1 / 41

Dr. Robert C. Nelson 1 , J. Charles McKibben 2 , Dr. Kiratadas Kutikkad 2 , and Leslie P. Foyto 2

Thermal-Hydraulic Transient Analysis of the Missouri University Research Reactor (MURR) TRTR Annual Meeting September 17-20, 2007. Dr. Robert C. Nelson 1 , J. Charles McKibben 2 , Dr. Kiratadas Kutikkad 2 , and Leslie P. Foyto 2 1 RRSAS 2 MURR. Introduction.

kharbin
Download Presentation

Dr. Robert C. Nelson 1 , J. Charles McKibben 2 , Dr. Kiratadas Kutikkad 2 , and Leslie P. Foyto 2

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Thermal-Hydraulic Transient Analysis of the Missouri University Research Reactor (MURR)TRTR Annual MeetingSeptember 17-20, 2007 Dr. Robert C. Nelson1, J. Charles McKibben2, Dr. Kiratadas Kutikkad2, and Leslie P. Foyto2 1 RRSAS 2 MURR

  2. Introduction • Potential for fuel damage has been evaluated for various accidents and transients postulated for the MURR. • Criterion for ‘no fuel damage’ is that fuel plate peak temperatures do not approach the minimum fuel plate blister temperature of 900 °F (484 °C). • Model includes full core – 8 fuel elements; each with all 24 fuel plates and 25 coolant channels. • The model developed and analyses for the LOCA and LOF transients will be discussed.

  3. MURR Model • Fuel region is cooled by a pressurized primary coolant system. • Pool coolant system is separate from primary coolant system. • Pressurized primary coolant system is located in the reactor pool allowing direct heat transfer during normal operation and a transition to natural convection under accident conditions. • Reflector region, control blade region, and center test hole are cooled by pool water (forced flow transitioning to natural convection).

  4. Detailed RELAP5 Model of the MURR Primary Coolant Loop

  5. Detailed RELAP5 Model of the MURR Bulk Reactor Pool and Pool Coolant Loop

  6. MURR 24 Plate Core Model

  7. Fuel Plate Power Distribution

  8. Calculated Accidents • Loss of Primary Coolant • Cold Leg • Hot Leg • Loss of Primary Flow

  9. Loss of Coolant Accident (LOCA) • Historically the most serious accident considered. • Initiated in theory by the double-ended rupture in a section of main coolant piping. • Mitigated by use of engineered Safety Features (ESF) – Anti-Siphon System. • These features are demonstrated in the following schematic of the in-pool portion of the primary coolant system.

  10. PT 943 PS 938 V527C

  11. Top Level LOCA Results • Peak Steady State Temperature – 272.1 °F (133.4 °C) [centerline of plate number-1] • Hot Leg Break – 282.1 °F (138.4 °C) [centerline of plate number-1 at 0.2 seconds] • Cold Leg Break – 311.7 °F (155.4 °C) [centerline of plate number-3 at 0.5 seconds] • No challenge to fuel plate blister temperature of 900 °F (482 °C) NORMAL REACTOR OPERATING CONDITIONS AND CONSERVATIVE ASSUMPTIONS WHEN THE LOCA INITIATES 1 Pressure above atmosphere

  12. Cold Leg LOCA

  13. Junction Flow Rates During The First 20 Seconds of the Cold Leg LOCA

  14. Coolant Flow Through the 25 Individual Channels During the First 20 Seconds of the Cold Leg LOCA

  15. Centerline Temperature of the 24 Fuel Plates (Section 4) During the First 20 Seconds of the Cold Line LOCA

  16. Liquid Fraction of the 25 Individual Coolant Channels (Volume 1) During the First 600 Seconds of the Cold Leg LOCA

  17. Liquid Fraction of the 25 Individual Coolant Channels (Volume 2) During the First 600 Seconds of the Cold Leg LOCA

  18. Liquid Fraction of the 25 Individual Coolant Channels (Volume 3) During the First 600 Seconds of the Cold Leg LOCA

  19. Liquid Fraction of the 25 Individual Coolant Channels (Volume 4) During the First 600 Seconds of the Cold Leg LOCA

  20. Centerline Temperature of the 24 Fuel Plates (Section 1) During the First 20 Seconds of the Cold Leg LOCA

  21. Centerline Temperature of the 24 Fuel Plates (Section 2) During the First 20 Seconds of the Cold Leg LOCA

  22. Centerline Temperature of the 24 Fuel Plates (Section 3) During the First 20 Seconds of the Cold Leg LOCA

  23. Temperature of the 25 Individual Coolant Channels (Volume 1) During the First 20 Seconds of the Cold Leg LOCA

  24. Temperature of the 25 Individual Coolant Channels (Volume 4) During the First 20 Seconds of the Cold Leg LOCA

  25. Coolant Flow Through the 25 Individual Channels During the First 20 Seconds of the Cold Leg LOCA

  26. Volume Pressures During the First 20 Seconds of the Cold Leg LOCA

  27. Hot Leg LOCA

  28. Centerline Temperature of the 24 Fuel Plates (Section 3) During the First 40 Seconds of the Hot Leg LOCA

  29. Temperature of the 25 Individual Coolant Channels (Volume 1) During the First 200 Seconds of the Hot Leg LOCA

  30. Cold Leg LOCA Channel Temperatures (Volume 1)

  31. Hot Leg LOCA Channel Temperatures (Volume 1)

  32. LOCA Conclusions • None of the postulated scenarios results in uncovering of the core or core damage, including the most serious cold line break. • Post LOCA, decay heat can safely be dissipated to the reactor pool with no core damage. • Sufficient redundant safety features exist to prevent core damage as a result of a double-ended rupture of the largest diameter primary coolant piping without any additional protective system. • Model does not include two small check valves that allow make-up water from the reactor pool into the primary coolant system inverted loop.

  33. LOF Accident • Loss of Flow (LOF) accident initiation • Loss of Facility or pump power • Inadvertent closure of coolant loop isolation valves • Inadvertent loss of pressurizer pressure • Locked rotor in a coolant circulation pump • Failure of a coolant circulation pump coupling

  34. Downward, Upward, and Net Coolant Flow Through the Core During the First 12 Seconds of the LOF Accident

  35. Downward, Upward, and Net Coolant Flow Through the Core During the First 100 Seconds of the LOF Accident

  36. Coolant Flow Through the 25 Individual Coolant Channels During the First 60 Seconds of the LOF Accident

  37. Centerline Temperature of the 24 Fuel PlatesDuring the First 60 Seconds of the LOF Accident

  38. Temperature of the 25 Individual Coolant ChannelsDuring the First 60 Seconds of the LOF Accident

  39. Summary • A new detailed RELAP5 model has been developed to evaluate the thermal-hydraulic characteristics of the MURR during normal and accident conditions. • Evaluation of LOCA and LOF accidents, including individual fuel plate and coolant channel temperatures, demonstrate that fuel clad integrity is not challenged. • Future efforts will evaluate potential effects of the new LEU fuel element design, which includes wider coolant channels, and an expansion of the model for consideration of fuel elements with variable burn-up histories.

More Related