ML16256A445
| ML16256A445 | |
| Person / Time | |
|---|---|
| Site: | Waterford  |
| Issue date: | 08/25/2016 |
| From: | Entergy Operations |
| To: | Office of Nuclear Reactor Regulation |
| Shared Package | |
| ML16256A115 | List:
|
| References | |
| W3F1-2016-0053 | |
| Download: ML16256A445 (70) | |
Text
WSES-FSAR-UNIT-3 9.1-1 Revision 304 (06/10) 9.0 AUXILIARY SYSTEMS
9.1 FUEL STORAGE AND HANDLING
9.1.1 NEW FUEL STORAGE
9.1.1.1 Design Bases
The new fuel storage racks are designed for the storage of new fuel assemblies prior to loading them into the core. The new fuel storage racks are designed to:
a) store 80 fuel assemblies (more than 1/3 of a core),
b) store new fuel assemblies with new control element assemblies (CEAs) inserted, (EC-18742, R304) c) provide a geometrically safe c onfiguration, resulting in a k eff of 0.95 or less, assuming flooding with uniform density cold clean water with no credit taken for the steel structure, and (EC-18742, R304) d) maintain a subcritical array, with the assu mption in c), under all design loadings, including the safe shutdown earthquake.
The racks and their associated anchorages are designed to maintain the minimum allowable fuel
spacing, to support the contained fuel assemblie s without damaging them and to allow for subsequent fuel assembly removal for the following conditions (in addition to thermal expansion loads and the dead loads of the fuel assemblies with CEAs):
a) the impact load resulting from a fuel assembly drop, or
b) loads resulting from seismic disturbances (safe shutdown earthquake or operating basis earthquake).
For an operating basis earthquake (OBE) or a safe shutdown earthquake (SSE), racks are designed for simultaneous loads from horizontal and vertical seismi c accelerations which are obtained from the floor response spectra curves.
9.1.1.2 Facilities Description
(DRN 01-692, R11-A)
New fuel assemblies arrive on-site in shipping c ontainers. Upon receiving the shipping containers, personnel use the fuel handling crane to lift each shippi ng container up to the +46 ft. level of the Fuel Handling Building. On +46 ft., personnel remove the new fuel from each container for an inspection.
Once finding that the fuel meets the inspection acc eptance criteria, they place the new fuel assemblies into the locations that the Special Nuclear Material s Transfer Report specifies, usually a vertical rack location in the spent fuel pool. New fuel can also be stored in a separate dry fuel storage vault. The remainder of this FSAR section describes the dry storage vault.
(DRN 01-692, R11-A)
The dry racks are in the 27.5 ft. by 29.25 ft. by 22.0 ft. hi gh new fuel concrete vault located west of the spent fuel storage pool (FSAR Figures 1.2-15 and 1.2-16). The vault side walls restrain dry rack lateral
motion.
WSES-FSAR-UNIT-3 9.1-2 Revision 304 (06/10)
The vault base slab (at elevation +24.00 ft. MSL) suppor ts the weight of the dry racks. Note the racks actually rest on a two inch redwood floor deck inside the vault, built on top of the base slab.
The fuel storage racks consist of vertical storage cells, grouped in parallel rows, such that fuel assemblies are removed from the top. The storage racks are divided into two units, each consisting of a
uniform four by 10 array. Each fuel assembly has a design minimum edge-to-edge spacing of 12 in. or a center-to-center spacing of 21 in.
The rack dimensions are such that no portion of any fuel assembly, with a control element assembly installed, will project out of the rack. The depth of the individual cells is 190 in. The cell openings are 8 15/16 in. x 8 15/16 in. at the lateral support points.
The individual new fuel assemblies are supported axia lly by the lower end fitting of the assembly. The seating surface is designed to prevent damage of the alignment pins or positioning surfaces.
The fuel assembly lateral restraints are located adjac ent to fuel grids and/or fuel end fittings. The length of these restraints provides adequate support and guidance for the new fuel assembly during insertion
and removal, to prevent any direct l oading or rubbing on the new fuel rods.
Provisions are made to allow lifting of the rack modules for possible removal.
