ML20101G910

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Rev 7 to 25A5447, Certified Design Matl
ML20101G910
Person / Time
Site: 05200001
Issue date: 03/22/1996
From:
GENERAL ELECTRIC CO.
To:
Shared Package
ML20101G908 List:
References
25A5447, 25A5447-R07, 25A5447-R7, NUDOCS 9603280191
Download: ML20101G910 (21)


Text

25AS447 Rsv. 7 ABWR certiriacesienatuisi

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's 3.0 Additional Certified Design Material 3.1 Human Factors Engineering 3.2 Radiation Protection 3.3 Piping Design 3.4 Instrumentation and Control 3.5 Inidal Test Program 3.6 Design Reliability Assurance Program 4.0 Interface Requirements 4.1 Ultimate Heat Sink 1

4.2 Offsite Power System (2.12.1)

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4.3 Makeup Water Preparation System l 1

4.4 Potable and Sanitan Water System (2.11.23) '

4.5 Reactor Service Water System (2.11.9) p 4.6 Turbine Senice Water System (2.11.10) 4.7 Communication System (2.12.16) 4.8 Site Security 4.9 Circulating Water System (2.10.23) i 4.10 Heating, Ventilating and Air Conditioning (2.15.5) 5.0 Site Parameters Appendices Appendix A Legend For Figures Appendix B Abbreviations and Acronyms Appendix C Conversion to ASME Standard Units

  • Underlined sections -Title only, no enty for design certification.

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G' l ** Section number in parenthesis - Section under which the subject is covered 9603280191 960322 PDR ADOCK 05200001 A PDR Table of Contents VM i M

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.j: Table 2.7.1a Main Control Room Panels Fixed Position Alarms, Displays and Controls (Continued) b h A. Fixed Position Controls (Continued)

$ ARI(B) Logic Reset Switch RHR (A) Suppression Pool Cooling Mode Div. ll ADS Manual ADS Channel 2 Initiation 25 j initiation Switch Switch 0 CRD Charging Water Pressure Low Scram RHR (B) Suppression Pool Cooling Mode RCIC Div. I Isolation Logic Reset Switch

? Bypass Switch (A) Initiation Switch E CRD Charging Water Pressure Low Scram RHR (C) Suppression Pool Cooling Mode RCIC Div.11 Isolation Logic Reset Switch Bypass Switch (B) Initiation Switch CRD Charging Water Pressure Low Scram RHR (B) Primary Containment Vessel Spray RCIC Inboard Isolation Control Switch Bypass Switch (C) Mode Initiation Switch CRD Charging Water Pressure Low Scram RHR (C) Primary Containment Vessel Spray RCIC Outboard Isolation Control Switch Bypass Switch (D) Mode initiation Switch l Manual Scram Reset Switch SGTS (B) Initiation Switch Fire Protection System Motor Pump Control Switch l RPS Div. I Trip Reset Switch SGTS (C) Initiation Switch Fire Protection System Diesel Pump Control Switch y l RPS Div. Il Trip Reset Switch Div. I Manual ADS Channel 1 FCS (B) Control Switch k N

initiation Switch l RPS Div.111 Trip Reset Switch Div. I Manual ADS Channel 2 FCS (C) Control Switch initiation Switch RPS Div. IV Trip Reset Switch Div.11 Manual ADS Channel 1 Initiation Switch n

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$ Table 2.7.1a Main Control Room Panels Fixed Position Alarrr.s, Displays and Controls (Continued) b I #

B. Fixed Position Displays RPV Water Level RCIC Flow SRV Positions RCIC Turbine Speed RCIC Injection Valve Status Suppression Pool Level Wetwell Pressure HPCF (B) Injection Valve Status Main Steamline Flow Suppression Pool Bulk Average HPCF (C) Injection valve status SLC Boron Tank Water Level Temperature HPCF (B) Flow RHR (A) Flow Recirculation Pump Speeds HPCF (C) Flow RHR (A) Injection Valve Status Average Drywell Temperature RPV Pressure RHR (B) Flow Wetwell Hydrogen Concentration Level Drywell Pressure RHR (B) Injection Valve Status Drywell Hydrogen Concentration Level Reactor Power Level, RHR (C) Flow Drywell Oxygen Concentration ,

