure of the modified fibers were significantly reduced, by 75% and 55%, respectively, ensuring localization of the break in the expanded region; however, the fiber stiffness was only reduced by 17%. Using harsher irradiation conditions, carbon fibers were completely cut, resulting in cottonbud fiber end shapes. Single fiber pull-out tests performed using these fibers revealed a 6.75-fold increase in work of pull-out compared to pristine carbon fibers. Controlled laser irradiation is a route to modify the shape of continuous carbon fibers along their lengths, as well as to cut them into controlled lengths leaving tapered or cotton-bud shapes.
Characterization of the mechanical properties of interphases is essential when designing multicomponent materials such as fiber-reinforced matrices, protective coatings or multi-layered structures for integrated circuits. It can provide vital information about the durability of the finished product as a composite because failure is often initiated in the interfacial region induced by internal or external stress during fabrication or service. Nanoindentation is a powerful tool for investigating mechanical properties on the micro/nano scale. However, there are some challenges associated with conducting nanoindentation near interface regions. One main challenge is that the small thickness of the interphase region (typically 1-2µm) makes it difficult to apply several adjacent indents without overlap. Another issue is that the indentations are usually restricted by local reinforcement, and it becomes difficult to isolate the change in mechanical properties due solely to interphase formation. In this study we try to gauge the feasibility of nanoindentation for characterizing epoxy/Cu interphases. We develop a sample preparation method and optimize nanoindentation parameters in an attempt to avoid the restrictions mentioned above. Atomic force microscopy (AFM) and finite element analysis are employed as reference techniques to evaluate the effectiveness of our technique. We show the influence of preparation method and nanoindentaion parameters on measurements of interphase properties and how they relate the mentioned challenges.