Material stresses determined by combining the dead load and the OBE seismic loading do not exceed
the AISC allowable stresses. Material stre sses determined by combining the dead load and the SSE seismic loading do not exceed 90 percent of yield stress or 90 percent of critical buckling stress of the materials, as applicable. Shear yield stress is taken as 58 percent of tensile yield stress.
Stress comparisons are as follows:
a) Impact load resulting from a fuel assemb ly drop on 0.25 in. checkered plate cover, (EC-18742, R304) actual fb = 24.07 KSI < 27 KSI Fb allowable (EC-18742, R304) where fb = bending stress
Fb = allowable bending stress
b) Most critically stressed member due to a se ismic occurrence (bottom rack strut C8 x 11.5),
actual fa = 4.6 KSI < 5.3 KSI Fa allowable
where fa = compressive stress WSES-FSAR-UNIT-3 9.1-3 Revision 304 (06/10) c) Most critically stressed member due to a seismic occurrence (to grid member W8 x 17), 019620..Fby fby Fbx fbx where: fbx = bending stress about x-x axis
fby = bending stress about y-y axis
Fbx = allowable beading stress about x-x axis
Fby = allowable bending stress about y-y axis
d) Seismic supports transferring seis mic loads from racks to wall:
actual P = 4.9 kips < 16.7 kips allowable (for one in. diameter extra strong pipe)
actual P = 4.9 kips < 17.8 kips allowable (for A325 0.75 in.
diameter bolt)
where P = seismic load
9.1.1.3 Safety Evaluation
The racks are designed to provide protection against damage to the new fuel and to prevent new fuel assemblies from being inserted in other than prescri bed locations. Above each new fuel storage cell is a one-quarter in. checkered plate hinged cover. In order to place the new fuel in a storage cell, the checkered plate hinged cover of the storage cell mu st be opened and the new fuel lowered by the cask crane auxiliary hook. By keeping all the other hi nged covers closed and having fixed one-quarter in.
checkered plate over all areas between these hinged covers, new fuel assemblies are prevented from being inserted in other than prescribed locations.
(EC-5000082411, R301; EC-18742, R304)
Criticality design calculations have been perform ed (Reference 5) and consider the effects of manufacturing tolerances in the rack, wear of the racks over their design life and uncertainty of fuel assembly position in the racks.
(EC-5000082411, R301)
Sufficient margin to criticality is maintained under a ll conditions for the storage of new fuel assemblies of maximum enrichment (5.0 weight percent U-235 in UO 2). Specifically, analyses have been performed which confirm that a keff of less than 0.98 would exist for storage of 5.0 weight percent enriched fuel in optimum moderation conditions. (EC-18742, R304)
The new fuel storage racks are designed in accordance with the following:
a) AISC - Specification for the De sign, Fabrication and Erection of Stru ctural Steel for Building, July 1970 WSES-FSAR-UNIT-3 9.1-4 Revision 306 (05/12) b) American Society of Mechanical Engineers (ASME) 1974 Edition, up to and including the Summer 1976 addenda: ASME Section II, Material Specifications ASME Section IX, Welding Qualifications
Fa = allowable compressive stress
c) American Society for Testing Material (ASTM) - ASTM A-167 Type 304 Standard Finish (1974)
d) American Welding Society-AWS Dl
.1-1972, Structural Welding Code (EC-18742, R304)
The racks are designed to safely withstand all exter nal loads and forces, (including a SSE) and transmit these loads and forces to the surrounding concrete v ault structure. Details of seismic designs are discussed in Section 3.7. The most severe force acti ng in either the east-west direction or the north-south direction are directly combined with the vertical force in the upward or the downward direction. (EC-14275, R306) 9.1.2 SPENT FUEL STORAGE IN THE FUEL HANDLING AND CONTAINMENT BUILDINGS (EC-14275, R306) 9.1.2.1 Design Basis (DRN 99-1097, R11, R11)
Fuel assemblies are stored underwater in high density top entry spent fuel st orage racks in the spent fuel pool, the spent fuel cask storage area and, after permanent plant shutdown, in the refueling canal.