(Neutron Flux, APRM)

Operating Status N l MSIV Position Status (Inboard And Emergency Diesel Generator (B) FCS (C) Operating Status Outboard Valves) Operating Status Reactor Mode Switch Mode Indications Emergency Diesel Generator (C) Main Stack Radiation Level Operating Status Main Steamline Radiation Primary Containment Water Level Time Scram Solenoid Lights (8) Status Condensate Storage Tank Water Level Drywell Radiation Level f.

p Manual Scram Switch (A) Indicating Light Status SLC Pump (A) Discharge Pressure Wetwell Radiation Level

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g l Manual Scram Switch (B) Indicating Light Status SLC Pump (B) Discharge Pressure h g

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2.8.1 Nuclear Fuel Design Description The fuel assembly is designed to ensure that possible fuel damage would not result in the release of radioactive materials in excess of prescribed limits. The fuel assembly is comprised of the fuel bundle, channel and channel fastener. The fuel bundle is comprised of fuel rods, water rods, fuel rods containing burnable neutron absorber, spacers, springs and assembly end fittings.

The following is a summary of the principal design requirements which must be met by the fuel and is evaluated using methods and criteria to assure that:

l (1) Fuel rod failure is predicted to not occur as a result of normal operation and anticipated operational occurrences.

(2) Control rod insertion will not be prevented as a result of normal operation, anticipated operational occurrences or postulated accident.

(3) The number of fuel rod failures will not be underestimated for postulated O accidents.

b (4) Coolability will be maintained for all design basis events, including seismic and LOCAes us.

(5) Specified acceptable fuel design limits (thennal and tnechanical design limits) will not be exceeded during any condition of normal operation, including the effects of anticipated operational occurrences.

(6) In the power operating ranges, the prompt inherent nuclear feedback characteristics will tend to compensate for a rapid increase in reactivity.

(7) The reactor core and associated coolant, control and protection systems will be designed to assure that power oscillations which can result in conditions exceeding specified acceptable fuel design limits are not possible or can be reliably and readily detected and suppressed.

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2.8.3 Control Rod Design Description l Control rods in the reactor perform the funcdons of power distribution shaping, reactivity control, and scram reactivity insertion for safety shutdown response and have the following design features:

(1) A cruciform cross-sectional envelope shape.

(2) A coupling at the bottom for attachment to the control rod drive.

(3) Contain neutron absorbing materials.

The following is a summary of the principal design criteria which are met by the control rod:

(1) The control rod stresses, strains, and cumulative fatigue will be evaluated to not exceed the ultimate stress or strain of the material.

p (2) The control rod will be evaluated to be capable ofinsertion into the core during design basis modes of operation including safe shutdown earthquake event combined with LOCA event.

(3) The material of the control rod will be compatible with the reactor emironment.

l (4) The reactivity worth of the control rods will be included in the plant core analyses, and will provide, under conditions of normal operation (including anticipated operational occurrences), appropriate margin for malfunctions l such as two stuck rods (associated with a given accumulator), or accidental control rod withdrawal, without exceeding specified acceptable fuel design limits.

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Control Rod 2.8.3-1/2

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'% J l 2.8.4 Loose Parts Monitoring System Design Description l The Loose Parts Monitoring System (LPMS) monitors the reactor pressure vessel (RPV) for indicadons ofloose metallic parts within the reactor pressure vessel. The LPMS detects structure borne sound that can indicate the presence ofloose parts impacting against the reactor pressure vessel and internals. The system alarms when sensor signal characteristics exceeds preset limits.

The LPMS consists of sensors, cables, signal conditioning equipment, alarming monitors, signal analysis and data acquisition equipment. The LPMS processes signals from muldple sensors mounted on the external surfaces of the reactor coolant pressure boundary. The LPMS is classified as non-safety-related.

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The LPMS has provisions for both automatic and manual stanup of data acquistion ,

equipment with automatic activation in the event the preset alert level is reached or l exceeded. The system also initiates an alarm in the main control room when an alert condition is reached. l O)

(V The LPMS electronic components located inside the primary containment perform their function following all seismic events which do not require plant shutdown.

l l Inspections, Tests, Analyses and Acceptance Criteria l l

Tables 2.8.4 provides a definition of the inspections, tests and/or analyses, together with associated acceptance criteria, which will be undertaken for LPMS.

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(/O) l Loose Parts Monitoring System 2.8.4-1 l

$ Table 2.8.4 Loose Parts Monitoring System b

"+ CD Inspections, Tests, Analyses and Acceptance Criteria Design Commitment inspections, Tests Analyses Acceptance Criteria

1. Equipment comprising the LPMS is 1. Inspection of the as-built system will be 1. The as-built LPMS conforms with the defined in Section 2.8.4. conducted. description in Section 2.8.4.
2. The LPMS monitors the RPV for indication 2. Tests will be conducted on the as-built 2. The LPMS sensitivity, without the of loose metallic parts. LPMS. background noise associated with plant operation, is such that it can detect a metallic loose part that weighs from 0.11 kg to 13.6 kg and impacts with a maximum kinetic energy of 0.68 joules on the inside surface of the RPV within 0.91m of a sensor.
3. Main control room alarms provided for 3. Inspections will be performed on the main 3. Alarms exist or can be retrieved in the the LPMS are defined in Section 2.8.4. control room alarms for the LPMS. main control room as defined in Section u 2.8.4. 5 E
4. The LPMS electronic components located 4. Analyses will be performed or tests will 4. An analysis or test report exists which  ;

inside the primary containment perform be conducted on the seismic capability of concludes that the LPMS electronic  ;!

their function following all seismic events the LPMS electronic components located components located inside the primary N which do not require plant shutdown. in the primary coritainment. containment perform their function following all seismic events which do not require plant shutdown.

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2.12.1 Electrical Power Distribution System Design Description The AC Electrical Power Distribution (EPD) System consists of the transmission network (TN), the plant switching stations, the Main Power Transformer (MI'T). the Unit Auxiliary Transformers (UAT), the Reserve Auxiliary Transformer (s) (RAT (s)),

the plant main generator (PMG) output circuit breaker, the medium voltage metal-clad (M/C) switchgear, the low voltage power center (P/C) switchgear, and the motor control centers (MCCs). The distribution system also includes the power, instrumentation and control cables and bus ducts to the distribution system loads, and the protection equipment provided to protect the distribution system equipment. The EPD System within the scope of the Certified Design starts at the low voltage terminals of the MI'T and the low voltage terminals of the RAT (s) and ends at the distribution system loads. Interface requirements for the TN, plant switching stations, MPT, and RAT (s) are specified below.

The plant EPD System can be supplied power nom multiple power sources; these are independent transmission lines from the TN, the PMG, and the combustion turbine generator (CTG). In addition, the EPD System can be supplied from three onsite Class 1E Standby Power Sources (Emergency Diesel Generators (DGs)). The Class IE portion V of the EPD System is shown in Figure 2.12.1. l During plant power operation, the PMG supplies power through the PMG output i circuit breaker through the MI'T to the TN, and to the UATs. When the PMG output l circuit breaker is open, power is backfed from the TN through the MPT to the UATs. 1 The UATs can supply power to the non-Class IE load groups of medium voltage M/C power generation (PG) and plant investment protection (PIP) switchgear, and to the three Class 1E divisions (Division I, II, and III) of medium voltage M/C switchgear.

The RAT (s) can supply power to the non-Class 1E load groups of medium voltage M/C PG and PIP switchgear, and to the three Class 1E divisions (Division I, II, and III) of medium voltage M/C switchgear.

1 Non-Class 1E load groups of medium voltage M/C switchgear are supplied power from a UAT with an alternate power supply from a RAT. In addition, the non-Class IE medium voltage M/C switchgear can be supplied power from the CTG.

Class 1E medium voltage M/C switchgear are supplied power directly (not through any l l bus supplying non-Class 1E loads) from at least a UAT or a RAT. Class 1E medium l voltage M/C switchgear can also be supplied power from their own dedicated Class 1E DG or from the non-Class 1E CTG.

V The UATs are sized to supply their load requirements, during design operating modes, of their respective Class 1E divisions and non-Class 1E load groups. UATs are separated Electrical Power Distribution System 2.12.1-1

2SAS447 R1v. 3 ABWR certifiedcasiannesterisi O

from the RAT (s). In addition, UATs are provided with their own oil pit, drain, fire deluge system, grounding, and lightning protection system.

