“…It is completed, for some ITER specific aspects by ITER structural design criteria for in-vessel components (SDC-IC). In this work [5,6] the reference load cases and the related rules for the assessment were defined, identifying at the same time the missing rules and the lack of characterization for the TBM EUROFER structural material. Three different loading conditions (LC) have been studied; the first one corresponds to normal operation during a typical D-T phase plasma pulse (LC1), the second to the typical power excursion occurring during a MARFE event (LC2) and the third one corresponds to the accidental pressurization of the box in case of internal LOCA (LC3).…”
“…It is completed, for some ITER specific aspects by ITER structural design criteria for in-vessel components (SDC-IC). In this work [5,6] the reference load cases and the related rules for the assessment were defined, identifying at the same time the missing rules and the lack of characterization for the TBM EUROFER structural material. Three different loading conditions (LC) have been studied; the first one corresponds to normal operation during a typical D-T phase plasma pulse (LC1), the second to the typical power excursion occurring during a MARFE event (LC2) and the third one corresponds to the accidental pressurization of the box in case of internal LOCA (LC3).…”
“…A correct evaluation of HTC in the manifold stages is important for the correct assessment of the TBM box structural behaviour. In the current design the rear region of the TBM box features high stresses [8] but secondary stress underestimation could be induced by implementing HTC values too far from the real ones. In the TBM design cycle with a simplified assumption (based on the Gnielinsky correlation) a constant HTC of 2000 W/m 2 K has been considered in the MF stages.…”
Section: Thermal Analyses Of the Manifold Stagesmentioning
confidence: 98%
“…The HCPB TBM design has been extensively described in [7][8][9]. The HCPB TBM features a box structure (EUROFER as structural material): the U shaped FW is closed along the poloidal direction by the lateral Caps; an internal structure of horizontal and vertical Stiffening Grids (hSG and vSG, addressed as sub-components together with the Caps) defines the volume allocation for the Breeder Units (BUs).…”
Section: Hcpb Tbm Design Descriptionmentioning
confidence: 99%
“…starting from the preliminary design and neutronic analyses till the detailed fluid dynamic, thermal and structural analyses [7,8]. In the design assessment phase a fundamental role is played by the fluid dynamic analyses of the TBM sub-components and of the manifolds (MF) stages.…”
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