ML18250A019
| ML18250A019 | |
| Person / Time | |
|---|---|
| Site: | Brunswick  |
| Issue date: | 08/11/2016 |
| From: | Duke Energy Progress |
| To: | Office of Nuclear Reactor Regulation |
| Shared Package | |
| ML18250A015 | List:
|
| References | |
| BSEP 16-0069 | |
| Download: ML18250A019 (35) | |
Text
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 25 Chapter: 6 Page: 1 of 2 LIST OF FIGURES FIGURE NUMBER TITLE 6-1 DELETED IN REVISION 21 6-2 DELETED IN REVISION 21 6-3 DELETED IN REVISION 21 6-4 DELETED IN REVISION 21 6-5 DELETED IN REVISION 21 6-6 DELETED IN REVISION 21 6-7 DELETED IN REVISION 21 6-8 DELETED IN REVISION 21 6-9 DELETED IN REVISION 21 6-10 VARIATION OF PEAK DRYWELL PRESSURE WITH DRYWELL FREE VOLUME 6-11 CONTAINMENT PRESSURE RESPONSE TO DESIGN BASIS ACCIDENT LOCA AT 120 PERCENT UPRATE 6-12 CONTAINMENT TEMPERATURE RESPONSE TO DESIGN BASIS ACCIDENT LOCA AT 120 PERCENT UPRATE 6-13 DELETED IN REVISION 18A 6-14 ORIGINAL CALCULATED DRYWELL CONDITIONS FOLLOWING LOSS OF COOLANT ACCIDENT (SCALED UP 25 PERCENT TO ESTABLISH DESIGN CONDITIONS) 6-15 LOSS OF COOLANT ACCIDENT PRIMARY CONTAINMENT PRESSURE RESPONSE (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT) 6-16 PRIMARY CONTAINMENT TEMPERATURE RESPONSE TO LOSS OF COOLANT ACCIDENT (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT) 6-17 DRYWELL PRESSURE RESPONSE TO STEAM LINE BREAKS AT 120 PERCENT UPRATE 6-18 DRYWELL TEMPERATURE RESPONSE TO STEAM LINE BREAKS AT 120 PERCENT UPRATE 6-19 PRESSURE AND TEMPERATURE TRANSIENTS FOR SMALL STEAM LINE BREAKS (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT) 6-20 PRESSURE AND TEMPERATURE TRANSIENTS FOR SMALL STEAM LINE BREAKS (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT) 6-21 PRIMARY CONTAINMENT CAPABILITY INDEX FOR METAL-WATER REACTION 6-22 DELETED IN REVISION 21 6-23 DELETED IN REVISION 21 6-24 SUPPRESSION CHAMBER MAXIMUM NEGATIVE DIFFERENTIAL PRESSURE 6-25 MAXIMUM NEGATIVE DIFFERENTIAL PRESSURE VERSUS 6-26 PRESSURE-TEMPERATURE RESPONSE FOLLOWING LOSS OF DRYWELL COOLING 6-27 DELETED IN REVISION 17F 6-28 RECIRCULATION LINE AT SACRIFICIAL SHIELD 6-29 SHORT-TERM DESIGN BASIS ACCIDENT LOCA CONTAINMENT PRESSURE RESPONSE AT 120 PERCENT UPRATE 6-30 SHORT-TERM DESIGN BASIS ACCIDENT LOCA CONTAINMENT TEMPERATURE RESPONSE AT 120 PERCENT UPRATE 6-31 POOL TEMPERATURE RESPONSE VERSUS RESIDUAL HEAT REMOVAL COOLING INITIATION UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 25 Chapter: 6 Page: 2 of 2 LIST OF FIGURES FIGURE NUMBER TITLE 6-32 SCHEMATIC DIAGRAM - HIGH PRESSURE COOLANT INJECTION AND REACTOR CORE ISOLATION COOLING SYSTEMS 6-33 DELETED IN REVISION 21 6-34 DELETED IN REVISION 21 6-35 DELETED IN REVISION 21 6-36 DELETED IN REVISION 21 6-37 SUPPRESSION CHAMBER UNCONTROLLED HYDROGEN AND OXYGEN CONCENTRATION FOLLOWING A LOSS OF COOLANT ACCIDENT, NO CONTAINMENT LEAKAGE 6-38 DRYWELL UNCONTROLLED HYDROGEN AND OXYGEN CONCENTRATION FOLLOWING A LOSS OF COOLANT ACCIDENT, NO CONTAINMENT LEAKAGE 6-39 CONTROLLED HYDROGEN AND OXYGEN CONCENTRATION FOLLOWING A LOSS OF COOLANT ACCIDENT, NO CONTAINMENT LEAKAGE 6-40 MAXIMUM NITROGEN REQUIRED FOR DILUTION, SAFETY GUIDE NO. 7 ASSUMPTIONS, 0.5 PERCENT PER DAY CONTAINMENT LEAKAGE 6-41 DELETED BY REVISION 18A 6-42 DELETED BY REVISION 18A 6-43 DELETED BY REVISION 18A 6-44 CONTAINMENT PRESSURE RESPONSE TO CONTAINMENT ATMOSPHERE DILUTION OPERATION 6-45 PROCESS DIAGRAM - HIGH PRESSURE COOLANT INJECTION 6-46 DELETED IN REVISION 21 6-47 CHARACTERISTIC CURVE - HIGH PRESSURE COOLANT INJECTION PUMPS (MAIN AND BOOSTER) 6-48 CORE SPRAY SYSTEM PROCESS DIAGRAM 6-49 CHARACTERISTIC CURVE - CORE SPRAY PUMP 6-50 AVAILABLE NET POSITIVE SUCTION HEAD - REACTOR CORE ISOLATION COOLING AND HIGH PRESSURE COOLANT INJECTION PUMPS 6-51 RESIDUAL HEAT REMOVAL HEAD AND RESISTANCE CURVES 6-52 SCHEMATIC DIAGRAM - CONTROL ROOM VENTILATION SYSTEM - AIR FLOW DIAGRAM FOR HIGH RADIATION ISOLATION 6-53 SCHEMATIC DIAGRAM - CONTROL ROOM VENTILATION SYSTEM - AIR FLOW DIAGRAM FOR CHLORINE ISOLATION 6-54 STANDBY GAS TREATMENT SYSTEM UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-10 Page: 1 of 1 VARIATION OF PEAK DRYWELL PRESSURE WITH DRYWELL FREE VOLUME UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-11 Page: 1 of 1 CONTAINMENT PRESSURE RESPONSE TO DESIGN BASIS ACCIDENT LOCA AT 120 PERCENT UPRATE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-12 Page: 1 of 1 CONTAINMENT TEMPERATURE RESPONSE TO DESIGN BASIS ACCIDENT LOCA AT 120 PERCENT UPRATE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-14 Page: 1 of 1 ORIGINAL CALCULATED DRYWELL CONDITIONS FOLLOWING LOSS OF COOLANT ACCIDENT (SCALED UP 25 PERCENT TO ESTABLISH DESIGN CONDITIONS)
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-15 Page: 1 of 1 LOSS OF COOLANT ACCIDENT PRIMARY CONTAINMENT PRESSURE RESPONSE (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT)
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-16 Page: 1 of 1 PRIMARY CONTAINMENT TEMPERATURE RESPONSE TO LOSS OF COOLANT ACCIDENT (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT)
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-17 Page: 1 of 1 DRYWELL PRESSURE RESPONSE TO STEAM LINE BREAKS AT 120 PERCENT UPRATE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-18 Page: 1 of 1 DRYWELL TEMPERATURE RESPONSE TO STEAM LINE BREAKS AT 120 PERCENT UPRATE 0 50 100 150 200 250 300 350 Temperature (°F) 1 10 100 1,000 10,000 100,000 1,000,000 10000000 0.75 sq ft SLB 0.30 sq ft SLB 0.10 sq ft SLB 0.01 sq ft SLB UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-19 Page: 1 of 1 PRESSURE AND TEMPERATURE TRANSIENTS FOR SMALL STEAM LINE BREAKS (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT)
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-20 Page: 1 of 1 PRESSURE AND TEMPERATURE TRANSIENTS FOR SMALL STEAM LINE BREAKS (FOR ORIGINAL RATED THERMAL POWER, 2436 MWT)
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-21 Page: 1 of 1 PRIMARY CONTAINMENT CAPABILITY INDEX FOR METAL-WATER REACTION UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-24 Page: 1 of 1 SUPPRESSION CHAMBER MAXIMUM NEGATIVE DIFFERENTIAL PRESSURE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-25 Page: 1 of 1 MAXIMUM NEGATIVE DIFFERENTIAL PRESSURE VERSUS UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-26 Page: 1 of 1 PRESSURE-TEMPERATURE RESPONSE FOLLOWING LOSS OF DRYWELL COOLING UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-28 Page: 1 of 1 RECIRCULATION LINE AT SACRIFICIAL SHIELD UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-29 Page: 1 of 1 SHORT-TERM DESIGN BASIS ACCIDENT LOCA CONTAINMENT PRESSURE RESPONSE AT 120 PERCENT UPRATE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-30 Page: 1 of 1 SHORT-TERM DESIGN BASIS ACCIDENT LOCA CONTAINMENT TEMPERATURE RESPONSE AT 120 PERCENT UPRATE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-31 Page: 1 of 1 POOL TEMPERATURE RESPONSE VERSUS RESIDUAL HEAT REMOVAL COOLING INITIATION (BASED ON ORIGINAL DESIGN)
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-32 Page: 1 of 1 SCHEMATIC DIAGRAM - HIGH PRESSURE COOLANT INJECTION AND REACTOR CORE ISOLATION COOLING SYSTEMS UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-37 Page: 1 of 1 SUPPRESSION CHAMBER UNCONTROLLED HYDROGEN AND OXYGEN CONCENTRATION FOLLOWING A LOSS OF COOLANT ACCIDENT, NO CONTAINMENT LEAKAGE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-38 Page: 1 of 1 DRYWELL UNCONTROLLED HYDROGEN AND OXYGEN CONCENTRATION FOLLOWING A LOSS OF COOLANT ACCIDENT, NO CONTAINMENT LEAKAGE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-39 Page: 1 of 1 CONTROLLED HYDROGEN AND OXYGEN CONCENTRATION FOLLOWING A LOSS OF COOLANT ACCIDENT, NO CONTAINMENT LEAKAGE UPDATED FSAR CHAPTER TITLE CHAPTER 6 FIGURES Revision: 24 Figure: 6-40 Page: 1 of 1 MAXIMUM NITROGEN REQUIRED FOR DILUTION, SAFETY GUIDE NO. 7 ASSUMPTIONS, 0.5 PERCENT PER DAY CONTAINMENT LEAKAGE UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-44 Page: 1 of 1 CONTAINMENT RESPONSE TO CONTAINMENT ATMOSPHERE DILUTION OPERATION UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-45 Page: 1 of 1 PROCESS DIAGRAM - HIGH PRESSURE COOLANT INJECTION UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-47 Page: 1 of 1 CHARACTERISTIC CURVE - HIGH PRESSURE COOLANT INJECTION PUMPS (MAIN AND BOOSTER)
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-48 Page: 1 of 1 CORE SPRAY SYSTEM PROCESS DIAGRAM UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-49 Page: 1 of 1 CHARACTERISTIC CURVE - CORE SPRAY PUMP UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-50 Page: 1 of 1 AVAILABLE NET POSITIVE SUCTION HEAD - REACTOR CORE ISOLATION COOLING AND HIGH PRESSURE COOLANT INJECTION PUMPS UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-51 Page: 1 of 1 RESIDUAL HEAT REMOVAL HEAD AND RESISTANCE CURVES UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-52 Page: 1 of 1 SCHEMATIC DIAGRAM - CONTROL ROOM VENTILATION SYSTEM - AIR FLOW DIAGRAM FOR HIGH RADIATION ISOLATION UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-53 Page: 1 of 1 SCHEMATIC DIAGRAM - CONTROL ROOM VENTILATION SYSTEM - AIR FLOW DIAGRAM FOR CHLORINE ISOLATION NOTES 1. The chlorine protection/isolation system has intentionally been rendered non-functional by powering off the detectors for this system, and the chlorine tank car has been permanently removed from the site while the chlorine protection mode has been rendered non-functional. See Section 6.4.4.2 for additional information.
UPDATED FSAR ENGINEERED SAFETY FEATURES CHAPTER 6 FIGURES Revision: 24 Figure: 6-54 Page: 1 of 1 STANDBY GAS TREATMENT SYSTEM