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IPP Annual Report 2007 - Max-Planck-Institut für Plasmaphysik ...

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and distributes them via CVD-diamond vacuum barrier windows<br />

to individually movable antennas (launchers) in the<br />

W7-X torus. Two symmetrically arranged MBWGs are used<br />

to transmit the power of all gyrotrons. In <strong>2007</strong>, a major work<br />

package was the design completion and manufacturing of<br />

the transmission system near the torus. This comprises the<br />

reflectors type M13 and M14, which will be installed in two<br />

“towers” in front of the W7-X ports.<br />

The fabrication of both towers was finished, and the installation<br />

of control systems for reflectors and launchers, support<br />

structures, and granite absorbing plates has started.<br />

Both towers, one of them is seen in figure 28, have to be<br />

stored until W7-X assembly is completed and access is provided<br />

for the installation at their final position in the torus<br />

hall. In the meantime, retro-reflectors were mounted in the<br />

beam-duct in the image plane at half distance of the MBWG<br />

transmission line. Full distance transmission can be simulated<br />

and tested by this arrangement. First calorimetric high<br />

power measurements of the two-pass transmission efficiency<br />

of the first part of the MBWG were performed, yielding a<br />

loss of about 3 % for 10 reflections on the 2×3 MBWG-mirrors<br />

and the 4 additional guiding mirrors, which is in good<br />

agreement with calculations and low power measurements.<br />

This result confirmes the high quality of the quasi-optical<br />

concept for high power, long distance and low loss microwave<br />

transmission.<br />

8.1.4 In-vessel-components (<strong>IPP</strong>)<br />

The design of the front steering ECRH-antennas in the Aand<br />

E-type ports is compatible with full power cw requirements<br />

and was finished in <strong>2007</strong>. The CAD-drawing is<br />

shown in figure 29. Most of the antenna components are<br />

already manufactured, the assembly has started.<br />

Figure 29: ECRH front steering antenna with bi-axially and individually<br />

movable front mirrors<br />

For the two optional high-field side launchers to be installed<br />

in the narrow N-ports, it was decided to adopt the<br />

remote steering scheme, which is based on the imaging<br />

Wendelstein 7-X<br />

57<br />

properties of a square corrugated waveguide. A movable<br />

reflector at the waveguide entrance controls the direction of<br />

the beam injected into the waveguide; at the exit of the<br />

waveguide near to the plasma edge, the beam is launched at<br />

the same angle. For the N-ports, a solution with a bent<br />

waveguide was chosen. This eases the integration of the<br />

waveguides and leads to a lower antenna beam divergence<br />

due to increased waveguide cross-section, but requires<br />

thorough optimization of the position of the mitre bend and<br />

the vacuum valve in the waveguide. The conceptual design,<br />

as well as first optimization calculations have been started.<br />

The ECRH operation range can be strongly extended if<br />

heating scenarios with the second harmonic ordinary mode<br />

(O2) and the third harmonic extraordinary mode (X3) can<br />

be applied. The first enables high plasma density, which is<br />

necessary for efficient divertor operation, the second allows<br />

operation at a lower magnetic field. An incomplete single<br />

pass absorption in the range of 40 % to 80 % has to be<br />

accepted for W7-X parameters. Specially shaped reflectors<br />

made from TZM (titanium, zirconium, molybdenum alloy)<br />

will be installed to avoid the thermal overload of the high<br />

field side heat shield by the microwave shine-through.<br />

After first preliminary high power test in 2006 the reflectortile<br />

was redesigned and its surface was polished to reduce<br />

losses. The watercooled reflector tile was retested in the<br />

ECRH-installation at Greifswald with about 0.5 MW incident<br />

power, which is the expected “worst case” loading for<br />

W7-X. The calorimetrically measured absorption reached<br />

values of 0.3 %, which is consistent with the theoretical<br />

value deduced from the material properties and with previous<br />

low power tests. The surface temperature reaches<br />

470 °C and 390 °C are measured at the cooling plate,<br />

respectively, after 200 s for the worst case, which is acceptable.<br />

The knowledge of the beam position and power load<br />

at the reflector tiles is essential for reliable X3- and O2operation.<br />

An array of small pick-up holes will therefore be<br />

integrated into the tiles to measure the exact beam position<br />

and the single pass absorption. The microwave signal is<br />

transferred by 4 mm copper waveguides towards the B-type<br />

port in the W7-X vacuum vessel. The positions of the<br />

120 pick-up horns and the routing of the related waveguides<br />

were defined in close cooperation with the W7-X<br />

KIP group.<br />

8.1.5 Advanced components and ITER-related R&D<br />

8.1.5.1 Improved e-beam power dissipation at the Gyrotron<br />

collector<br />

The peak power load of the electron beam at the gyrotron<br />

collector is a limiting factor for the next generation cw high<br />

power gyrotrons with 1.5-2 MW output power. The W7-X<br />

Gyrotrons are equipped with a conventional vertical sweep<br />

coil system, which moves the electron beam intersection with<br />

the collector surface up and down in the vertical direction.

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