Conceptual design of the LHCD system on CFETR
1An overall engineering design of the LHCD system on CFETR, including the neutronics analysis and the discussion on the maintenance scheme, is presented.2The LH launchers located at high filed side and low field side are compared in both physics and engineering aspects.3The major challenges in reali...
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Veröffentlicht in: | Fusion engineering and design 2023-04, Vol.189 (6), p.113444, Article 113444 |
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Sprache: | eng |
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Zusammenfassung: | 1An overall engineering design of the LHCD system on CFETR, including the neutronics analysis and the discussion on the maintenance scheme, is presented.2The LH launchers located at high filed side and low field side are compared in both physics and engineering aspects.3The major challenges in realizing this system are discussed.
With the capability of saving flux consumption in the current ramp up phase, controlling the safety factor (q) profile, providing the required off-axis current drive (CD), a lower hybrid current drive (LHCD) system was eventually determined to be used on the China Fusion Engineering Test Reactor (CFETR). In this paper, a 20 MW/4.6 GHz system composed of 40 units of 500 kW continuous wave (CW) klystron amplifier is preliminarily designed. The feasibility of the frequency choice of 4.6 GHz in the physical aspect is discussed. In order to minimize the transmission loss, a TE01 over-mode of circular waveguide will be used in the transmission system. Although previous calculations indicates that high field side (HFS) launcher location results in waves damping at inner region than low field side (LFS) launcher, which is favorable for plasma stability, HFS launcher will be extremely difficult in engineering due to the limited space. Calculations show that the tritium breeding ratio (TBR) will be decreased by ∼ 1.5% with HFS launcher, while it will be decreased by ∼ 0.22% only with LFS launcher. As a result, the LH power will be coupled to plasma from the top port at LFS. The designed passive active multi-junction (PAM) launcher is arranged in an array of 5 rows and 8 columns with the height of 1181 mm and the width of 794 mm. A shielding block with a thickness of 20 cm will be equipped around the feeding waveguides to protect the feeding waveguides and to prevent neutron leakage. A preliminary scheme of the remote maintenance for the LFS launcher is given. The modeling results shows that the density for optimum coupling is ∼ 1.8 × 1017/m³, lower than the 4.6 GHz cut-off density ne_co = 2.6 × 1017/m³. Around this density, the power directivity (Dp) can be high as 71%. |
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ISSN: | 0920-3796 1873-7196 |
DOI: | 10.1016/j.fusengdes.2023.113444 |