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Status of safety analysis for HCPB TBM Susana Reyes TBM Project meeting, UCLA, Los Angeles, CA May 10-11, 2006 Work performed under the auspices of the U. S. Department of Energy by Lawrence Livermore National Laboratory under Contract W-7405-Eng-48.
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2 SR—5/11/06 Outline Background Objectives Status of safety analysis –Source terms (radioactive, energy) –Decay heat removal –Ex-vessel LOCA analysis Summary and plan
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3 SR—5/11/06 Background Each TBM contains radioactivity and energy source terms that must be identified –Radioactive source terms: tritium, activated components and materials –Energy source term: chemical, decay heat, enthalpy Two steps must be completed as part of the TBM licensing process: –ITER Report on Preliminary Safety (RPrS), and associated documents (beg 2008) –Final Safety Report (by 2016) Work now is focussed on updating DDD safety section, input from DDD will be used for the ITER RPrS –July 2006: initial DDD safety sections, including operational releases, radioactive inventories, decay heat, chemical sources, WDR –December 2006: final DDD safety sections, including specific accident scenarios –December 2006 to July 2007: ITER will select enveloping TBM results per category to include in the RPrS (not all TBM results will be included)
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4 SR—5/11/06 It is likely that full blown accident analysis will not be necessary for US HCPB TBM as long as it is similar to JA or EU concepts Need to demonstrate that accident source term (radioactive inventories, chemical energy and enthalpy) in US TBM are similar or smaller than those in JA and EU HCPB TBM Objectives of preliminary safety analysis: –address source terms (energy sources, activation products), decay heat and WDRs –demonstrate that the change in geometry in US TBM concept does not affect the decay heat removal capability of TBM –analyze thermal response of the module to an ex-vessel LOCA Objectives
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5 SR—5/11/06 New US HCPB TBM dimensions (1/3 of half-port submodule) Started to update safety analyses using new configuration Status of safety analysis for US HCPB submodule 1/4 port submodule (91cmx73cmx60cm) 1/3 of half port submodule (71cmx38.9cmx60cm)
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6 SR—5/11/06 Source terms in US HCPB TBM Material source term
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7 SR—5/11/06 Activation calculations needed to determine radioactive source term Do not have full neutronics analysis for US HCPB TBM, it would take a few weeks to set up 3-D neutronics Monte Carlo model FW neutron flux for ¼ port submodule is known (M. Youssef, 4/05) and used to calculate new submodule FW activation ACAB calculation using 41494 pulses of 400 s on, 1800 s cooling (to reach 0.3 MWa/m2 at average ITER NWL=0.57 MW/m2) –at shutdown Fe-55, Mn-56, Mn-54, Cr-51 and W-185, sum up 85% of the total 5.9x10 4 Ci (DCLL TBM is 7.65x10 4 Ci) –inventories for rest of HCPB submodule should be bounded by EU and JA TBMs –preliminary WDR estimation using FW neutron flux for all the components shows WDR acceptable
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8 SR—5/11/06 Activation calculations: decay heat Results from FW activation show that decay heat is less than that calculated for EU and JA HCPB TBMs, it can be anticipated that decay heat removal is not a concern for US HCPB submodule For a detailed decay heat removal calculation need to have neutron fluxes for all components (need neutronics calculation) JA HCPB TBMUS HCPB TBM
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9 SR—5/11/06 Assumed parallel configuration, surface heat flux = 0.5 MW/m 2 Used nuclear heating from previous TBM design and scaled for actual configuration (M. Youssef, et al., Fusion Eng. and Design 81, 2006) Ex-vessel He LOCA at power, 2 scenarios considered: –Plasma shutdown occurs when Be armor melts (~1250 C) –Active plasma shutdown at t =100 s Ex-vessel LOCA analysis Manifold FW Be multiplier Cooling plates Breeder channels CHEMCON 1-D heat transfer model
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10 SR—5/11/06 Be temperatures in front portion of the bed is well above 800 °C (reaction rates high and access O 2 should be avoided) FW temperatures above 900 °C, material has practically no rigidity and we must assume FW failure It is proposed here to introduce an active system for plasma shut down at t=100 s FW front reaches high temperatures but the rear <800 °C, as the mechanical load is small rupture of the first wall is inhibited Ex-vessel LOCA analysis: results Temperature evolution during ex- vessel LOCA, no plasma shutdown Temperature evolution during ex-vessel LOCA, plasma shutdown at t=100 s
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11 SR—5/11/06 Summary and plan Preliminary safety analysis initiated for US HCPB TBM Demonstrated that accident source term (radioactive inventories, chemical energy and enthalpy) in US TBM is smaller than JA and EU HCPB TBM Full blown accident analysis will probably not be necessary for US HCPB TBM, however: –need detailed neutronics analysis for US HCPB TBM –need detailed activation analysis for decay heat and radioactive inventory/waste assessments –other accident scenarios (in-vessel LOCA, in TBM-box LOCA)? Need to address tritium inventories and releases Still need to address the impact of the edge-on configuration on safety analyses
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12 SR—5/11/06 Comparison to EU and JA ex-vessel LOCA results EU HCPB TBM JA HCPB TBM US HCPB TBM
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