The PMG,its output circuit breaker, and UAT power feeders are separated from the RAT (s) power feeders. The PMG, its output circuit breaker, and UAT instmmentation and control circuits, are separated from the RAT (s) instmmentation and control circuits.

The MPT and its switching station instrumentation and control circuits, from the switchyard (s) to the main control room (MCR), are separated from the RAT (s) and its switching station instrumentation and control circuits.

The medium voltage M/C switchgear and low voltage P/C switchgear, with their l respective transformers, and the low voltage MCCs are sized to supply their load requirements. M/C and P/C switchgear, with their respective transformers, and MCCs are rated to withstand fault currents for the time required to clear the fault from the power source. The PMG output circuit breaker, and power feeder and load circuit breakers for the M/C and P/C switchgear, and MCCs are sized to supply their load requirements and are rated to intermpt fault currents.

Class IE equipment is protected from degraded voltage conditions.

EPD System interrupting devices (circuit breakers and fuses) are coordinated so that the circuit intermpter closest to the fault opens before other devices.

Instrumentation and control power for the Class IE divisional medium voltage M/C switchgear and low voltage P/C switchgear is supplied from the Class IE DC power system in the same division.

The PMG output circuit breaker is equipped with redundant trip devices which are supplied from separate, non-Class IE DC power systems.  !

EPD System cables and bus ducts are sized to supply their load requirements and are j rated to withstand fault cunents for the time required to clear the fault from its power I source. I For the EPD System, Class IE power is supplied by three independent Class 1E divisions. ,

Independence is maintained between Class IE divisions, and also between Class 1E l divisions and non-Class IE equipment.

The only non-Class 1E loads connected to the Class 1E EPD System are the Fine Motion l

Control Rod Drives (FMCRDs) and the associated AC standby lighting system.

There are no automatic connections between Class 1E divisions. '

2.12.1-2 Electrical Power Distribution System J

I 25AS447 Rw. 7 ABWR conmucessonneserist l O k'

l 2.12.14 Vital AC Power Supply Design Description l l

The Vital AC Power Supply consists of Class 1E and non-Class 1E uninterruptible power supplies, and their respecdve alternating current (AC) distribution panels, power, and instrumentation and control cables to the distribution system loads. The AC distribution system also includes the protection equipment provided to protect the AC i

distribution equipment. The Class 1E Vital AC Power Supply connections to the Electrical Power Distribudon (EPD) System and the Direct Current Power Supply are shown on Figure 2.12.14.

1 The Cass 1E Vital AC Power Supply consists of four divisions (Divisicn I, II, III, and IV) l l of unintermptible power supplies with their respective distribution panels. Each Class l 1E power supply provides uninterruptible, regulated AC power to Class 1E circuits which require continuity of power during a loss of preferred power (LOPP). Each Gass  ;

1E Vital AC Power Supply is a constant voltage constant frequency (CVCF) inverter '

power supply unit.

, p The non-Class IE Vital AC Power Supply consists of uninterruptible power supplies with

(' their respective distribution panels. Each non-Class 1E power supply prosides l

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uninterruptible, regulated AC power to non-Class 1E circuits which require continuity l of power during a LOPP. Each non-Class 1E Vital AC Power Supply is a CVCF inverter l power supply unit. I i Each Oass 1E CVCF unit has three input power sources. Except for the Division IV CVCF unit, the normal power to each Gass 1E CVCF unit is supplied from an AC motor control center (MCC) in the same Class 1E division as the CVCF unit. The Division IV Gass 1 E CVCF unit is supplied AC power from a Division II AC MCC. The backup power for each Cass 1E CVCF unit is supplied from the direct current (DC) battery in the ,

same Class 1E division as the CVCF unit. In addition, each Class 1E CVCF unit contains l l an alternate power supply. The alternate power supply is supplied power from the same l AC power source as the normal power supply. I I

Each Gass 1E CVCF normal and backup power supply is synchronized, in both i frequency and phase, with its alternate power supply and maintains continuity of power during transfer from the inverter to the alternate supply. Automatic transfer between each Class IE CVCF unit's three power sources is provided. Manual transfer between each Class 1E CVCF unit power source is also provided.

Each Class 1E CVCF unit is sized to provide output power to its respective distribution j

^ panel loads. There are no automatic connections between Class 1E divisions.

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Vital AC Power Supply 2.12.14-1

l 2SA54.37 Riv. 2 ABWR certifiedoesion nateriai O

Class IE CVCF units and their respective distribution panels are identified according to j their Class IE division and are located in Seismic Category I structures and in their respective divisional areas. Independence is provided between Class IE divisions, and also between Class IE divisions and non-Class IE equipment. l l

Class IE Vital AC Power Supply system distribution panels and their circuit breakers and l fuses are sized to supply their load requirements. Distribution panels are rated to  !

withstand fault currents for the time required to clear the fault from its power source.

Circuit breakers and fuses are rated to interrupt fault currents.  ;

l Class 1E Vital AC Power Supply system interrupting devices (circuit breakers and fuses) are coordinated so that the circuit interrupter closest to the fault opens before other desices.

Class 1E Vital AC Power Supply system cables are sized to supply their load requirements j and are rated to withstand fault currents for the time required to clear the fault from its power source.

The Class 1E Vital AC Power Supply system supplies an operating voltage at the terminals of the Class 1E utilization equipment that is within the utilization equipment's voltage tolerance limits.

Class IE Vital AC Power Supply system cables and raceways are identified according to their Class IE division. Class IE divisional cables are routed in Seismic Category I sauctures and in their respective divi.sional raceways.

The Class IE Vital AC Power Supply has alarms for high and low CVCF unit output l voltage and frequency in the main control room (MCR). l 4

1 Class 1E equipment is classified as Seismic Category I. I Class IE equipment which is located in areas designated as harsh emironment areas is qualified for harsh environments.

l Inspections, Tests, Analyses and Acceptance Criteria Table 2.12.14 provides a definition of the inspections, tests, and/or analyses, together with associated acceptance criteria, which will be undertaken for the Vital AC Power Supply.

O 2.12.14-2 Vital AC Power Supply

2SAS447 Rev. 7 ABWR certitiesoesig naterial O

V CLASS 1E VITAL AC POWER SUPPLY DC DISTRIBUTION PANEL AC MCC I I I CVCF ALTERNATE POWER POWER SUPPLY SUPPLY

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V U REACTOR CONTROL BUILDING

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TYPICAL OF 4 1 PER DIVISION (DIVISIONS 1, ll, Ill, IV)

NOTES:

1. THE DIVISION IV CLASS 1E CVCF UNIT IS SUPPLIED AC POWER FROM A DIVISION 11 AC MCC.

Figure 2.12.14 Vital AC Power Supply Vital AC Power Supply 2.12.14-3

Table 2.12.14 Vital AC Power Supply g t inspections, Tests, Analyses and Acceptance Criteria g Design Commitment inspections, Tests, Analyses Acceptance Criteria N

1. The basic configuration of the Vital AC 1. Inspections of the as-built system will be 1. The as-built Vital AC Power Supply Power Supply is described in Section conducted. conforms with the basic configuration 2.12.14. described in Section 2.12.14.
2. Each Class 1E CVCF unit has three input 2. Inspections of the as-built Class 1E Vital 2. Each as-built CVCF unit has three input power sources. Except for the Division IV AC Power Supply system will be power sources. Except for the Division IV CVCF unit, the normal power to each conducted. CVCF unit, the normal power to each Class 1E CVCF unitis supplied from an AC CVCF unit is supplied from an AC MCC in MCC in the same Class 1E division as the the same Class 1E division as the CVCF CVCF unit. The Division IV Class 1E CVCF unit.The Division IV CVCF unit is supplied unit is supplied AC power from a Division AC power from a Division II AC MCC. The 11 AC MCC.The backup power for each backup power for each CVCF unit is Class 1E CVCF unit is supplied from the supplied from the DC battery in the same y Class 1E division as the CVCF unit. In m DC battery in the same Class 1E division as the CVCF unit. In addition, each Class 1E CVCF unit contains an alternate power addition, each Class 1E CVCF unit contains an alternate power supply. The f;

l supply. The alternate power supply is alternate power supply is supplied power  ;

supplied power from the same AC power from the same AC power source as the N source as the normal power supply. normal power supply.

