TY - JOUR A1 - Schloesser, J. A1 - Bäker, M. A1 - Rösler, J. A1 - Pulz, Robert T1 - Oxidation behavior of thermal barrier coatings on copper substrates JF - Advances in science and technology N2 - In rocket engine combustion chambers, the cooling channels experience extremly high temperatures and environmental attack. Thermal protection can be provided by Thermal Barrier Coatings. Due to the need of good heat conduction, the inner combustion liner is made of copper. The performance of a standard coating system for nickel based substrates is investigated on copper substrates. Thermal cycling experiments are performed on the coated samples. Due to temperature limitations of the copper substrate material, no thermally grown oxide forms at the interface of the thermal barrier coating and the bond coat. Delamination of the coatings occurs at the interface between the substrate and the bond coat due to oxide formation of the copper at uncoated edges. In real service a totally dense coating can probably not be assured which is the reason why this failure mode is of importance. Different parameters are used for thermal cycling to understand the underlying mechanisms of delamination. Furthermore, laser heating experiments account for the high thermal gradient in real service. Pilot tests which led to a delamination of the coating at the substrate interface were performed successfully. KW - Thermal barrier coating KW - Copper substrate KW - Rocket engine KW - Oxidation protection PY - 2010 DO - https://doi.org/10.4028/www.scientific.net/AST.66.74 SN - 1662-0356 VL - 66 SP - 74 EP - 79 PB - Techna CY - Faenza AN - OPUS4-22125 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Hartnig, C. A1 - Manke, I. A1 - Schloesser, J. A1 - Krüger, P. A1 - Kuhn, R. A1 - Riesemeier, Heinrich A1 - Wippermann, K. A1 - Banhart, J. T1 - High resolution synchrotron X-ray investigation of carbon dioxide evolution in operating direct methanol fuel cells JF - Electrochemistry communications N2 - The carbon dioxide evolution and bubble formation in an operating fuel has been studied by means of synchrotron X-ray radiography. Two different observation directions have been chosen: a through-plane insight has been employed to track the formation of bubbles starting at the corner of the lands of the flow field; a depth profile of the carbon dioxide evolution has been derived from cross sectional studies describing an affected area of up to 100 µm. The dynamics of the bubble formation and detachment of the bubbles from the position of formation is strongly correlated with the current density. Cracks and breaks in the catalyst layer which result from the preparation process are visible under operating conditions and a possible swelling of the catalyst layer does not reach a complete vanishing of the cracks. KW - DMFC KW - Carbon dioxide evolution KW - Synchrotron radiography KW - In situ study KW - Cross section KW - Through-plane PY - 2009 DO - https://doi.org/10.1016/j.elecom.2009.05.047 SN - 1388-2481 VL - 11 IS - 8 SP - 1559 EP - 1562 PB - Elsevier CY - Amsterdam AN - OPUS4-20577 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER -