NSD-NRC-97-5152, Forwards Addl Info Re SSAR Markup Indicating Addl Changes to Passive Containment Cooling Sys & Revised SSAR Figures Indicating Results of Revised Wgothic Containment Pressure Analyses

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Forwards Addl Info Re SSAR Markup Indicating Addl Changes to Passive Containment Cooling Sys & Revised SSAR Figures Indicating Results of Revised Wgothic Containment Pressure Analyses
ML20140C439
Person / Time
Site: 05200003
Issue date: 05/23/1997
From: Mcintyre B
WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP.
To: Quay T
NRC OFFICE OF INFORMATION RESOURCES MANAGEMENT (IRM)
References
NSD-NRC-97-5152, NUDOCS 9706090268
Download: ML20140C439 (42)


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Westinghouse Energy Systems Ba 355 Electric Corporation Pittsbutgh Pennsylvania 15230-0355 NSD-NRC-97-5152 DCP/NRC0885

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l Docket No.: STN-52-003 May 23,1997 Document Control Desk

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U.S. Nuclear Regulatory Commission

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Washington, DC 20555 1

i ATTENTION: - MR. T. R. QUAY f

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SUBJECT:

AP600 DESIGN CHANGES TO ADDRESS POST 72-HOUR ACTIONS

Dear Mr. Quay:

In Westinghouse letter, Brian McIntyre to T. R. Quay, dated March 14,1997, Westinghouse indicated J

additional design changes were being implemented to address containment cooling in the post 72-hour l

to 7 day time frame after an event. Westinghouse also indicated that WGOTHIC containment l

pressure analyses with appropriate input were being performed. The attachments provide additional information related to these items as follows i

' - SSAR markup indicating additional changes to the passive containment cooling system.

j l - Description of method to account for circumferential (2-dimensional) conduction

-l through the steel containment shell for containment pressure analyses.

] - Revised SSAR figures indicating the results of the revised WGOTHIC containment i

pressure analyses.

l The SSAR markups in Attachments 1 and 3 will be incorporated in Revision 13 to the AP600 SSAR.

The NRC is requested to review the attached mataial and provide any further comments to Westinghouse by June 16,1997. Please contact Mr. Ron Vijuk on (412) 374-4728 if you have any questions concerning this transmittal.

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Brian A. McIntyre, Manager Advanced Plant Safety and Licensing l

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s-l Attachments 1-cc:

W. C. Huffman, NRC (w/ Attachments) l J. M. Sebrosky, NRC (w/ Attachments)

N. J. Liparulo, Westinghouse (w/o Attachments)

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3. Design of Structures, Components, Equipment, and Systems l

Table 3.2 3 (Sheet 8 of 64)

AP600 CLASSIFICATION OF MECHJLNICAL AND FLUID SYSTEMS, COMPONENTS, AND EQUIPMENT Tag Number Description AP600 Selsmic Principal Con-Comments Class Category struction Code i

Main Turbine and Generator Lube Oil System (LOS)

Location-Turbine Building i

System components ce Class E i

Mechanical Handling System (MHS)

Location: Various MHS-MH-01 Containment Polar Crane C

I AShE NOG-1 MHS-MH-05 Equipment H&tch Hoist C

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I Balance of system components are Class E l

Msin Steam System (MSS)

Location: Turbine Building l

System components are Class E I

Main Turbine System (MTS) location: Turbine Building I

System components are Class E I

Passive Containment Ccoling System (PCS) Locadon: Containment Shield Building and Auxiliary building i

PCS MT-Oi Passive Containment Cooling C I

ACI 349 See subsection l

Water Storage Tank 6.2.2.2.3 for I

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requirements 1

PCS MT-03 Water Distribution Bucket C

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I ASME III 3 PCS PL V001B PCCWST Isolation C

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3. Design of Structures, Ccmponents, Equipment, and Systems

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Table 3.2 3 (Sheet 10 of 62)

AP600 CLASSIFICATION OF MECHANICAL AND FLUID SYSTEMS, COMPONENTS, AND EQUIPMENT Tag Number Description AP600 Seismic Principal Con-Comments Class Category struction Code Passive Containment Cooling System (Continued)

PCS PL VOIS Recirculadon Pump 'Ihrottle D NS ANSI 16.34 Valve PCS PL V021 Recirculation Suction D

NS ANSI 16.34 Isolation Valve PCS PL V023 PCS Recirculation Return C

I ASME III 3 Isolation PCS PL V029 PCCWST Isolation Valve C

I ASME m 3 Leakage Detection Drain PCS PL-V032A Recirculation Pump Suction D

NS ANSI 16.34 Isolation Valve j

PCS PL-V032B Recirculation Pump Suction D

NS ANSI 16.34 Isolation Valve PCS PL-V033 R'ecirculation Pump Post.

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ASME III 3 Accident Makeup Isolation PCS-PL-V034 Recirculation Pump Post.

D NS ANS! 16.34 Accident Discharge Isolation PCS-PL V035 PCCWST/ Fire Protection C

I ASME III-3 Root Valve PCS PY B01 Spent Fuel Pool Emergency C I

ASME W-3 Makeup Isolation Balance of system components are Class E

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t 6.2.2 Passive Containment Cooling System The passive containment cooling system (PCS) is an engineered safety features system. Its functional objective is to reduce the containment temperature and pressure following a loss of coolant accident (LOCA) or main steam line break (MSLB) accident inside the containment by removing thermal energy from the containment atmosphere. The passive containment cooling system also serves as the means of transferring heat to the safety-related ultimate heat sink for other events resulting in a significant increase in containment pressure and temperature.

The passive containment cooling system limits releases of radioactivity (post-accident) by reducing the pressure differential between the containment atmosphere and the external environment, thereby diminishing the driving force for leakage of fission products from the containment to the atmosphere. This subsection describes the safety design bases of the safety-related containment cooling function.

Nonsafety-related containment cooling, a function of the containment l

recirculation cooling system, is described in subsection 9.4.6.

The passive containment cooling system also provides a source of makeup water to the spent fuel pool in the event of a prolonged loss of normal spent fuel pool cooling.

6.2.2.1 Safety Design Basis The passive containment cooling system is designed to withstand the effects of natural phenomena such as ambient temperature extremes, earthquakes, winds, tornadoes, or floods.

