1. magnetic confinement - ENEA - Fusione
1. magnetic confinement - ENEA - Fusione
1. magnetic confinement - ENEA - Fusione
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28<br />
<strong>1.</strong> MAGNETIC CONFINEMENT<br />
<strong>1.</strong>2 FTU Facilities<br />
Table <strong>1.</strong>II Machine efficiency in 2001<br />
January February March April May June July September October November December<br />
Total pulses 111 180 238 352 406 92 130 141 265 202<br />
Successful pulses (sp) 103 159 214 312 375 80 116 138 239 173<br />
I(sp) 0.93 0.88 0.90 0.89 0.92 0.87 0.89 0.98 0.90 0.86<br />
Total<br />
2117<br />
1909<br />
0.90<br />
Potential experimental days 10 9.5 11 18 17 4 5 7 12.1 10<br />
Real experimental days 5 8 10 14 17 4 5 7 12.1 9<br />
I(ed) 0.50 0.84 0.91 0.78 <strong>1.</strong>00 <strong>1.</strong>00 <strong>1.</strong>00 <strong>1.</strong>00 <strong>1.</strong>00 0.90<br />
104<br />
91<br />
0.88<br />
Experimental minutes 1819 2879 3971 6023 7640 1803 2165 2561 4845 3867<br />
Delay minutes 1323 1925 2402 2403 2801 621 640 1622 2672 1958<br />
I(et) 0.58 0.60 0.62 0.71 0.73 0.74 0.77 0.61 0.64 0.66<br />
A(sp/d) 20.60 19.88 2<strong>1.</strong>40 22.29 22.06 20.00 23.20 19.71 19.75 19.22<br />
A(p/d) 22.20 22.50 23.80 25.14 23.88 23.00 26.00 20.14 2<strong>1.</strong>90 22.44<br />
37573<br />
18367<br />
0.67<br />
20.95<br />
23.24<br />
DELAY FOR SYSTEM (minutes)<br />
January February March April May June July September October November December Total %<br />
MACHINE 0 43 466 52 159 193 29 19 140 228 274 1603 8.7<br />
POWER SUPPLIES 0 192 528 894 310 239 22 31 287 10 279 2792 15.2<br />
RADIO FREQUENCY 0 81 59 280 697 738 188 112 247 221 53 2676 14.6<br />
CONTROL SYSTEM (PROMETEO) 0 347 235 319 232 402 223 24 19 344 287 2432 13.2<br />
DAS 0 0 0 172 44 92 7 4 52 63 54 488 2.7<br />
FEEDBACK 0 20 0 0 22 0 0 17 27 24 10 120 0.7<br />
NETWORK 0 143 208 92 0 0 0 0 0 461 84 988 5.4<br />
DIAGNOSTIC SYSTEMS 0 213 219 85 179 276 17 166 89 133 150 1527 8.3<br />
ANALYSIS 0 279 209 350 634 785 135 265 735 1009 734 5135 27.9<br />
OTHERS 0 5 17 158 126 76 0 2 26 179 33 622 3.4<br />
TOTALE 0 1323 1941 2402 2403 2801 621 640 1622 2672 1958 18383 100<br />
Summary of machine maintenance<br />
Maintenance of the FTU system was carried out according to schedule. Visual<br />
inspection of the vacuum vessel revealed ten displaced tiles, most of which in the<br />
upper and bottom rows. The rupture was investigated through specific laboratory<br />
tests and it was found that the fragility of tungsten-zirconium-molybdenum (TZM)<br />
can damage the supporting-screw thread. A new design tile-support structure was<br />
developed and will be tested in 2002.<br />
The new data storage system based on SAN architecture was released, and the whole<br />
FTU experimental data archive is on line. A preliminary test of Opto22 technology in<br />
slow acquisition, i.e., replacing the traditional PLC, was carried out.<br />
Future activities<br />
In 2002 the machine will operate up to July and then from mid-September to mid-<br />
October if the injector for launching pellets from the high-field side is ready. New<br />
diagnostics and the new passive-active multijunction (PAM) lower hybrid launcher<br />
will be installed during the second shutdown in 2002. All four ECRH gyrotrons will<br />
be in operation, so a total power of <strong>1.</strong>6 MW should be available. A new density<br />
feedback system based on VME architecture will be implemented.<br />
Boronisation system<br />
Direct current glow discharge deposition is used to coat the vacuum vessel walls<br />
with a boron film. The deposition system is the same as that used for the vacuum<br />
chamber conditioning, but the vessel is fuelled with a mixture of helium and<br />
diborane (90% He and 10% B 2 H 6 ). The aim of boronisation is to reduce the effective<br />
charge Z eff and the plasma radiation losses by introducing a low-Z element as firstwall<br />
material.