The function of the spent fuel storage racks is to vertically support, physically separate and facilitate cooling of spent fuel assemblies with control elem ent assemblies inserted. The design of spent fuel storage racks precludes insertion of a fuel assembly in any other region except regions designated for fuel assemblies. (DRN 99-1097, R11, R 11; EC-18742, R304)
(EC-14275, R306)
There are four spent fuel storage racks, D, E, F, and G, and their respective storage pedestals, in the Cask Storage Area which must be removed in order for dry cask storage operations to proceed. An option is maintained for the spent fuel storage racks to be available for re-installation as needed. (EC-14275, R306)
The spent fuel storage racks are designed to: (DRN 99-1097, R11, R11) a) have storage positions for 2398 fuel assemblies; 1849 spaces in the spent fuel pool; 255 spaces in the spent fuel cask storage area; and 294 spaces in the refueling canal. (DRN 99-1097, R11, R11)
(EC-18742, R304) b) remain subcritical with a k eff of less than 1.0 assuming spent fuel is flooded with nonborated water, and (EC-18742, R304) c) maintain a subcritical array, with the assu mption of b), under all design loadings, including the safe shutdown earthquake. (DRN 99-1097, R11, R11)
(DRN 99-1097, R11, R11)
(EC-8884, R303)
The spent fuel storage racks are designed as a seismic Category I structure (Reference 6). The racks and their associated anchorages are designed to mainta in the minimum allowable fuel spacing, to support the contained fuel assemblies without damaging them (i.e., no fuel cladding rupture), to allow sufficient fuel cooling, and to allow subsequent fuel assembly removal for the following conditions, (in addition to thermal expansion loads of the fuel assemblies with CEAs and the fuel pool water):
a) the impact load resulting from a fuel assembly (with CEA) being dropped in the vertical position from the maximum height it can be lifted above the racks (approximately 18 ft. from the bottom of the fuel assembly to the bottom of pool) (References 6 and 7), (EC-8884, R303) b) loads resulting from seismic disturbances (SSE and OBE), or WSES-FSAR-UNIT-3 9.1-5 Revision 306 (05/12) c) maximum uplift loads of 5000 lbs. that can be produced by the spent fuel handling machine.
9.1.2.2 Facilities Description (DRN 99-1097, R11, R11)
The spent fuel storage racks are located in the spent fuel storage pool, the spent fuel cask storage area and, after permanent plant shutdown, the refueling canal of the Fuel Handling Building. The spent fuel pool is approximately 31'11" wide, 32'6" long, and 41'6" deep. The normal level of the water in the pool is at elevation +44'0". The bottom of the pool is at elevation +4'6". The spent fuel cask storage area is located adjacent to (on the West side of) the spent fuel pool. The spent fuel cask storage area is
approximately 13'1" wide, 14'9" long and 45'6" deep (the bottom is at elevation +0'6"). The refueling canal is located adjacent (on the West side of) the spent fuel cask storage area. The refueling canal is
approximately 5' wide, 36'6" long, and 41'6" deep (the botto m is at elevation 4'6"). To the North of the spent fuel cask storage area is the spent fuel cask decontamination area. Stainless steel liners are placed directly against the concrete to form the sides of the three regions (spent fuel pool, spent fuel cask storage area and refueling canal). The stainless steel floor liner plate is supported on a steel beam grillage, which in turn is supported by the concrete base. The entir e steel grillage is then completely grouted to the underside of the floor liner plate. The spent fuel pit liner is shown in Figure 9.1-2 and the location of the three regions, within the Fuel H andling Building, is shown in Figures 1.2-15 and 16. (DRN 99-1097, R11, R11)
A leak detection system is provided to monitor 100 perc ent of the pool liner welds. The system consists of a network of stainless steel angles attached to t he outside of the pool liner walls and floor by means of seal welds.
These monitor channels do not constitute part of the pool liner boundary but are water tight to the extent necessary to collect and isolate any leakage through the liner plate. In the event that one of the liner plate weld seams develops a leak, the liquid enter s the monitor channel system and flows to one of a number of collection points at the base of the pad. In this way, the leakage c an be traced to a specific area of the pool. The actual point of leakage c an be determined by pressurizing the leaking channel and looking for bubbles inside the pool. Each of the c hannels can be valved off in order to prevent further leakage from the pool.