Passive containment cooling system operation is automatically initiated upon receipt of a Hi-2 contaiament pressure signal.

The passive containment cooling system is designed so that a single failure of an active component, assuming loss of offsite or onsite ac power sources, will n' t impair the o

capability of the system to perform its safety-related function.

Active components of the passive containment cooling system are capable of being tested during plant operation. Provisions are made for inspection of major components in accordance with the intervals specified in the ASME Code,Section XI.

1 The passive containment cooling system components required to mitigate the consequences

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of an accident are designed to remain functional in the accident environment and to withstand the dynamic effects of the accident.

The passive containment cooling system is capable of removing sufficient thennat energy including subsequent decay heat from the containment atmosphere following a design basis event resulting in containment pressurization such that the containment pressure remains l

below the design value with no operator ction required for :c ca days 72_ hours. He passive containment cooling system is designed to reduce containment pressure to less than one-half its design pressure within 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> following a postulated loss of coolant accident.

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The passive containment cooling system is designed and fabricated to appropriate codes e

consistent with Regulatory Guides 1.26 and 1.32 and in accordance with Regulatory Guide 1.29 as described in Section 1.9.

l 6.2.2.2 System Design 6.2.2.2.1 General Description l

The passive containment cooling system and components are designed to the codes and standards identified in Section 3.2; flood design is described in Section 3.4; missile protection is described in Section 3.5. Protection against dynamic effects associated with the postulated rupture of piping is described in Section 3.6.

Seismic and environmental design and equipment qualification are described in Sections 3.10 and 3.11. The actuation system is described in Section 7.3.

6.2.2.2.2

System Description

The passive containment cooling system is a safety-related system which is capable of transferring heat directly from the steel containment vessel to the environment. This transfer of heat prevents the containment from exceeding the design pressure and temperature following a postulated design basis accident, as identified in Chapters 6 and 15. Contaimnent pressure is further reduced to one-half the design pressure within 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> following the worst postulated loss of coolant accident.

The passive containment cooling system makes use of the steel containment vessel and the concrete shield building surrounding the containment. The major components of the passive containment cooling system are: the passive containment cooling water storage tank (PCCWST) which is incorporated into the shield building structure above the containment; an air baffle, located between the steel containment vessel and the concrete shield building, which defmes the cooling air flowpath; air inlets and an air exhaust, also incorporated into the shield building structure; and a water distribution system, mounted on the outside surface of the steel containment vessel, which functions to distribute water flow on the containment._A. passive _.gontainment_gooling_ ancillary water. storage. tank _ and_two. recirculation pumps are proyidedfor onsitejtorage..of. additional PCS coo. ling water and_to transfer the inventory.to..the P.CCWSL A normally isolated, manually-opened tiow path is available between the passive containment cooling system water storage tank and the spent fuel pool.

A recirculation patb is provided to control the passive containment cooling water storage tank water chemistry and to provide heating for freeze protection. Passive containment cooling water storage tank filling cperations and normal makeup needs are provided by the demineralized water transfer and storage system discussed in subsection 9.2.4.

The system piping and instrumentation diagram is shown in Figure 6.2.2-1. System parameters are shown in Table 6.2.2-1. A simplified system sketch is included as Figure 6.2.2-2.

6.2.2.2.3 Component Description j

The mechanical components of the passive containment cooling system are described in this subsection. Table 6.2.2-2 provides the component design parameters.

Passive Containment Cooling SyMem Water Storage Tank-The passive containment cooling l

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a system water storage tank is incorporated into the shield building structure above the containment vessel. The inside wetted walls of the tank are lined with stainless steel plate. It is filled with l

demineralized water and has a useable volume of greater than 400,000 53LO.00 gallons for passise containment cooling functions. The passive containment cooling system functions as the safety-related ultimate heat sink. The passive containment cooling water storage tank is seismically designed and miasile protected.

The surrounding reinforced concrete supporting structure is designed to ACI 349 as described in subsection 3.8.4.3.

The welded seams of the plates forming part of the leak tight boundary are examined by liquid penetrant after fabrication to confirm that the boundary does not leak.

The tank also has redundant level measurement channels and alarms for monitoring the tank water level and redundant temperature measurement channels to monitor and alarm for potential freezing.

To maintain system operability, a recirculation loop that provides chemistry and temperature control is connected to the tank.

The tank is constructed to provide sufficient thermal inertia and insulation such that draindown can be accomplished without heater operation.

In addition to its containment heat removal function, the passive containment cooling system water storage tank also serves as a source of makeup water to the spent fuel pool and a seismic Category I water storage reservoir for fire protection following a safe shutdown earthquake.

The PCCWST suction pipe for the fire protection system (FPS) is configured so that actuation of l

the FPS will not infringe on the MO;000 53L00_0 gallons volume allocated to the passive containment cooling function. Additionally actuation of the passive containment cooling system will not infringe on the 18,000 gallon volume allocated to the fire protection system.

Passive Containment Cooling System Water Storage Tank Isolation Valves - The passive containment cooling system water storage tank outlet piping is equipped with two sets of redundant isolation valves. The air-operated butterfly valves are nonnally closed and open upon receipt of a Hi-2 containment pressure signal. These valves fail-open, providing a fail-safe position, on the loss of air or loss of IE de power. The normally-open motor-operated gate valves are located upstream of the butterfly valves. They are provided to allow for testing or maintenance of the butterfly valves.

The storage tank isolation valves, along with the passive containment cooling water storage tank discharge piping and associated instrumentation between the passive containment cooling water storage tank and the downstream side of the isolation valves, are contained within a temperature-controlled valve room to prevent freezing. Valve room heating is provided to maintain the room temperature above 50 F.

Flow Control Orifices - Orifices are installed in each of the four passive containment cooling svstem water storage tank outlet pipes. They are used, along with the different elevations of the outlet pipes, to control the flow of water from the passive containment cooling system water storage tank as a function of water level. The orifices are located within the temperature-controlled valve room.

i Water Distribution Bucket - A water distribution bucket is provided to deliver water to the outer surface of the containment dome. The redundant passive containment cooling water delivery pipes and auxiliary water source piping discharge into the bucket, below its operational water level, to prevent excessive splashing. A set of circumferentially spaced distribution slots are included around the top of the bucket. The bucket is hung from the shield building roof and suspended just above the containment dome for optimum water delivery. The structural requirements for safety-related structural steel identified in subsection 3.8.4 apply to the water distribution bucket.

ANSI /ASCE-8-90 (Reference 24) is used for design and analysis of stainless steel cold formed parts. The water distribution bucket is fabricated from one or more of the materials included in j

Table 3.8.4-6, ASTM-A240 austenitic stainless steel, or ASTM-A276 austenitic stainless steel.

Water Distribution Weir System - A weir-type water delivery system is provided to wet the i

containment shell during passive containment cooling system operation. The system includes channeling walls and collection troughs, equipped with distribution weirs. The distribution system l

is capable of functioning during extreme low-or high-ambient temperature conditions. The structural requirements for safety related structural steel and cold fomied steel structures identified in subsection 3.8.4 apply to the water distribution weir system. ANSI /ASCE-8-90, (Reference 24) is used for design and analysis of stainless steel cold formed parts. The water distribution weir system is fabricated from one or more of the materials included in Table 3.8.4-6, ASTM-A240 austenitic stainless steel, or ASTM-A276 austenitic stainless steel.

Air Flow Path - An air flow path is provided to direct air along the outside of the containment shell to provide containment cooling. The air flow path includes a screened shield building inlet, an air baffle that divides the outer and inner flow annuli, and a chimney to increase buoyancy.

Subsection 3.8.4.1.3 includes information regarding the air baille. The general arrangement drawings provided in Section 1.2 provide layout information of the air flow path.

Passive Containment Cooline Ancillarv Water Storane Tank-The passive containment cooling. system ancillary.. water _ storage _ tank _is..a cylindrical..steeltank.. located at. ground level near the auxiliary bu_il. ding._It is_fi.lled..with_ demineralized._ water and_has. a. useable _ volume _of greater than 400,000. gallons. for_ makeup to the passive containment..coolling water _ storage ank, The tanis t

is_. designed as an ASME_section. Vill component and_to withstand.. seismic _.(SSE)_ conditions and a 145 mph. wind, The_ tank _has.. a. leyel_ measurement _and_an, alarm. for_ monitoring _the._ tank _ water _ level _and a temperature measurement channel to monitor and alarmfor potential freezing To. maintain systen) operabili.tymartin_ternalheater pontrolled.by...the. temperature... instrument _.is_provided to_ maintain water _ contents. aboyefreezingand chemistry.can be adjusted by PCCWST.. recirculation. loop.,

. The_tankjs insulated..to_ assure _ sufficient. thermal.. inertia _of.the contents. is_available_._to. prevent freezingfoL_ days without heater operation. The. transfer pipingis. maintained dry also to preclude 7

freezing; Chemical Addition Tank - The chemical addition tank is a small, venical, cylindrical tank that is sized to inject a solution of hydrogen peroxide to maintain a passive containment cooling water storage tank concentration for control of algae growth.

Recirculation Pumps - Each recirculation pump is a 100 percent capacity centrifugal pump with wetted components made of austenitic stainless steel. The pump is sized to recirculate the entire

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vd.coe of tank water once every week.

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Recirculation Heater - The recirculation heater is provided for freeze protection. The heater is sized based on heat losses from the passive containment cooling system water storage tank and recirculation piping at the minimum site temperature, as defmed in Section 2.3.

6.2.2.2.4 System Operation

. Operation of the passive containment cooling system is initiated upon receipt of two out cf four Hi-2 containment pressure signals. Manual actuation by the operator is also possible from either the main control room or remote shutdown workstation. System actuation consists of opening the passive containment cooling system water storage tank isolation valves. This allows the passive containment cooling system water storage tank water to be delivered to the top, external surface of i

the steel containment shell. The flow of water, provided entirely by the force of gravity, forms a l

water film over the dome and side walls of the containment structure.

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The flow of water to the containment outer surface is initially established at approximately 440 gpm for short-term containment cooline following a design basis loss of coolant accident. The l

flow rate is reduced over a period of 72 hours8.333333e-4 days <br />0.02 hours <br />1.190476e-4 weeks <br />2.7396e-5 months <br /> to a value of approximately M 61 gpm. and fna!!y l*

te app =!=atc!y !S ;p at :=c: day:. This flow provides the desired reduction in containment pressure over time and removes decay heat. The flow rate change is dependent only upon the decreasing water level in the passive containment cooling water storage tank.,_ Prior to 12_ hours l

aftetthe event. operator actions. are takenjo_ align the passive _ containment g.coling angillary_3 vater j

storage tank _.to.the.. suction.of.the PCS_recirculati.on pumps.Joleplenish_the.gooling._watetsupply_to l

the P_CCWST.,._ Sufficient.._ inventory _is_ avaibble_within. the PCCAWST_to_ main _tain_the. 63_.gpm flow rate for.an... additional 1 day.s,

. To adequately wet the containment surface, the water is delivered to the distribution bucket above j

the center of the containment dome which subsequently delivers the water to the containment' i

surface. A weir-type water distribution system is used on the dome surface to distribute the water for effective wetting of the dome and vertical sides of the containment shell. The weir system

contains radial arms and weirs located considering the effects of tolerances of the containment vessel design and construction. A corrosion-resistant paint or coating for the containment vessel is specified to enhance surface wetability and film formation.

The cooling water not evaporated from the vessel wall flows down to the bottom of the inner containment annulus into floor drains. The redundant floor drains route the excess water to stor drains. The drain lines are always open (without isolation valves) and each is sized to accept maximum passive containment cooling system flow. The interface with the storm drain system is j

an open connection such that any blockage in the sto_rm drains would result in the annulus drams overflowing the connection draining the annulus independently of the storm drain system.

1 A path for the natural circulation of air upward along the outside walls of the containment j.

structure is always open. The natural circulation air flow path begins at the shield building inlet, i'

where atmospheric air enters horizontally through openings in the concrete structure. Air flows past a set.of fixed louvers and is forced to turn 90 degrees downward into an outer annulus. This I

outer shield building annulus is encompassed by the concrete shield building on the outside and a removable baffle on the inside. At the bottom of the baffle wall, curved vanes aid in turning the flow upward 180 degrees into the inner containment annulus. This inner annulus is encompassed

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by the baffle wall on the outside and the steel containment vessel on the inside. Air flows up through the inner annulus to the top of the containment vessel and then exhausts through the shield building chimney.

