1. magnetic confinement - ENEA - Fusione
1. magnetic confinement - ENEA - Fusione
1. magnetic confinement - ENEA - Fusione
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3. FUSION TECHNOLOGY 67<br />
3.2 First Wall and Divertor<br />
5 mm<br />
Fig. 3.3 - Temperature distribution for RAE=10 MeV for 0.1s.<br />
Fig. 3.2 - Normalised<br />
energy density (GeV/cm 3 )<br />
deposited by 10-MeV<br />
RAE.<br />
On the basis of the FLUKA outputs, the temperature pattern inside<br />
the first-wall structures was defined with the use of the finiteelement<br />
heat-conduction code ANSYS. The RAE energy deposition<br />
density was assumed to be 50 MJ/m2, and both 10- and 100-µs<br />
deposition times were considered. The temperature pattern just after<br />
the RAE energy deposition, for an electron energy of 10 MeV and<br />
energy deposition time of 0.1 s, is shown in figure 3.3 for geometry<br />
1). The amount of armour material exceeding the melting<br />
temperature is shaded grey in the figure.<br />
The analysis demonstrated that for all the options but the Be flat-tile port limiter, the<br />
heatsink and the cooling tube beneath the armour are well protected for both the<br />
RAE energies and both the energy deposition times. However, there is a high degree<br />
of melting (ablation) of the W (Be) surface layers, which would eventually affect the<br />
PFC lifetime. As for the primary first wall with CFC poloidal limiters, the limiters<br />
suffer severe ablation, the heat loads being six times larger than those in toroidally<br />
uniform structures. As much as 15 mm of carbon per pulse is removed from the<br />
limiter heads.<br />
3.3 Vacuum Vessel and Shield<br />
3.3.<strong>1.</strong> EM analyses of in-vessel components for ITER-FEAT<br />
[3.3] EFDA Contract 00-<br />
544, Design of the plasma<br />
facing component (PFC)<br />
for the divertor of ITER-<br />
FEAT (2000)<br />
[3.4] EFDA Contract 00-<br />
570, EM analyses of<br />
shielding blanket for<br />
ITER-FEAT design<br />
options, during plasma<br />
disruptions (2000)<br />
In ITER, the electro<strong>magnetic</strong> (EM) loads driven by plasma disruptions are one of the<br />
most problematic issues for the in-vessel engineering. Considerable effort has been<br />
spent on design analysis and R&D to obtain in-vessel components capable of<br />
withstanding the EM loads induced by plasma disruptions. During 2001, extensive,<br />
very detailed EM analyses were performed in support of this issue. For the support<br />
to be really effective, the analyses had to have competing objectives: very accurate<br />
component modelling, precision in describing the EM transient and, due to the very<br />
large number of cases to be treated, very short computing time. The objectives were<br />
achieved with the use of the zooming procedure developed at <strong>ENEA</strong>, which made it<br />
possible to run the number of cases needed to select, for each component, the design<br />
option with the best performance [3.3, 3.4].<br />
The EM loads induced by the ITER reference plasma disruptions were evaluated for<br />
the following in-vessel components: divertor, ICRH assembly, equatorial port limiter