The ITER blanket system removes the surface heat flux from the plasma and f
rom bulk heating by the neutrons, reduces the activity in the vacuum vessel
(VV) structural material to the level allowable to ensure vessel reweldabi
lity for the ITER fluence goal and, in combination with the vacuum vessel,
protects the superconducting coils and other ex-vessel components from exce
ssive nuclear heating and radiation damage. The blanket system contributes
with its eddy currents to the passive stabilization of the plasma motion. I
t minimizes the effects of electromagnetic loads on the VV due to plasma di
sruptions, and provides a well defined load path to the VV for net vertical
and horizontal loads arising from vertical displacement events (VDE's). Th
e system is designed to allow the possibility of replacing the shield with
a breeding blanket, within the same dimensional, maintenance, and coolant c
onstraints, to provide the tritium to meet the technical objectives of the
Enhanced Performance Phase.
The basic blanket system concept as well as the arrangement and function of
its components is essentially unchanged from that established in 1995(1).
However, as discussed in this paper, the design of each component has progr
essed significantly as a result of the detail design and technical analysis
efforts of the last two years. The main components of the blanket system a
re:
A back plate: a structure comprising a double wall shell that supports the
first wall/shield modules and routes the coolant water to them.
First wall/shield modules: comprising a plasma facing first wall (FW) secti
on, and a shielding (or later breeding) section. Primary wall and baffle mo
dules are distinguishable by the function of their FW.
Limiters: define the plasma boundary during plasma start-up and shutdown an
d are located in equatorial ports.
Flexible connectors, electrical straps, and branch pipes: the remote handli
ng compatible structural, electrical, and cooling connections between the m
odules and back plate.
Filler shields: shielding permanently mounted to the back plate in the tria
ngular gaps between FW/shield modules.
The system will use austenitic stainless steel 316L(N)-IG (ITER Grade) as t
he primary structural material cooled by water with inlet conditions of 3.8
MPa and 140 degrees C. The plasma facing surface of the FW will be berylli
um except the lower region of the baffles, where tungsten is used. The elec
trical straps and heat sink layer in the FW will be copper alloy. A titaniu
m alloy is the prime candidate material for the flexible connectors.