3. Automatic transfer between each Class 1E 3. Tests on each as-built Class 1E CVCF unit 3. Each as-built Class 1E CVCF unit CVCF unit's three power sources is will be conducted by providing a test automatically and manually transfers provided and maintains continuity of signal in one power source at a time. A between the unit's three power sources power during transfer from the inverter to test of the manual transferwill also be and maintains continuity of power during the alternate supply. Manual transfer conducted. transfer from the inverter to the alternate between each Class 1E CVCF unit power supply.

source is also provided.

4. Each Class 1E CVCF unit is sized to 4. Analyses for each as-built Class 1E CVCF 4. Analyses for each as-built Class 1E CVCF g.

3 Q provide output power to its respective unit to determine the power requirements unit exist and conclude that each CVCF g, g distribution panelloads. of its loads will be performed. unit's capacity, as determined by its e

p nameplate rating, exceeds its analyzed j.=

{ load requirements.

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& Table 2.14.6 Atmospheric Control System (Continued) b Inspections, Tests, Analyses and Acceptance Criteria

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~j. Design Commitment inspections, Tests, Analyses Acceptance Criteria 3

I k 6. Main control room displays and controls 6. Inspections will be performed on the 6. Displays and controls exist or can be

{ provided for the AC System are as main control room displays and controls retrieved in the main control room as y defined in Section 2.14.6. forthe AC System. defined in Section 2.14.6.

$ 7. RSS displays provided for the AC System 7. Inspections will be performed on the RSS 7. Displays exist on the RSS as defined in are as defined in Section 2.14.6. displays for the AC System. Section 2.14.6.

8. The COPS pneumatic actuated valves 8. Testswill be conducted in a test facility for 8. Upon receipt of an actuating signal, each shown on Figure 2.14.6 have active both cpening and closing under valve both opens and closes.

safety-related functions to both open and differential pressure, fluid flow and close, and perform these functions temperature conditions.

l against a pressure of 0.72 MPa (absolute) 5% and under fluid flow and temperature conditions. y m

9. The two valves in the containment 9. Tests will be conducted on the as-built AC 9. The two valves in the containment overpressure protection system fail open System pneumatic valves. overpressure protection system fail open y on loss of pneumatic pressure or loss of on loss of pneumatic pressure or loss of if electrical power to the valve actuating electrical power to the valve actuating [

solenoid. The other pneumatic valves solenoid. The other pneumatic valves shown on Figure 2.14.6 fail closed on loss shown on Figure 2.14.6 fail closed on loss of pneumatic pressure orloss of electrical of pneumatic pressure or loss of electrical power to the valve actuating solenoids. power to the valve actuating solenoids.

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I 25AS447 Riv. 7 ACWR corawedDesivounserior C

Fire dampers with fusible links in IWAC duct work close under air flow condidons.

The R/B Safety-Related Electrical Equipment HVAC System has the following displays and controls in the main control rooms:

(1) Controls and status indication for the active safety-related components shown on Figures 2.15.5f,2.15.5g, and 2.15.5h.

(2) Parameter displays for the instruments shown on Figures 2.15.5f,2.15.5g and 2.15.5h.

R/B Safety-Related Diesel Generator HVAC System The R/B Safety-Related DG IWAC System provides vendlation for the DG rooms when the DGs operate, and consists of three independent divisions. Each division consists of )

a filter unit and two supply fans. Figure 2.15.5i shows the basic system configuration and )

scope. j l

The R/B Safety-Related DG IWAC System is classified as safety-related.

On receipt of a DG start signal, both DG supply fans start. When the DG is operating, .

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the R/B Safety-Related DG INAC System and the R/B Safety-Related Electrical Equipment IWAC System maintain the temperature below 50'C.

l The R/B Safety-Related DG IWAC System is classified as Seismic Category I. The R/B

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Safety-Related DG IWAC System is located in the Reactor Building. l

, Each of the three divisions of the R/B Safety-Related DG HVAC System is powered from the respective Class IE division as shown on Figure 2.15.5i. In the R/B Safety-Related DG HVAC System, independence is provided between Class IE divisions, and also between the Class 1E divisions and non-Class 1E equipment.

Each mechanical division of the R/B Safety-Related DG IWAC System (Divisions A, B, C) is physically separated from the other divisions.