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As the containment structure heats up in response to high containment temperature, heat is i

removed from within the containment via conduction through the steel containment vessel.

convection from the containment surface to the water film, convection and evaporation from the water film to the air, and radiation from the water film to the air baffle. As heat and water vapor are transfe: red to the air space between the containment structure and air baille, the air becomes less dense than the air in the outer annulus. This density difference causes an increase in the natural circulation of the air upward between the containment structure and the air baffle, with the l

air finally exiting at the top center of the shield building.

The passive containment cooling system water storage tank provides water for containment wetting l

for seven daysRhoun following system actuation. Operator action can be taken to replenish this water supply fronLthe PCCAWST or to provide an alternate water source directly to the containment shell through an installed safety-related seismic piping connection. In addition, water sources used for nonnal filling operations can be used to replenish the water supply.

The arrangement of the air inlet and air exhaust in the shield building structure has been selected so that wind effects aids the natural air circulation. The air inlets are placed at the top, outside of the shield building, providing a synunetrical air inlet that reduces the effect of wind speed and direction or adjacent structures. The air / water vapor exhaust stnicture is elevated above the air inlet to provide additional buoyancy and reduces the potential of exhaust air being drawn into the air inlet.

The air flow inlet and chimney regions are both designed to protect against ice or snow buildup and to prevent foreign objects from entering the air flow path.

Inadvertent actuation of the passive containment cooling system is terminated through operator action by closing either of the series isolation valves from the main control room.

Subsection 6.2.1.1.4 provides a discussion of the effects ofinadsertent system actuation.

6.2.2.3 Safety Evaluation The safety-related portions of the passive containment coo ing system are located within the shield l

building structure. This building (including the safety-related portions of the passive containment cooling system) is designed to withstand the effects of natural phenomena such as earthquakes, winds, tornadoes, or floods. Components of the passive centainment cooling system are designed to withscand the effects of ambient temperature extremes.

Operation of the containment cooling system is initiated automatically following the receipt of a Hi 2 contamment pressure signal. The use of this signal provides for system actuation during l

transients, resulting in mass and energy releases to containment, while avoiding unnecessary actuations. System actuation requires the openmg of eith::r isolation valve, with no other actions required to imtiate the post-accident heat removal function since the cooling air flow path is always open. Operation of the passive containment cooling system may also be initiated from the main control room and from the remote shutdown work station. A description of the actuation system is contained in Section 7.3.

The active components of the passive containment cooling system, the isolation valves, are located in two redundant pipe lines. Failure of a component in one train does not affect the operability of

the other mechanical train or the overall system performance. The fail-open, air-operated valves require no electrical power to move to their safe (open) position. The normally open motor-operated valves are powered from separate redundant Class IE de power sources. Table 6.2.2-3 presents a failure modes and effects analysis of the passive containment cooling system.

Capability is provided to periodically test actuation of the passive containment cooling system.

Active components can be tested periodically during plant operation to verify operability. The system can be inspected during unit shutdown. Additional information is contained in subsections 3.9.6 and 6.2.2.4, as well as in the Technical Specifications.

The passive containment cooling system components located inside containment, the containment pressure sensors, are tested and qualified to perform in a simulated design basis accident environment. These components are protected from effects of postulated jet impingement and pipe whip in case of a high-energy line break.

1 The-containment-pressure analyses demonstrate-that-the-passive-eentaimnent-eeoling-system 49 j

capable-of-removing sumetent-heat-energy including subsequent decay heat 4 rem 4he-containment etmosphere so-that-the-peak pressure-foHowing-the-worst-pestulated 103 of ecolant-accident-is belev the containmentwksign pressure-with-no-operator-actien-toweplenish the tank foe-et-least seven-dam Analyses also show that the containment pressure is reduced to below one-half of the design pressure within 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> following the most limiting design basis loss of coolant accident.

The containment pressure analyses are based on an ambient air temperature of 115 F dry bulb and 80 F coincident wet bulb. The passive containment cooling system water storage tank water temperature basis is 120 F. Results of the analyses are provided in subsection 6.2.1.

6.2.2.4 Testing and Inspection 6.2.2.4.1 Inspections The passive containment cooling system is designed to permit periodic testing of system readiness as specified in the Technical Specifications.

The portions of the passive containment cooling system from the isolation valves to the passive containment cooling system water storage tank are accessible and can be inspected dunng power operation or shutdown for leaktightness. Examination and inspection of the pressure retaining piping welds is performed in accordance with ASME Code,Section XI. The design of the containment vessel and air baffle retains provisions for the inspection of the vessel during plant shutdowns.

6.2.2.4.2 Precperational Testing Preoperation testing for the passive containment cooling system is addressed in Chapter 14.

6.2.2.4.3 Operational Testing Operational testing is performed to:

l Demonstrate that the sequencing of valves occurs on the initiation of Hi-2 contamment l

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pressure and demonstrate the proper operation of remotely operated valves.

Verify valve operation during plant operation. The normally open motor-operated valves, in series with each normally closed air-operated isolation valve, are temporarily closed.

This closing permits isolation valve stroke testing without actuation of the passive containment cooling system.

l Verify water flow delivery, consistent with the accident analysis.

Verify visually that the path for containment cooling air flow is not obstructed by debris or foreign objects.

Test frequency is consistent with the plant technical specifications (Section 16.3.6) and l

insersice testing program (Section 3.9.6).

i 6.2.2 5 Instrumentation Requirements The status of the passive containment cooling system is displayed in the main control room. The operator is alerted to problems with the operation of the equipment within this system during both normal and post-accident conditions.

Normal operation of the passive containment cooling system is demonstrated by monitoring the recirculation pump discharge pressure, flow rate, passive containment cooling system water storage tank level and temperature,. passive.. containment. cooling.ancillaryavater storage.. tank. level and tempgrature, and valve room temperature. Post-accident operation of the passive containment cooling system is demonstrated by monitoring the passive containment cooling system water storage tank level, passive containment cooling system eeeleg water flow rate, containment pressure and external cooling air discharge temperature.

The information on the activation signal-generating equipment is found in Chapter 7.

The protection and safety monitoring system providing system actuation is discussed in Chapter 7.