(DRN 99-1097, R11; EC-14275, R306)
The spent fuel pool, spent fuel cask storage area and refueling canal are all designed to be flooded with borated water. The spent fuel ca sk decontamination area is designed to be a dry area (washdown of the spent fuel transfer cask only). The spent fuel pool can be separated from the spent fuel cask storage area with a removable, watertight gate (Gate #1), the spent fuel cask storage area can be separated from the refueling canal with a removable, wate rtight gate (Gate #2) and t he spent fuel cask storage area can be separated from the cask decontamination area with two removable, watertight gates (Gates
- 3A and 3B). Gate #3A is presently seal welded closed. The cask decontamination area is separated from the rail bay by a removable non-watertight gate (Gate #4). Administrative controls are in place to ensure that Gate #1 is not installed whenever spent fuel is stored in the s pent fuel cask storage area.
Administrative controls will be implemented, prior to installing storage racks in the refueling canal, to ensure that Gate #2 is not installed when s pent fuel is stored in the refueling canal. (DRN 99-1097, R11; EC-14275, R306)
The spent fuel racks are high density poison design shown in Figure 9.1-3. These racks are modular in
design with storage positions arranged in a square pa ttern. This honeycomb structure is inherently strong while providing large surface-to-surface beari ng areas that will provide internal friction damping during a seismic incident as an added margin of design conservatism.
Each rack assembly is made by joining a number of parallel rows of square box es. Each box contains one fuel assembly compartment and two poison a ssembly compartments. The compartments are arranged so that the fuel assembly compartments in a rack assembly are separated from one another by poison assembly compartments. Each box is fi tted with a bottom plate which supports the fuel assembly.
WSES-FSAR-UNIT-3 9.1-6 Revision 306 (05/12)
Openings through the bottom plate provide for water circulation through all three compartments. The design permits only one fuel assembly to be inserted into each storage location. (DRN 99-1097, R11; EC-18742, R304)
The spent fuel storage racks are free standing and go wall to wall in the spent fuel pool and spent fuel cask storage area. The spent fuel storage racks are grouped into two design styles, designated as Region 1 and Region 2. Both rack styles contain Boral as the acti ve neutron absorbing poison.
Boral consists of finely divided particles of boron carbide (B 4 C) uniformly distributed in type 1100 aluminum powder, clad in type 1100 aluminum and pressed and sintered in a hot-rolling pr ocess. Region 1 racks are located in the spent fuel cask storage area and have the capability to store 255 fuel assemblies in four separate rack modules.
Region 2 racks have the capability to store 1849 fuel a ssemblies in sixteen separate rack modules in the spent fuel pool and 294 fuel assemblies in five separat e modules in the refueling canal. Region 1 racks have a center to center spacing of 10.185 inch and Region 2 racks have a center to center spacing of 8.692 inch. (EC-18742, R304)
Each poison assembly compartment contains a pois on assembly. The neutron poison assembly consists of a sheet of Boral. (DRN 99-1097, R11)
The determined seismic response loads consider all degrees of fuel loading of the racks, including racks empty of any fuel, partially loaded with fuel, or filled wi th fuel with CEAs inserted. The effect of water within the rack cavities is considered. Floor response spectra curves are given in Subsection 3.7.2.
(DRN 99-1097, R11)
Material stresses determined by combining the dead load and OBE seismic loading do not exceed the ASME allowable stresses. (DRN 99-1097, R11)
(EC-18742, R304)
The spent fuel storage racks are constructed entirely of stainless steel. Thus, material compatibility between components of the spent fuel pool and the Zi rcaloy-4 clad fuel assemblies is established. (EC-18742, R304)
(DRN 99-1097, R11; EC -28458 R305; EC -30504, R305; EC-14275, R306)
The spent fuel storage pool is so located in the F uel Handling Building that no equipment, other than the spent fuel handling machine hoist and the cask crane auxiliary hoists will be able to be in both areas.
The main hoist on the Fuel Handling Building cask crane is able to access the cask decontamination area and the rail bay; and access the spent fuel cask storage ar ea with administrative controls. The accidental dropping of any heavy object by the spent fuel handli ng machine will be avoided by the stringent controls as described in Subsection 9.1.4. The auxiliary hoi sts of the cask crane will only be used to handle the poison assemblies of less than 200 pounds (including the we ight of the tool) during the surveillance test.
