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Featured researches published by Jan Schulte-Fischedick.


Materials Science and Engineering A-structural Materials Properties Microstructure and Processing | 2002

The morphology of silicon carbide in C/C-SiC composites

Jan Schulte-Fischedick; Achim Zern; Joachim Mayer; M. Rühle; Martin Friess; Walter Krenkel; Richard Kochendörfer

Abstract In the present investigations C/C–SiC has been studied by means of SEM, X-ray diffraction (XRD) and TEM to reveal the morphology of the silicon carbide areas. It was found that there exist two different areas of SiC, a fine grained β-SiC layer with a high amount of stacking faults at the C–SiC interface, and a zone of coarser β-SiC at the SiC–Si interface. From these observations, reaction mechanisms governing the siliconization of porous C/C preforms are proposed. After an initial reaction of carbon with silicon vapour, liquid silicon has to diffuse through the already formed SiC. A violent reaction far away from equilibrium conditions and a high number of nucleation sites leads to the observed formation of a fine grained SiC with a high density of stacking faults. Thermodynamically this is an instable configuration so that the coarser grained zone emerges by solution and precipitation.


Computational Materials Science | 2003

Discrete element simulation of transverse cracking during the pyrolysis of carbon fibre reinforced plastics to carbon/carbon composites

Falk K. Wittel; Jan Schulte-Fischedick; Ferenc Kun; Bernd Kröplin; Martin Frieß

The fracture behavior of fiber-ceramics like C/C-SiC strongly depends on the initial damage arising during the production process. We study the transverse cracking of the 90{\deg} ply in [0/90]S cross-ply laminates due to the thermochemical degradation of the matrix material during the carbonization process by means of a discrete element method. The crack morphology strongly depends on the fiber-matrix interface properties, the transverse ply thickness as well as on the carbonization process itself. To model the 90{\deg} ply a two-dimensional triangular lattice of springs is constructed where nodes of the lattice represent fibers. Springs with random breaking thresholds model the disordered matrix material and interfaces. The spring-lattice is coupled by interface springs to two rigid bars which capture the two 0{\deg} plies or adjacent sublaminates in the model. Molecular dynamics simulation is used to follow the time evolution of the model system. It was found that under gradual heating of the specimen, after some distributed cracking, segmentation cracks occur in the 90{\deg} ply which then develop into a saturated state where the ply cannot support additional load. The dependence of the micro-structure of damage on the ply thickness and on the disorder in spring properties is also studied. Crack density and porosity of the system are monitored as a function of the temperature and compared to an analytic approach and experiments.


ASME 2008 2nd International Conference on Energy Sustainability collocated with the Heat Transfer, Fluids Engineering, and 3rd Energy Nanotechnology Conferences | 2008

CFD Analysis of the Cool Down Behaviour of Molten Salt Thermal Storage Systems

Jan Schulte-Fischedick; Rainer Tamme; Ulf Herrmann

CFD analysis has been conducted to obtain information on heat losses, velocity and temperature distribution of large molten salt Thermal Energy Storage (TES) systems. A two-tank 880 MWh storage system was modeled according to the molten salt TES containment design proposed for the 50 MWel commercial parabolic trough solar thermal power plants in Spain. Heat losses were established using the Finite Element Method (FEM), and used to determine the boundary conditions for the subsequent two- and three-dimensional Computational Fluid Mechanics (CFD) calculations. The investigations reveal that a high heat loss flux occurs at the lower edges of the salt storage tanks (between side wall and bottom plate). Thus the maximum temperature difference can be found at this location, resulting in the onset of local solidification within 3.25 days in the case of the empty cool tank. As a consequence, the detailed design of the lower edge has a large impact on both the overall heat losses and the period until the onset of local solidification.


Applied Thermal Engineering | 2007

An innovative ceramic high temperature plate-fin heat exchanger for EFCC processes

Jan Schulte-Fischedick; Volker Dreißigacker; Rainer Tamme


Materials Science and Engineering A-structural Materials Properties Microstructure and Processing | 2004

Oxidation behaviour of C/C–SiC coated with SiC–B4C–SiC–cordierite oxidation protection system

Jan Schulte-Fischedick; Jens Schmidt; Rainer Tamme; Ulrike Kröner; J. Arnold; B. Zeiffer


Archive | 2004

Plate heat exchanger, process for manufacturing a plate heat exchanger, and ceramic fibre reinforced composite material, more particularly for plate heat exchanger

Ulrike Kröner; Matthias Scheiffele; Jens Schmidt; Jan Schulte-Fischedick; Rainer Tamme


Archive | 2006

Development of C-SiC ceramic compact plate heat exchangers for high temperature heat transfer applications

Per F. Peterson; Haihua Zhao; Fenglei Niu; Wensheng Huang; Jens Schmidt; Jan Schulte-Fischedick


Archive | 2005

Platten-Wärmeübertrager, Verfahren zur Herstellung eines Platten-Wärmeübertragers und keramischer Faserverbundwerkstoff, insbesondere für einen Platten-Wärmeübertrager

Jan Schulte-Fischedick; Jens Schmidt; Rainer Tamme; Ulrike Kröner; Matthias Scheiffele


Materials Science and Engineering A-structural Materials Properties Microstructure and Processing | 2004

Oxidation behaviour of C/CSiC coated with SiCB 4CSiCcordierite oxidation protection system

Jan Schulte-Fischedick; Jonathan M. Schmidt; Rainer Tamme; Ulrike Kröner; Jerimy Arnold; B. Zeiffer


Archive | 1999

Crack Microstructure During the Carbonization of Carbon Fibre Reinforced Plastics to Carbon/Carbon Composites

Jan Schulte-Fischedick; Martin Frieß; Walter Krenkel; Richard Kochendörfer; M. König

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Rainer Tamme

German Aerospace Center

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Jens Schmidt

German Aerospace Center

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B. Zeiffer

German Aerospace Center

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