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- MALDI-TOF MS (2)
- Polylactide (2)
- Additive manufacturing (1)
- Biobased (1)
- Capillary (1)
- Corrosion resistance (1)
- Crystalinity (1)
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Organisationseinheit der BAM
Twice recrystallized L-lactide was polymerized with a dozen of different tin or bismuth catalysts in bulk at 160°C for 24 h and was annealed at 150°C afterwards. In two cases Tm values above 197.0°C were obtained. The parameters causing a scattering of the DSC data were studied and discussed. The samples prepared with SnCl2, 2,2-dibutyl-2-stanna-1,3-ditholane (DSTL) or cyclic tin(II) bisphenyldioxide (SnBiph) were subject to annealing programs with variation of time and temperatures, revealing that the Tm´s did not increase. However, an increase of Hm was achieved with maximum values in the range of 93-96 J g-1 corresponding to crystallinities off around 90%. Further studies were performed with once recrystallized L-lactide. Again, those samples directly crystallized from the polymerization process showed the highest Tm values. These data were compared with the equilibrium Tm0 and Hm0 data calculated by several research groups for perfect crystallites. A Tm0 of 213+/-2°C and a Hm0 of 106 J g-1 show the best agreement with the experimental data. The consequences of annealing for the thickness growth of crystallites are discussed on the basis of SAXS measurements. Finally, a comparison of cyclic and linear poly L-lactide)s is discussed.
Instead of foreseeing and preparing for all possible scenarios of machine failures, accidents, and other challenges arising in space missions, it appears logical to take advantage of the flexibility of additive manufacturing for “in-space manufacturing” (ISM). Manned missions into space rely on complicated equipment, and their safe operation is a great challenge. Bearing in mind the absolute distance for manned missions to the Moon and Mars, the supply of spare parts for the repair and replacement of lost equipment via shipment from Earth would require too much time. With the high flexibility in design and the ability to manufacture ready-to-use components directly from a computer-aided model, additive manufacturing technologies appear to be extremely attractive in this context. Moreover, appropriate technologies are required for the manufacture of building habitats for extended stays of astronauts on the Moon and Mars, as well as material/feedstock. The capacities for sending equipment and material into space are not only very limited and costly, but also raise concerns regarding environmental issues on Earth. Accordingly, not all materials can be sent from Earth, and strategies for the use of in-situ resources, i.e., in-situ resource utilization (ISRU), are being
envisioned. For the manufacturing of both complex parts and equipment, as well as for large infrastructure, appropriate technologies for material processing in space need to be developed.
Die Korrosionsbeständigkeit martensitischer nichtrostender Stähle (MNS) wird wesentlich von der chemischen Zusammensetzung und dem Wärmebehandlungszustand beeinflusst. Beides bestimmt die Verteilung der Legierungselemente im Gefüge und die daraus resultierenden Werkstoffeigenschaften. Das Legieren mit Stickstoff bewirkt im Allgemeinen eine Verbesserung der Lochkorrosionsbeständigkeit von nichtrostenden Stählen. Bei martensitischen nichtrostenden Stählen ist dieser Effekt nicht nur auf den Stickstoffgehalt selbst zurückzuführen, sondern auch auf den gleichzeitig verringerten Kohlenstoffgehalt, der ebenfalls das Ergebnis der Wärmebehandlung beeinflusst. In dieser Arbeit wird der Einfluss von Stickstoff auf die Korrosionsbeständigkeit in Bezug zum Härtungsprozess von MNS dargestellt. Dazu wird vergleichend der Effekt von Austenitisierungsdauer, -temperatur und Abkühlgeschwindigkeit auf Gefüge, Härte und Korrosionsbeständigkeit der MNS X50CrMoV15 und X30CrMoN15 1 untersucht. Die Abkühlgeschwindigkeit wurde mit dem Stirnabschreckversuch gezielt variiert, um den Einfluss von Abkühlgeschwindigkeiten von > 100 K/s bis 1 K/s zu charakterisieren. Die Veränderungen der Korrosionsbeständigkeit werden durch die elektrochemisch potentiodynamische Reaktivierung (EPR) und durch die Bestimmung kritischer Lochkorrosionspotentiale dokumentiert. Neben diesem experimentellen Ansatz werden auch die Ergebnisse von thermodynamischen Berechnungen mit der Software Thermocalc vorgestellt und abschließend auch zur Interpretation des Einflusses von Stickstoff auf die Korrosionsbeständigkeit martensitischer nichtrostender Stähle genutzt.
Absorption effects in total reflection X-ray fluorescence (TXRF) analysis are important to consider, especially if external calibration is to be applied. With a color X-ray camera (CXC), that enables spatially and energy resolved XRF analysis, the absorption of the primary beam was directly visualized for mL-droplets and an array of pL-droplets printed on a Si-wafer with drop-on-demand technology. As expected, deposits that are hit by the primary beam first shade subsequent droplets, leading to a diminished XRF signal. This shading effect was quantified with enhanced precision making use of sub-pixel analysis that improves the spatial resolution of the camera. The measured absorption was compared to simulated results using three different model calculations. It was found they match very well (average deviation < 10%). Thus errors in quantification due to absorption effects can be accounted for in a more accurate manner.
Ring-expansion polymerizations (REPs) catalyzed by two cyclic tin catalysts (2-stanna-1.3-dioxa-4,5,6,7-dibenzazepine [SnBiph] and
2,2-dibutyl-2-stanna-1,3-dithiolane [DSTL]) are performed at 140 °C in bulk.
Small amounts (4 vol%) of chlorobenzene or other solvents are added to
facilitate transesterification reactions (ring–ring equilibration) in the solid poly(l-lactide)s. In the mass range up to m/z 13 000 crystalline PLAs displaying a so-called saw-tooth pattern in the MALDI-TOF mass spectra are obtained indicating the formation of extended-ring crystals. The characteristics of extended-ring crystallites and folded-ring crystallites are discussed. Furthermore, extremely high melting temperatures (Tm’s up to 201.2 °C) and melting enthalpies (𝚫Hm’s up to 106 J g−1)) are found confirming that 𝚫Hm max, the 𝚫Hm of a perfect crystal, is around or above 115 J g−1 in contrast to literature data.
Glycolide was polymerized in bulk by means of four different ROPPOC catalysts: tin(II) 2-ethylhexanoate (SnOct2), dibutyltin bis(pentafluoro-phenoxide) (BuSnOPF),zinc biscaproate (ZnCap), and zinc bis(pentafluoro-phenyl sulfide) (ZnSPF). The temperature was varied between 110 and 180°C and the time between 3 h and 7 days. For the few polyglycolides (PGAs) that were soluble extremely high molecular masses were obtained. The MALDI TOF mass spectra had all a low signal-to-noise ration and displayed the peaks of cyclic PGAs with a“saw-tooth pattern ”indicating formation of extended-ring crystallites in the mass range below m/z 2500. The shape of DSC curves varied considerably with catalyst and reaction conditions, whereas the long-distance values measured by SAXS were small and varied little with the polymeriza-tion conditions.