12.07.2015 Views

16.2 - Severe Accident Analysis (RRC-B) - EDF Hinkley Point

16.2 - Severe Accident Analysis (RRC-B) - EDF Hinkley Point

16.2 - Severe Accident Analysis (RRC-B) - EDF Hinkley Point

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

SUB-CHAPTER : <strong>16.2</strong>PRE-CONSTRUCTION SAFETY REPORTCHAPTER 16: RISK REDUCTION AND SEVEREACCIDENT ANALYSESPAGE : 102 / 295Document ID.No.UKEPR-0002-162 Issue 04deflagration of hydrogen. A maximum size of this region of 20,000 m 3 is found for two scenarios:7.5 cm (46 cm 2 ) SB(LOCA) at the top of the pressuriser with fast secondary cooldown, and 5 cm(20 cm 2 ) SB(LOCA) in the cold leg with fast secondary cooldown and re-flood. For bothscenarios the combustion process is analysed with COM3D (see section 2.3.3 of this subchapter).Generally, the maximum size of the region with 13% hydrogen by volume is reachedsoon after hydrogen release starts, when the gas distribution is still quite inhomogeneous, andlong before the end of release, when the size of the region with 4% by volume reaches itsmaximum. These values are also indicated in Sub-section <strong>16.2</strong>.2.3 - Table 2.In this discussion, SB(LOCA) type scenarios are selected because of the low steam content inthe containment. This property results in an aggravated hydrogen combustion risk compared toLB(LOCA) scenarios for example, where the high steam concentration yields significantly moreinert containment conditions. In addition, probabilistic studies show that SB(LOCA) scenariosare much more likely severe accident scenarios than LB(LOCA) scenarios.2.3.2.3. AICC and Expected Combustion PressureHydrogen combustion can proceed in different modes. For hydrogen concentrations belowabout 10% by volume, the flame speed is expected to be subsonic, i.e. no shock waves occur.The maximum possible peak pressure from such a combustion is given by the AICC pressure.However, this pressure cannot be reached in a realistic containment for the following reasons:• As the flame velocity is low, heat is efficiently transferred to structures, inert gasessuch as steam, and also to droplets. This is a departure from the adiabaticcondition.• If hydrogen concentration is below 8% by volume, combustion is not complete. Alsothe complex structure of the large containment leads to incomplete combustion incase of a deflagration. This is a departure from the completeness condition.Therefore, examples of both AICC pressure and laminar combustion pressures calculated withGASFLOW are presented. Laminar combustion leads to a quasi-static pressure increase, whichmeans that the pressure rise is isotropic and steady.Four representative scenarios have been analysed with respect to AICC pressure history [Ref]:• 5 cm (20 cm 2 ) SB(LOCA) in the cold leg with fast secondary cooldown (f.s.c.),• 5 cm (20 cm 2 ) SB(LOCA) in the hot leg with fast secondary cooldown (f.s.c.),• 7.5 cm (46 cm 2 ) SB(LOCA) at the top of the pressuriser with fast secondarycooldown (f.s.c.),• 5 cm (20 cm 2 ) (SB)LOCA in the cold leg with only partial cooldown (p.c.; withconsideration of ex-vessel hydrogen).In addition, as another severe accident test case a LOOP scenario with loss of all dieselgenerators, which yields a higher steam concentration in the containment than a SB(LOCA) typescenario, has also been analysed with GASFLOW. However, for these scenarios withdepressurisation at a core outlet temperature of 650°C, it has been found that steamconcentration is sufficiently high so that no global combustion can occur [Ref].In addition, two bounding scenarios have been analysed [Ref]:

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!