Effects of process parameters on structure and properties of copper-titanium carbide: C.Sauer et al. (Dresden University of Technology, Dresden, Germany.)

Abstract

Heat load tests are performed on actively cooled graphite/stainless steel laminated structures, for the simulation of steady-state first wall operations in nuclear fusion reactors. Graphite armor tiles (40 mm × 40 mm × 10 mm) are brazed to stainless steel substrates (1 mm thick, 68 mm diameter) with the insertion of copper-carbon fiber composite (Cu-C) compliant layers (1.7 mm thick). Ag-28 wt%Cu-5wt%Ti solder and Ag-28wt%Cu solder are used for brazing the graphite/ Cu-C interface and Cu-C/stainless steel interface, respectively. Fine grain isotropic graphite and carbon fiber felt reinforced carbon composite (felt C-C) are chosen for armor tile materials. Thermal conductivities of these graphite materials, being measured through a laser flashing method, are 109 and 170 W/mK at room temperature, respectively.Heat load tests are carried out by using a 40 kW DC power source (maximum current: 1000 A). Pulsed thermal loads at heat fluxes ranging from 1 to 6 MW/m2 are realized either through resistance heating of a carbon felt heater on test specimens (1–4 MW/m2) or through electric arcing between a cathode graphite rod and graphite tiles of test specimens (> 4 MW/m2).Surface temperatures of graphite tiles are found to reach equilibrium temperatures at around 20 s after the start of heating. The equilibrium temperatures are higher by 30–40% for isotropic graphite tiles as compared to felt C-C tiles: 1800 °C for isotropic graphite and 1300 °C for felt C-C, at 6 MW/m2. The equilibrium temperature at the Cu-C layer for a 6 MW/m2 heat flux is measured to be around 600 °C.