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Determination of the temperature of the graphite probe surface in graphite probe furnace atomic absorption spectrometry
Institution:1. Oak Ridge National Laboratory, Oak Ridge, TN, 37830, USA;2. Nuclear Graphite Research Group, Department of Mechanical, Aerospace and Civil Engineering, The University of Manchester, M13 9PL, United Kingdom;3. Ludwig-Maximilians-Universität München (LMU Munich) Department of Chemistry and Center for NanoScience Butenandtstrasse 5–13 (E) 81377 Munich;4. Canadian Nuclear Laboratories, Chalk River, Ontario, Canada, K0J 1J0;5. USNC, 2288 W Commodore Way Suite 300, Seattle, WA 98199;6. Photon Science Institute, Department of Materials, The University of Manchester, M13 9PL, United Kingdom
Abstract:An apparatus for determining the temperature of a graphite probe in graphite probe furnace atomic absorption spectrometry has been developed and tested. By measuring the change in the reflection of a laser beam from various pure metals which are deposited on the probe surface at the usual location for sample deposition, it has been found that the heating of the graphite probe surface occurs in two stages. When the probe is inserted into a pulse-heated, commercial graphite furnace after it has been heated to a steady-state temperature, the probe surface is initially rapidly heated by the radiation from the heated graphite tube wall, and thereafter the probe maintains that steady-state temperature for a short time. For a given graphite probe, the heating rate at the initial stage and the corresponding steady-state temperature at the final stage are mainly determined by the final tube wall temperature; the steady-state temperature of the probe is considerably lower than the final tube wall temperature because of thermal conduction by the probe to that part of its body which is lying outside the tube wall. The higher the final tube wall temperature, the higher is the heating rate of the probe at the initial stage, the higher is its steady-state temperature at the final stage, and the less is the difference between the final tube wall temperature and the steady-state temperature of the probe surface. The heating rate of the probe surface at 1600 K is 180 K s?1, whereas at 2300 K it is 3600 K s?1; the differences between the probe surface and tube wall temperatures at the former temperature is 700 K, whereas at the latter temperature it is 250 K.
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