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Commissioning result of the KSTAR in-vessel cryo-pump

  • Chang, Y.B. (National Fusion Research Institute) ;
  • Lee, H.J. (National Fusion Research Institute) ;
  • Park, Y.M. (National Fusion Research Institute) ;
  • Lee, Y.J. (National Fusion Research Institute) ;
  • Kwag, S.W. (National Fusion Research Institute) ;
  • Song, N.H. (National Fusion Research Institute) ;
  • Park, D.S. (National Fusion Research Institute) ;
  • Joo, J.J. (National Fusion Research Institute) ;
  • Moon, K.M. (National Fusion Research Institute) ;
  • Kim, N.W. (National Fusion Research Institute) ;
  • Yang, H.L. (National Fusion Research Institute) ;
  • Oh, Y.K. (National Fusion Research Institute)
  • Published : 2013.12.31

Abstract

KSTAR in-vessel cryo-pump has been installed in the vacuum vessel top and bottom side with up-down symmetry for the better plasma density control in the D-shape H-mode. The cryogenic helium lines of the in-vessel cryo-pump are located at the vertical positions from the vacuum vessel torus center 2,000 mm. The inductive electrical potential has been optimized to reduce risk of electrical breakdown during plasma disruption. In-vessel cryo-pump consists of three parts of coaxial circular shape components; cryo-panel, thermal shield and particle shield. The cryo-panel is cooled down to below 4.5 K. The cryo-panel and thermal shields were made by Inconel 625 tube for higher mechanical strength. The thermal shields and their cooling tubes were annealed in air environment to improve the thermal radiation emissivity on the surface. Surface of cryo-panel was electro-polished to minimize the thermal radiation heat load. The in-vessel cryo-pump was pre-assembled on a test bed in 180 degree segment base. The leak test was carried out after the thermal shock between room temperature to $LN_2$ one before installing them into vacuum vessel. Two segments were welded together in the vacuum vessel and final leak test was performed after the thermal shock. Commissioning of the in-vessel cryo-pump was carried out using a temporary liquid helium supply system.

Keywords

References

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