The R/B Safety-Related DG HVAC System has the following displays and controls in the main control room:

(1) Controls and status indication for the active safety-related components shown on Figure 2.15.5i.

R/B Secondary Containment HVAC System The R/B Secondary Containment HVAC System provides heating and cooling for the secondary containment. Figure 2.15.5j shows the basic system configuration and scope, a

O Heating. Ventilating and Air Conditioning Systems 2.15.S-7

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2SAS447 Retr. 3 i ABWR certifiedDesign nsaterial O 1 l

Except for the secondary containment isolation dampers, the R/B Secondary Containment HVAC System is classified as non-safety-related.

Normal Operating Mode In the normal operating mode, two supply fans and two exhaust fans operate. The supply fans operate only when the exhaust fans are operating.  !

l The R/B Secondary Containment HVAC System maintains a negative pressure in the secondary containment relative to the outside atmosphere.

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The R/B Secondary Containment HVAC System isolation dampers are closed upon l receipt of an isolation signal from the Leak Detection System (LDS) or a signal indicating loss of secondary containment exhaust fans.

Smoke Removal Mode The smoke removal mode is manually initiated by starting the standby exhaust and supply fans, opening the exhaust filter unit bypass dampers, and partially closing exhaust dampers for divisions not affected by fire.

The R/B Secondary Containment HVAC System penetrations of secondary containment and isolation dampers are classified as Seismic Category I. The R/B ,

Secondary Containment HVAC System is located in the Reactor Building, except for i some of the R/B secondary containment HVAC supply and exhaust air components which are located in the Turbine Building.

Each R/B Secondary Containment HVAC System isolation damper requiring electrical power is powered from the Class lE division, as shown on Figure 2.15.5j. In the R/B Secondary Containment HVAC System, independence is provided between Class IE divisions, and also between Class lE divisions and non-Class IE equipment.

Fire dampers with fusible links in HVAC duct work close under air flow conditions.

The R/B Secondary Containment HVAC System has the following displays and controls in the inain control room:

(1) Control and status indication for the active components shown on Figure 2.15.5j.

(2) Parameter displays for the instruments shown on Figure 2.15.5j.

The exhaust duct secondary containment isolation dampers are located in the secondary containment and qualified for a harsh environment.

2.15.S-8 Heating. Ventilating and Air Conditioning Systems

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1. THE OUTBOARD ISOLATION DAMPER R/B SECONDARY CONTAINMENT 4 SOLENOID VALVES ARE POWERED BY T/B CLASS 1E DIVISION 1. THE INBOARD g-ISOLATIOW DAMPER SOLENOID VALVES
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{ Figure 2.15.5j Reactor Building Secondary Containment HVAC System g  !

E Table 2.15.5a Control Room Habitability Area HVAC System b in ID Q inspections, Tests, Analyses and Acceptance Criteria Design Commitment inspections, Tests, Analyses Acceptance Criteria

1. The basic configuration of the CRHA 1. Inspections of the as-built system will be 1. The as-built CRHA HVAC System HVAC System is as shown on Figure conducted. conforms with the basic configuration 2.15.Sa. shown on Figure 2.15.Sa.
2. The emergency filtration unit have at least 2. 2. The emergency filtration unit efficiency is 95% removal efficiency for all forms of at least 95Yo.
a. Test will be conducted on each as-iodine (elemental organic, particulate, and built emergency filtration unit.

hydrogen ,odide).

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b. Tests in a test facility will be conducted on the iodine absorber material.
3. The exhaust fan automatically starts 3. Tests will be conducted on each division 3. The exhaust fan automatically starts when the supply fan is started. of the CRHA HVAC System by starting the when the supply fan is started.  %

supply fan. $

4. The MCAE is maintained at a minimum 4. Tests will be conducted on the as-built 4.

The MCAE is maintained at a minimum ~

pressure of 3.2 mm water gauge above the outside atmosphere.

CRHA HVAC System in the normal mode of operation.

pressure of 3.2 mm water gauge above the outside atmosphere.

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u x 5. 5. 5.

y. a. On receipt of a PRM System signal for a. Tests willbe conducted on each CRHA a. Upon receipt of a simulated initiation 9 high radiation in the outside air intake HVAC System division using a signal the following occurs:

{g of the operating division, the normal outside air intake dampers close, the simulated initiation signal.