Heavier loads than 200 pounds may be lifted over the spent fuel pool and the spent fuel cask storage area. However, these lifts will be controll ed by site procedures and will meet the NUREG-0612 requirements. Regulatory Guide 1.13, Spent Fuel Storage Facility Design Basis, is discussed in Subsections 9.1.3 and 9.1.4.
(DRN 99-1097, R11; EC -28458 R305; EC -30504, R305; EC-14275, R306)
Radiological considerations are discussed in Subsecti on 12.3.1.9. Ventilation is provided in this area as discussed in Subsection 9.4-2.
9.1.2.3 Safety Evaluation (DRN 99-1097, R11; EC-18742, R304)
The center-to-center spacing between fuel assemblies in the Region 1 racks is such as to maintain the array subcritical with a k eff of less than 1.0 when fully loaded with assemblies (without CEAs) of maximum enrichment of 5.0 w/o U-235 in UO 2 , without regard to fuel burnup, when flooded with pure water, and less than 0.95 with 85 ppm soluble boron. The R egion 2 racks have a minimum burnup requirement of 34,100 MWD/MTU for unrestricted fuel storage of asse mblies at an initial enrichment of 5.0 w/o U-235 (and meeting the same criticality design criteria as the Region 1 racks). Fuel assemblies not meeting the minimum burnup requirements may also be stored in R egion 2 utilizing a checkerboard storage pattern of either (1) new fuel and empty cells or (2) fuel of 27 MWD/MTU burnup with fuel of lower reactivity. Region 1 may also be used for storage of fuel assemblies not meeting the minimum burnup requirements established for Region 2. The racks, which compri se Regions 1 and 2, have Boral absorbers which have been sized to fully shadow the active fuel height of a ll fuel assembly designs stored in the pool. This design condition is maintained during all design l oadings described above. The Region 2 racks will (DRN 99-1097, R11; EC-18742, R304)
WSES-FSAR-UNIT-3 9.1-7 Revision 306 (05/12)
(DRN 99-1097, R11; EC-5000082411, R301; EC-18742, R304) maintain a subcritical array with a k eff less than 1.0 when flooded with pure water, and a k eff less than 0.95 with 524 ppm soluble boron. The soluble boron requirement to ensure a k eff less than 0.95 in the Region 1 and Region 2 racks under all accident conditions is 870 ppm.
Criticality analyses were also performed for Region 2 to establish requirements for the interfaces between
contiguous sub-regions containing different loading c onfigurations. No restrictions are necessary between a uniform loading pattern and either of the c heckerboard loading patterns, fresh or irradiated.
For interfaces between the fresh fuel checkerboar d and the irradiated fuel checkerboard, the high-reactivity irradiated assembly (e.g., 27 GWD/MTU) may be face-adjacent to no more than one fresh fuel assembly; each fresh fuel assembly may be face-adjac ent with up to two high-reactivity irradiated fuel assemblies.
The criticality design calculations were perform ed (References 1 and 4) using the MCNP and CASMO-4 codes. The calculations considered the effects of manuf acturing tolerances in the racks, variation in fuel pool water density and uncertainty of fuel assembly pos ition in the racks. The fuel assembly parameters used in the criticality analysis are described in Tabl e 9.1-8. Since the rack design meets the required seismic criteria, a seismic event will not alter k eff. (DRN 99-1097, R11; EC-5000082411, R301; EC-18742, R304)
The governing codes used in the design of t he spent fuel storage racks are as follows: (DRN 99-1097, R11)
A. Design: The Spent Fuel Storage Racks are des igned in accordance with the stress limits of ASME,Section III, Subsection NF for linear type supports (1996 Edition). The ASME Code Stamp is not required. Minimum fillet weld sizes have not been limited by the criteria of ASME Section Ill, Subsection NF (NF-3324.5d). B. Fabrication: The Spent Fuel Storage Ra cks have been fabricated in accordance with ASME,Section III, Subsection NF (1996 Edition).