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i Table 6.2.21 PASSIVE CONTAINMENT COOLING SYSTEM PERFORMANCE PARAMETERS jYl

' PCCWST" useable capacity Ior PCS (gal) - Minimum

' 'G.mxb PCCWST useable capacity for FPS * (gal) Minimum...

. x)

Injection tiow rate (gpm) Initial Minimum....

.440 Injection tiow rate (gpm) Flow at 72 hours8.333333e-4 days <br />0.02 hours <br />1.190476e-4 weeks <br />2.7396e-5 months <br /> Minimum....

. gd.8T Injection flow rate (gpm) - Finai at 7 days Minimum.

.1f4f.5%

injection duration (days) Minimum 7

PCCWST minimum temperature (*F)..

40 PCCWST maximum temperature ('F).

120 Notes:

1.

PCCWST = passive containment cooling water storage tank 2.

FPS = fire protection system i

I l

l l

i

Table 6.2.2 2 COMPOF'ENT DATA PASSIVE CONTAINMENT COOLING SYSTEM T

(Nominal)

Passive Containment Cooling ater Storage Tank Volume (gal). Nominal) f ert11T" Design iemperature ('F) 125 l

Design pressure (psig)

Material Atmospheric

..... Concrete with stainless steel ime-Passive Containment Ancillary Cooling ater Storage Tank Volume (gal). Nominal) 425.000 Design temperature (*F) 125 Design pressure (psig).

A t mosphe ric N Material..........

teel 7

Water Distribution Bucket Volume (gal). Nominal..

42 1

Design temperature (*F)..

150 Design pressure (psig)

Atmospheric Material...

Stainless steel Water Distribution Collection Troughs and Weirs Design temperature (*F)

. N/A Design pressure (psig)

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PCS - Operating i

3.6.6 ACTIONS (continued)

CONDITION REQUIRED ACTION COMPLETION TIME D.

Required Action and 0.1 Be in MODE 3.

8 hours9.259259e-5 days <br />0.00222 hours <br />1.322751e-5 weeks <br />3.044e-6 months <br /> associated Completion Time of Conditions A, AND B, or C not met.

D.2 Be in MODE 4.

72 hours8.333333e-4 days <br />0.02 hours <br />1.190476e-4 weeks <br />2.7396e-5 months <br /> 0_R LC0 not met for reasons other than A, B, or C.

SURVEILLANCE REQUIREMENTS SURVEILLANCE FREQUENCY SR 3.6.6.1 Verify the water storage tank temperature

- - NOTE----

2: 40 *F arrd :s 120*F.

Only required when the l

ambient temperature is s 32*F or a: 100*F f

24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br />

/

{

SR 3.6.6.2 Ve

_the ater storage tank volume 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> l

  1. ^,00a allons.

i l

SR 3.6.6.3 Verify each passive containment cooling 24 hours2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> system, power operated, and automatic l

valve in each flow path that is not locked, sealed, or otherwise secured in l

position, is in the correct position.

1 (continued) i 1

j(

i I

h AP600 3.6-15 08/96 Amendment 0

.,a, m ea m an ~ ~ ~

t I

. -. - ~ -. -

- -.- ~.-

PCS - Operating l

B 3.6.6

~

B 3.6 CONTAINMENT SYSTEMS B 3.6.6 Passive Containment Cooling System (PCS) - Operating BASES i

BACKGROUND The PCS provides containment cooling to limit post accident pressure and temperature in containment to less than the design values.

Reduction of containment pressure reduces the release of fissien product radioactivity from containment to the environment, in the event of a Design Basis Accident (DBA). The Passive Containment Cooling System is designed to meet the requirements of GDC 38

" Containment Heat Removal" and GDC 40 " Testing of Containment Heat Removal Systems" (Ref. 1).

P t%e The PCS consists of a C06300JPcooling water tank, t4 wee headered tank discharge lines with flow restricting orifices, and two separate full capacity discharge flow paths to the containment vessel with isolation valves, each capable of meeting the design bases.

The isolation valves on each flow path are powered from a separate Division.

Upon actuation of the isolation valves, gravity flow of water from the cooling water tank (contained in the shield building structure above the containment) onto the upper portion of the containment shell reduces the containment i

pressure and temperature following a DBA. The flow of water i

to the containment shell surface is initially established to assure that the required short term containment cooling requirements following the postulated worst case LOCA are achieved. As the decay heat from the core becomes less with l

time, the water flow to the containment shell is reduced in two steps. The change in flow rate is attained without sctive components in the system and ic dependent only on the decreasing water level in the elevated storage tank.

In order to ensure the containment surface is adequately and l,

effectively wetted, the water is introduced at the center of the containment done and flows outward. Weirs are placed on the dome surface to distribute the water and ensure effective wetting of the dome and vertical sides of the J

containment shell.

The path for the natural circulation of air is from the air intakes in the shield building, down the outside of the i

baffle, up along the containment shell to the top, center i

4 (continued) l

(

h AP600 B 3.6-30 08/96 Amendment 0 mmw.emiseesesumooisse

0 e

9 s

D 8

ATTACHMENT 2 DESCRIPTION CF METHOD TO ACCOUNT FOR CIRCUM FERENTIAL (2-DIMENSION AL) CONDUCTION THROUGH THE STEEL CONTAINMENT SHELL FOR CONTAINMENT PRESSURE ANALYSES.

l l

I e-

l TWO-DIMENSIONA.L CONDUCTION THROUGH TIIE AP600 CONTAINMENT l

SHELL FOR THE AP600 CONTAINMENT EVALUATION MODEL i

1.0 INTRODUCTION

l l

\\

The AP600 Passive Containment Cooling System transfers heat from the containment j

atmosphere to the outside environment. For the first seven days following a postulated accident, cooling water is applied to the outside surface of the shell to facilitate the heat removal process by evaporation of the applied water. Early in the postulated event, the water applied to the shell exterior provides at least 90% coverage of the external surface. As the transient progresses, the applied flow rate is reduced and the water coverage of the external surface area of the shell is reduced.

