2013
DOI: 10.1016/j.fusengdes.2013.01.019
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Development of design Criteria for ITER In-vessel Components

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Cited by 32 publications
(8 citation statements)
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“…The total elongations and fracture strains remain high (⩾10%) after irradiations around ∼2.5-3 dpa, and typically saturate between ∼5%-10% by ∼10-12 dpa (figure 6(b)). From a power-plant design point of view such as the descriptions in ITER structural design criteria for in-vessel components [61,155] or RCC-MRx, plastic flow localisation due to plastic instability in neutron irradiated RAFM steels is related to the loss of UE [156]-which presents the first failure mode, while ductility exhaustion induced local fracture is the second mode of component failure that is linked to the loss of total elongation [61]. The second mode of deformation is typically not a major issue for Gen-I RAFM steels because they retain sufficiently high total elongations (⩾5%, see figure 6(b)), and tensile failures are largely ductile.…”
Section: Low Temperature Hardening-embrittlement (Lthe) In Rafm and O...mentioning
confidence: 99%
“…The total elongations and fracture strains remain high (⩾10%) after irradiations around ∼2.5-3 dpa, and typically saturate between ∼5%-10% by ∼10-12 dpa (figure 6(b)). From a power-plant design point of view such as the descriptions in ITER structural design criteria for in-vessel components [61,155] or RCC-MRx, plastic flow localisation due to plastic instability in neutron irradiated RAFM steels is related to the loss of UE [156]-which presents the first failure mode, while ductility exhaustion induced local fracture is the second mode of component failure that is linked to the loss of total elongation [61]. The second mode of deformation is typically not a major issue for Gen-I RAFM steels because they retain sufficiently high total elongations (⩾5%, see figure 6(b)), and tensile failures are largely ductile.…”
Section: Low Temperature Hardening-embrittlement (Lthe) In Rafm and O...mentioning
confidence: 99%
“…This section will summarize the analysis approach and the obtained results. The structural design criteria, the material allowable and the verification methods used are taken from the SDC-IC Code [5] for assessing the CIT and the RCC-MR, Edition 2007 [6,7], including July 2017 Erratum for the bolts. The main loads acting on the component are (in no particular order): dead weight of the CIT, seismic acceleration forces due to a seismic level 2 earthquake, first plasma disruption generating halo and eddy currents, baking of the VV, plasma operation loads by direct radiative heating and ECRH stray radiation (max.…”
Section: System Load Specifications and Structural Integritymentioning
confidence: 99%
“…Table 2 illustrates the maximal deformation and m (P m is the general primary membrane equivalent stress, P L is the local primary membrane equivalent stress, P b is the primary bending equivalent stress). In a conservative way, the maximum P m is taken as the von Mises stress to calculate the margin [11,12]. However, the maximal deformation, 110.81 mm, is infeasible from the engineering design viewpoint.…”
Section: Design By Analysis Of the Manifold With Current Epsmentioning
confidence: 99%