(1) Normal outside air intake exhaust air dampers close, the dampers are closed.

s-7 exhaust fan stops, the minimum (2) Exhaust air dampers are closed.

{e outside air intake dampers open, and one fan of the emergency filtration (3) Exhaust fan is stopped. p

s 9 unit starts. (4) Minimum outside air intake g g dampers are opened. a.

[ (5) Emergency filtration unit fan is E.

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NOTE 1: Watertight doors to be provided in access corridor to prevent flood water external to the Reactor Building from entering the Reactor Building O

Figure 2.15.10h Reactor Building Arrangement, Floor B1F-Elevation 4800 mm 2.15.10-10 Reactor Building

2SA5447 Rev. 2 ABWR CertifiedDesipMaterist 5.0 Site Parameters This section provides a definition of the site parameters used as the basis for the Certified Design.

l Site Parameters ,

25A5447 Riv. 7 ABWR cenitiedoesiga uateriat O

Table 5.0 ABWR Site Parameters Maximum Ground Water Level: Extreme Wind: Basic Wind Speed:

61.0 cm below grade 177 km/hW/197 km/hm Maximum Flood (or Tsunami) level: Tornado 30.5 cm below grade

  • Maximum tornado wind speed: 483 km/h l
  • Maximum pressure drop: 13.827 kPaD Precipitation (for Roof Design):
  • Missile spectra: Spectrum I N
  • Maximum rainfall rate: 49.3 cm/hW

[

  • Maximum snow load: 2.394 kPa Ambient Design Temperature: Soil Properties:

1% Exceedance Values

  • Minimum stade bearing l
  • Maximum: 37.8'C dry bulb capacity: 718.20 kPa 25'C wet bulb (coincident)
  • Minimum shear wave velocity: 305 m/sW l 26.7'C wet bulb (non-coincident)
  • Liquefaction potential: None at plant site
  • Minimum: -23.3'C- resulting from site 0% Exceedance Values (Historical Limit) specific SSE ground
  • Maximum: 46.1'C dry bulb motion 26.7 C wet bulb (coincident) 27.2*C wet bulb (non<oincident) Stm.alogp
  • Minimum: -40*C
  • SSE respc.= cpectra: See Figures 5.0a and 5.0bW j Exclusion Area Boundary (EAB): An area whose Meteorological Dispersion (Chi /Q):

boundary has a Chi /Q less than or equal to a Maximum 2-hour 95% EAB 1.37 x 10-3 s/m 3 l 3 d 1.37x10-3s/m .

  • Maximum 2-hour 95% LPZ 4.11 x 10 s/m 3
  • Maximum annual average l 4

(8760 hour0.101 days <br />2.433 hours <br />0.0145 weeks <br />0.00333 months <br />) LPZ 1.17 x 10 s/m 3 (1)50-year recurrence interval; value to be utilized for design of non-safety-related structures only.

(2)100-year recurrence interval; value to be utilized for design for safety-related structures only.

(3) Maximum value for 1 hour1.157407e-5 days <br />2.777778e-4 hours <br />1.653439e-6 weeks <br />3.805e-7 months <br /> over 2.6 km2 probable maximum precipitation (PMP) with ratio of 5 minutes to 1 hour1.157407e-5 days <br />2.777778e-4 hours <br />1.653439e-6 weeks <br />3.805e-7 months <br /> PMP of 0.32. Maximum short-term rate: 15.7cm/5 min.

(4) Spectrum I missiles consist of a massive high kinetic energy missile which deforms on impact, a rigid missile to test penetration resistance, and a small rigid missile of a size sufficient to just pass through any openings in protective barriers.These missiles consists of an 1800 kg automobile, a 125 kg,20 cm diameter armor piercing artillery shell, and a 2.54 cm diameter solid steel sphere, all impacting at 35% of the maximum horizontal windspeed of the design basis tornado.The first two missiles are assumed to impact at normal incidence, the last to impinge upon barrier openings in the most damaging directions.

(5) At foundation level of the reactor and control buildings.

(6)This is the minimum shear wave velocity at low strains after the soil property uncertainties have been applied.

(7) Free-field, at plant grade elevation.

5.0-2 Site Pararneters