As evidenced by test data, the flow distribution weirs develop alternating wetted and dry, vertical " stripes" of containment surface areas. These stripes become clearly segregated as the applied water flow rate is reduced. Heat removal from the wetted areas is greater than from the dry areas; evaporative cooling in the wetted area is much greater than convection from the i

dry surface. This difference in heat removal capability results in a two-dimensional heat i

transfer through the thickness of the containment shell. Thermal energy is conducted from the hotter dry stripe areas into the adjacent portions of the containment shell cooled by a wetted stripe. The transfer of additional thermal energy to the wetted stripe increases the water evaporation rate, the containment heat removal rate, and the use of applied flow to cool the containment.

l l

2.0 EFFECT OF CIRCUMFERENTIAL (2-D) CONDUCTION THROUGH THE STEEL CONTAINMENT SHELL ON THE EVAPORATION OF WATER BY THE AP600 PASSIVE CONTAINMENT COOLING SYSTEM (PCS)

The AP600 water distribution testing, performed as part of the AP600 design certification program, showed that the outside surface of the containment shell will be partially wetted when the applied water flowrate is reduced below the high initial flowrate. At cold, unheated conditions, the observed side wall wetting was 47% with 110 gpm and 24% with 55 gpm equivalent applied flows for the AP600. The limited percentages of wetted area were a censequence of cold water being applied to the cold surface at discretely spaced locations and the fact that the cold water spread to a stream width that resulted in a Ib of ~290 lb/hr ft,4,,,.

Therefore, the observed stream width and wetted surface areas were directly proportional to the water flow rate. At the flow rates given above, the stream widths were observed to be less than the di,tance between weir slots and alternating, vertical, dry and wetted stripes formed down the containment below the lower distribution weir.

Since the rate of evaporation of water from the containment shell is largely a function of the water film temperature, heat transfer from the dry surface areas to the wetted surface areas I

l

i.

l l

r will result in a significant enhancement to the currently calculated evaporation rates. The currently calculated evaporation rates are based or one dimensional, radial conduction through the containment steel shell As the PCS flows are reduced and wetted areas decrease, a significant amount of heat will be conducted circumferentially through the steel shell from adjacent hotter dry vertical stripes to the cooler wetted vertical stripes. Following is a description of the method used to calculate the effect of circumferential 2-dimensional heat conduction on the water evaporation and resulting containment pressure for the AP600

)

passive containment cooling system.

2.1 Geometry of the Wet and Dry Veitical Stripes on the Containment Outside Steel Surface l

The occurrence of alternating wet and dry vertical stripes on the containment outside surface l

has been documented both on a cold, full scale model of 1/16th of the containment dome and l

top portion of the containment sidewall, in the AP600 Water Distribution Test (Ref. I and Figure 1), and on a hot surface with evaporation in progress in the PCS Large Scale Test (Ref. 2). In the water distribution test, it was demonstrated that water applied by the second (lower) set of weirs on the significantly downward sloped portion of the containment dome follows the natural fall line; resulting in wetted stripes at a spacing on the vertical sidewall i

that is equal to the spacing of applied water streams at the weir, multiplied by the ratio of the l

containment radius at the sidewall and the radius at the weir. For example, the 6-inch weir l

slot spacing at the ~50-foot radius of the dome produced stripes at a spacing of ~8-inches at the l

sidewall radius of 65-feet, and the stripes remained separated at low applied.flowrates. In the i

Large Scale Test, with heat transfer occurring, the wet stripes were observed to flow vertically to the bottom of the sidewall until almost all of the applied water was evaporated.

t l

This evaluation of the effects of 2-dimensional conduction on the wetted steel surface temperature and resulting water evaporation rate was based on the same attemating wet and dry stripe pattern and spacing produced by the water distribution weir (s) observed in the l

water distribution test. Namely, an 8.35 inch center-line to center-line stripe spacing was used. This corresponded to the lower weir position and weir notch spacing to be used in the l

plant. In addition, a wider dry stripe directly under the 16 weir collection boxes was taken into account.

I 2.2 Inside and Outside Heat Transfer Boundary Conditions for the Conduction Model The boundary conditions used in the 2-dimensional conduction model were established by a series of 1-dimensional steady state calculations of the PCS heat transfer process performed at steady state containment pressures ranging from 10 psig to 65 psig (24.7 to 79.7 psia). These calculations were done using the same heat and mass transfer methodology as used in l

WGOTHIC and provided the acat transfer and the temperature differences from the steam / air mixture inside wntainment to the inside stuface of the containment shell, through the steel shell, and from the wet and dry outside containment surface to the air. The heat transfer and i

d

?

4

_. ~ _ _ _

temperature differences were used to establish boundary condition heat transfer coefficients for each containment pressure condition. The outside heat transfer coefficients vs. the outside steel shell temperature obtained for each pressure condition for the wetted surface, were fitted using a second degree polynomial for use in the conduction model. These boundary conditions were reviewed to assure that the heat transfer rates at all containment pressure / temperature conditions were higher than the corresponding heat transfer calculated by WGOTHIC in the containment analysis. This assures that any increase in heat transfer, as compared to the heat transfer with radial cor: duction through the containment steel shell, is underpredicted.

2.3 Conduction (ANSYS) Model Description The effect of circumferential conduction through the AP600 steel containment shell on the shell surface temperatures and the resulting effects on the condensing heat transfer on the inside surface, the evapora'tive heat transfer on outside wetted surfaces, and the convective heat transfer from the dry outside surface; were quantified using the ANSYS computer code.

The ANSYS computer code is a multi-purpose, finite element program which has been commercialiy used since 1970. For this calculation ANSYS revision 5.3 was used.

The ANSYS calculation was a two dimensional thermal steady state analysis of a periodic half-cell (cross section) that consisted of a two-dimensional block that was 0.1354 feet i

(1.625 inches) thick and 0.3479 feet (4.174 inches) wide; corresponding to the AP600 containment steel shell thickness and the spacing of water streams at the containment sidewall perimeter imposed by the PCS water distribution weirs. The half-cell had a length of one unit (1-ft.). A conductivity of 24 Btu /hr-ft 'F was assigned for the steel material. Adiabatic boundary conditions were used for the right and left side of the half-cell model to represent symmetry and periodicity of the cell.

l The inside containment bulk temperature and a steam / air mixture heat transfer coefficient to the inside steel surface were input for each containment inside pressure condition analyzed.

The outside heat transfer coefficient vs. the wetted steel outside surface temperature and a l

constant dry surface heat transfer coefficient (with a fixed outside cooling air temperature) conservatively bounding the pressure conditions analyzed, established the outside heat transfer boundary conditions.

