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1. magnetic confinement - ENEA - Fusione

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98<br />

3. FUSION TECHNOLOGY<br />

3.9 Thermal-Fluidodynamics<br />

2001, the first experimental campaign started on four of the EDA mockups mounted<br />

inside EDA-BETA [3.44, 3.45].<br />

3.9.2 HE-FUS3 experimental cassette of lithium-beryllium pebble<br />

beds<br />

During 2001, a new thermal test campaign was started on the HELICHETTA solidbreeder<br />

mockup. The objective of the tests on a single prismatic cell filled with the<br />

reference breeder Li 4 SiO 4 and Li 2 TiO 3 pebble beds was to determine the influence<br />

of the filling factor on the thermal-mechanical parameters and the behaviour of the<br />

ceramic bed after mechanical pre-cycling and application of the spring-system lateral<br />

load. From July 2001 to the end of the year, 60 tests were carried out in air on the<br />

HEFUS-3 facility at <strong>ENEA</strong> Brasimone on both the reference materials. The measured<br />

Li 4 SiO 4 and Li 2 TiO 3 pebble packing factors were, respectively, 0.65 and 0.64. The<br />

results of the first HELICHETTA test campaigns are:<br />

i) the displacement of the beds is as large as 0.2 mm towards the cooling plates and<br />

ranges from 0.5 to 1 mm for L i 2TiO 3 and up to <strong>1.</strong>5 mm for Li 4 SiO 4 towards the<br />

sliding plug;<br />

ii) the washer springs and sliding plug systems prevent larger stresses on the<br />

containment structure;<br />

iii) the pebble bed thermal conductivities in air show good agreement with previous<br />

FZK experiments;<br />

iv) the pebble thermal mechanical hysteresis, well evident during the cyclic ramp<br />

up/down tests, affects the thermal-mechanical bed behaviour.<br />

The tender for construction of both HELICA and HEXCALIBER was launched in<br />

December 2001 and their fabrication will be finished, respectively, by June 2002 and<br />

December 2002 [3.46, 3.47].<br />

3.10 International Fusion Material<br />

Irradiation Facility (IFMIF)<br />

3.10.1 Design and mockup tests of lithium jet target<br />

One of the main tasks of the lithium target design is to guarantee the jet stability<br />

against overheating by the powerful deuteron beam. This is achieved with the use<br />

of a curved plate (backplate) on which lithium flows. A computer code (RIGEL)<br />

developed ad hoc by <strong>ENEA</strong> Bologna was used to determine the best working<br />

conditions (table 3.V) for the new IFMIF design parameters (Reduced Cost Design).<br />

[3.44] G. Dell’Orco et al.,<br />

Status of the Contracts<br />

EFDA 00/529 and<br />

00/533 for the thermal<br />

fatigue tests of Be<br />

protected EDA – PFW<br />

mock-ups, <strong>ENEA</strong>-EFDA<br />

Meeting (Brasimone<br />

2001)<br />

[3.45] G. Dell’Orco et al.,<br />

Report for the Task<br />

T216+, subtask E1, on the<br />

thermal fatigue tests of<br />

Be protected first wall<br />

mock-ups, <strong>ENEA</strong> Internal<br />

Report, SB-G-R-0051<br />

(2001)<br />

[3.46] G. Dell’Orco et al.,<br />

TAZZA mock-up pebble<br />

beds - Experimental and<br />

theoretical investigations,<br />

presented at the<br />

10th Int. Workshop on<br />

Ceramic Breeder Blanket<br />

Interactions (CCBI-10)<br />

(Karlsruhe 2001)<br />

[3.47] G. Dell’Orco et al.,<br />

Progress on pebble bed<br />

experimental activity for<br />

the HE-FUS3 mock-ups,<br />

presented at the 10th<br />

Int. Workshop on<br />

Ceramic Breeder Blanket<br />

Interactions (CCBI-10)<br />

(Karlsruhe 2001)<br />

Tab 3.V - IFMIF target input data and Li jet stability results<br />

Main input data<br />

r<br />

Main results<br />

Beam footprint 5×20 [cm×cm] Reynolds number 694417 [-]<br />

Jet thickness 0.025 [m] Max. pressure 12493 [Pa]<br />

Jet width 0.26 [m] Max. surface temperature 297 [°C]<br />

Jet velocity 15 [m/s] Max. temperature in the 441 [°C]<br />

bulk<br />

Backplate curvature 0.25 [m] Min. free surface boiling 35 [°C]<br />

radius<br />

margin<br />

Inlet temperature 250 [°C] Min. bulk boiling margin 403 [°C]<br />

Jet power deposition 10 [MW] Free surface evaporation 16 [g/year]

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