2.4 Conduction (ANSYS) Model Results The heat flux frotn the wetted portion of the half-cell model were compared with the wetted heat flux that occurs when radial heat conduction (1-dimensional conduction) is assumed.

Figure 2 shows the water evaporation rate with 2-dimensional conduction vs. the fraction of j

wetted area, normalized to the evaporation rate calculated with radial heat conduction (1-dimensional) outward through the steel shell, for containment pressures of 10,15,20, and 25 j

psig. Several additional plots to illustrate the effect of 2-dimensional conduction on the PCS g

heat transfer process are provided for the 20 psig containment pressure,25% wetted case. A i

l

temperature distribution contour plot is shown for the ANSYS half-cell model in Figure 3, with the surface inside containment at the top of the page. Figure 4 shows the thermal flux from the inside to outside surface (-y direction), perpendicular to the containment shell.

l Figures 5 and 6 show the thermal flux distribution on the outside and inside surface of the wall respectively.

2.5 Insights from the PCS Large Scale Testing Although the large scale PCS heat transfer testing was largely conducted with very high water coverage fractions, that minimize the effect of circumferential conduction on the water evaporation rate; a clear indication of this effect is demonstrated by comparing the results from test run RC048C of test matrix 212.1 and test run RC050C of test matrix 213.1. In these tests, the containment pressure and other boundary conditions were essentially the same j

with the exception that the amount of water applied to the external surface of the test vessel was 17.4 gpm in test RC048C and 6 gpm in test RC050C.

l The reduced water flow rate in test RC050C resulted in a significant reduction in the wetted i

area observed at the bottom of the test vessel sidewall,52% for test RC050C vs. 95% for test l

RC048C. In spite of the reduced wetted area in test RC050C, the total heat removed from i_

the test vessel and the amount of water evaporated in this test was equal to test RC048C. A l

re-examination of this test data is underway, however it can be stated that the inside/outside l

thermocouple pairs (used as local heat flux meters) where dry / wet stripes occur, demonstrate the following:

j Elevated wet surface temperatures and enhanced water evaporation occurs at wetted locations adjacent to dry stripes.

Large measured through wall temperature differences occur at dry locations adjacent to l

wet stripes, as would be expected with skewed isotherms similar to that shown in Figure 3.

Expected temperature differences and heat fluxes occur on both wet and dry surface locations not adjacent to the edges of stripes.

3.0 APPLICATION TO AP600 CONTAINMENT EVALUATION MODEL l

The AP600 PCS heat removal at a given containment pressure is determined largely by how much of the applied water is evaporated. The heat removal or cooling effectiveness of the

(

cooling water applied to the containment shell is maximized if all the water applied j.

evaporates. Consequently, the determination of how much water, if any, runs off the

{

containment shell is necessary m determining the effectiveness of the applied cooling water.

The current containment analysis approach calculates the effective PCS flow rate for input to t

i i

g 1

4

l the WGOTHIC code. The PCS flow is limited to only that flow which is calculated to be evaporated. This is done so that the code is not required to determine wetted area as a function of time. The applied PCS flow defined in this manner is called the " evaporation limited flow" in the AP600 WGOTHIC Applications Report, Reference 3. The use of j

" evaporation limited flow" for the containment evaluation model is conservative because it accounts for only evaporated water and discounts sensible heating of any runoff flow.

In the AP600 plant, as the water coverage of the containment shell decreases due to decreases in PCS flow rates, alternate wet and dry stripes are formed on the containment shell exterior surface and 2-dimensional (radial and circumferential) heat conduction is established in the containment shell. Initial calculations of "esaporation limited flow" accounted for only l-dimensional (radial) conduction through the containment shell.

Accounting for 2-dimensional conduction increases the temperature of the wetted steel surface, and therefore also increases the temperature of the liquid film, over what is calculated j

for 1-dimensional (radial) conduction only. The increase in the temperature of the liquid film, in turn, results in the evaporation of more water, reducing the calculated runoff from the shell. The following is a description of how the increase in water evaporation effectiveness of the PCS when both radial and circumferential heat conduction through the steel containment is accounted for in the AP600 containment evaluation model.

3.1 Calculating Fraction of PCS Water that Does Not Evaporate The amount of water runoff from the containment shell utilizes the simple relationship between the total film flow rate, th; the total circumference, or width of the wetted surface, W; and the film flow per unit width, F. The equation is; s=PW (1) and its derivative with respect to vertical distance is;

'd s W E + P A#-

(2)

=

dz dz dz The wetted coverage and runoff flow rate are calculated based on the following assumptions; l) The initial film flow rate per unit width, Foisy, is determined in part by the distribution system and the ability of cold water to spread on the cold containment surface.

l l

2)

The water flows in constant width stripes below each weir slot while the flow rate l-(water film thickness) decreases due to evaporation for Foist > r > Twy, The distance i

the stripe travels down the containment sidewall is bounded 0 < Z < Zwy, where Zwy

is the distance down the containment wall where F = Fum.

3) At F = Fum, evaporation causes the film stripe to narrow while F remains constant at MIN-Initial Coverage The wetted coverage on AP600 containment with cold water was characterized in the Water Distribution Tests. The initial film flow per unit width at the 65 ft radius, Foist, is presented in Table 7-2 of Reference 3. The film flow rate per unit width at the spring line is related to the wetted primeter, W and the applied flow rate, m, by Equation 1, m y = W searso a

srarso Foist where forsT = 293 lb /hr-ft.

Constant Widtin Coverage After the water distribution is established, the film evaporates at mass flux, $y, as it flows down the shell in stripes having parallel sides. Since the stripes are parallel sided, W is constant at Wsegma. For a constant width stripe, dr/dz = - $y. The change equations for th, F, and W for the constant width portion of the stripe are:

ds 4

W (3) dz 4y (4)

=

dW

=0 (5) dz With the three equations listed above, the film mass flow rate, rh; and the flow rate per un;t width, F; can be calculated for the constant width evaporation portion of the coverage. For the case with 4y = constant and W = constant as is assumed for r is7 > r > r and O < Z o

uiu

< Zum, the analytical expression for the mass flow rate is:

s=s

- $y W,37 Z

(6) os o

Equation 6 can be written in terms of difference equations for a numerical solution where Arh I

= m2 - mi and AZ = Z - Z 2

i 6

P l

j

~

As=-W

  • &w
  • A Z (7) sramo t

s - W,13a + $y %-Z )

2 i

3p i

Knowing th, the film flow rate per unit width 'is determined from Equation (1) where F is Emsr = m/W. The value of Z when F reduces to Fum is Zum. The value of Zum can be determined from Equation 6. That is, sos / Wmsr m

-P g,

g

$w Constant Fyn Coverage

- When F = Fum, the stripe width, W, begins to narrow while r is maintained at a constant um l

The resulting change equations for th, F, and W for this portion of the stripe are:

va ue.

b = 4, W (10) dz E0 (11) dz dW

- *u *

(12)

=

az r

When $y = constant and F = Fum = constant, the solution to the dW/dZ expression is the simple exponential function:

W =W exP*w

  • iU uin (13) asr When $y is not constant with height the analytical expression for W depends on the functional form of $u and is not necessarily a simple expressicn. However, a general expression is written for numerical integration:

Knowing W from equation 13,14 or 15, the mass flow rate at any Z is simply calculated j

7

= -

(14)

AW IMw W, -

(15)

M W,

=

I

~

Mm from Equation (1). The runoff flow rate is morr = WFum, where W is the value at the bottom of the containment shell, Z = Zm.

Source for Entr and Fyn The constant input values for the minimum stable film flow per unit width, fyrs and the source film, Fois7 are listed in Section 7 of Reference 3. It is assumed that the film thins while the film width, W, remains constant, until Furs is reached. The value for Fois7 is based on observations from the PCS Water Distribution Test. The thinning of the liquid film until Furs is reached and narrowing afterwards is consistent with observations from the Large Scale Test, and the value of Fum is based on test and analytical results, Reference 3.

3.2 Evaporation Limited Flow Calculation By inspection of equation 13, it is noted that W, the film flow per unit width, is always greater than zero. Thus, for constant values of $ and Fum, equation 13 will always predict some water will run off the wall without evaporating. However, from calculations performed with the WGOTHIC code and experimental obs:rvations, all the water applied to the containment shell can be evaporated for some transient conditions. Thus, the preceding calculation method is conservative in its execution. This calculational method is applied to WGOTHIC code calculations by reducing the PCS source flow used as an input to the calculations by the amount the water film model predicts to run off the containment shell based on an assumed 4 as discussed below. This reduced flow is defined as the " evaporation limited flow." Using this " evaporation limited flow" as an input to the WGOTHIC code, the WGOTHIC code will calculate the applied flow to completely evaporate.

Basic Methodology The input to the calculational scheme to calculate the input film flow rate to WGOTHIC such that the total evaporation is consistent with the preceding simple model is determined as follows; 1.

An average evaporation heat flux, $n, at selected time (s) is determined for the wet WGOTHIC climes below the lower weir. The evaporation mass flux is $y = &n/h.

g 2.

The runoff, rnorr is calculated for each time using Equations 6 and 13 for problems with constant evaporation mass flux, or Equations 7 and 14 for problems with variable 1

8 l

evaporation flux.

3.

The runoff, morr, is subtracted from the water source, mas, and the difference is available for input to WGOTHIC, thereby assuring that WGOTHIC predicts limited evaporation of PCS water.

4.

WGOTHIC is then run with the modified source input and the calculated results are used to defme $n for input to Step 1 to recalculate runoff.

When the WGOTHIC calculated values of $n are consistent with and slightly higher than the values assumed for input under Step 1, the solution is converged.

Inclusion of 2-Dimensional Conduction Effects At a given containment pressure, the benefit (increased evaporation of applied PCS flow from the outside surface of the containment shell) calculated for inclusion of 2-dimensional heat conduction is dependent upon the wetted width of the regularly spaced vertical stripes created by the water distribution system at reduced PCS flow rates. Consequentially, the film evaporation rate is also a function of the stripe width. Thus, the calculation of the width of the film stripe is accomplished by iteration.

Accounting for 2-dimensional conduction through the containment shell increases the evaporation at a given containment pressure. The change in evaporation with change in wetted region has been expressed as the ratio of the evaporation rate for a wet stripe versus the wetted fraction of the sidewall (W/W ), where W is the containment sidewall perimeter, o

o compared to the evaporation rate with only radial heat conduction. The function is:

2.6694 - 5.6293

+ 8.9047

- 7.0263

+ 2.0785 (16)

M

=

where M is a multiplier applied to the one-dimensional calculations. The value, M, for a given containment wetted fraction represents the increase in evaporation rate per unit area l.

resulting from accounting from 2-dimensional (radial and circumferential) heat transfer over j

that calculated for the one-dimensional (radial only) case.

I l

l The function defined in equation 16 has been evaluated to be applicable over a containment i

pressure range of 10 to 25 psig.

Application of Evaporation Multipliers During the initial high-flow PCS period, water coverage is high (~90% coverage) and two-dimensional effects are small. However, when PCS flow is initially reduced from the high flow value of 442 gpm to 123-110 gpm, coverage of the containment shell is predicted to be

')

s 4p"

reduced to about 50%. Thus, it is from this time forward that the multiplier for two-dimensional conduction is first applied to evaporation rates.

4.0

SUMMARY

The method used to account for two dimensional heat conduction in the containment shell to liquid stripes and the methodology used to calculate the evaporation limited PCS flow at a fixed evaporation rate, $u, have been described. The two-dimensional conduction through the containment shell provides for increased evaporation rate of the PCS applied liquid. resulting in an overall benefit to the predicted heat rejection rate of the PCS.

10

5.0 REFERENCES

1) WCAP-13960; AP600 Doc. No. PCS-T2R-019, Rev. O,12/93; PCS Water Distribution l

Phase 3 Test Data Report, by J. Gilmore.

2) WCAP-14135; AP600 Doc. No. PCS-T2R-032, Rev.1,4/97; Final Data Report for Large Scale Tests Phase 2 and Phase 3, by F. E. Peters.
3) A. Forgie, J. Narula, R. Ofstun, D. L. Paulsen, S. K. Slabaugh, M. Sredzinski, D. R.

Spencer, J. Woodcock, "WGOTHIC Application to AP600", WCAP 14407, Westinghouse Electric Corporation.

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