The ASME code stamp is not required. The racks have been fabricated under a 10CFR50 Appendix B program. C. Materials: All material, including welding fille r material, conforms to the requirements of Section II of the ASME Boiler and Pressure Vessel Code (1996 Edition). Requirements of
10CFR50 Appendix B apply. D. Welding: Welders and welding procedures were qualified in accordance with Section IX of the ASME Boiler and Pressure Vessel Code (1996 Edition). Welding requirements of ASME
Section III, Subsection NF, Subarticles NF
-4300 and NF-4400 apply to the fabrication and installation of the Spent Fuel Storage Ra cks. The ASME code stamp is not required. E. Visual Examination: All welds were gage checked and visually examined in accordance with ASME Section III, Subsection NF, Subar ticle NF-5360. Personnel qualification and certification were in accordance with Subarticle NF5520. F. Nondestructive Examination: All pedestal to baseplate welds and all fillet welds greater than 3/8" have been subjected to liquid penetrant exami nation in accordance with the following: (1) Liquid penetrant examinations were per formed in accordance with ASME Section V, Article 6 (1996 Edition). (2) Liquid penetrant examination acceptanc e standards were in accordance with ASME Section III, Subsection NF, Subarticle NF-5350. (3) Personnel qualification and verification were in accordance with ASME Section III, Subsection NF, Subarticle NF-5520. (DRN 99-1097, R11)
(EC-22227, R304)
G. Criticality Accident Requirements: Code of F ederal Regulations, 10 CFR 50.68, with credit taken for soluble boron, in compliance with 10 CFR 50.68(b). (EC-22227, R304)
The spent fuel storage racks are protected agai nst the design wind loadings and tornado-generated missiles for the design tornado conditions specified in Section 3.3.
(EC-18742, R304)
A boric acid concentration of greater than or equal to 1900 ppm is maintained in the water. Spent fuel pool radiation dose levels are as discussed in Subsection 12.3.1.9.
(EC-18742, R304)
WSES-FSAR-UNIT-3 9.1-8 Revision 306 (05/12)
The spent fuel cavity and total rack design is such t hat each fuel assembly and CEA will be kept sufficiently cool by natural convection cooling water flow pas t the assembly as described in Subsection 9.1.3.
9.1.2.4 Temporary Fuel Storage
9.1.2.4.1 Design Bases The temporary fuel storage rack consists of one row of five stainless steel boxes which are designed to:
a) Store up to five (5) new or spent fuel assemblies in containment during refueling. (DRN 99-1097, R11; EC-18742, R304) b) Prevent inadvertent crit icality by ensuring that k eff is less than 0.95 under all moderation conditions for fuel of maximum expected enrichment of 5.0 weight percent, including conditions
of full flooding and low water density spray mist, as might be used for fire fighting. (DRN 99-1097, R11; EC-18742, R304) c) Provide sufficient cooling water to s pent fuel as required during refueling.
d) Shield the spent fuel adequately to comply with the zone criteria of Section 12.3.
e) Perform their function and maintain subcriticality during safe shutdown earthquake, tornado, hurricane and flood conditions.
9.1.2.4.2 Facilities Description The temporary fuel storage rack is located inside containment in the refueling pool. (EC-18742, R304)
This rack is a temporary storage location for up to five new or spent fuel assemblies during refueling.
New fuel assemblies may be stored wet or dry befor e being transferred into the core. Fuel may be stored temporarily during fuel shuffling; spent fuel assemblies may be stored temporarily before transfer to the spent fuel pool. (EC-18742, R304)
The temporary fuel storage rack consists of five cavi ties comprised of five square stainless steel cans spaced 18 inches apart center to cent er in a single row. Each can measures 8.8 inches on all four sides, and the steel is 0.093 inches thick on all sides.
The rack is attached to the primary shield wall.
Each of the storage cavities has openings to prov ide cooling for stored spent fuel assemblies.
9.1.2.4.3 Safety Evaluation (DRN 99-1097, R11; EC-18742, R304)
The rack is designed to maintain a subcritical array with a k eff of less than 0.95 when fully loaded with five assemblies of maximum enrichment (5.0 w/o U235 in UO 2). This includes moderation by both pure water flooding and by low water density spray mists as might be encountered in fire fighting. The structure of the rack assures t hat the minimum separation distanc e between fuel assemblies cannot be violated. No control element assemblies (CEAs) are assumed to be present in the fuel assemblies.
Criticality analyses are su mmarized in Reference 1. (DRN 99-1097, R11)
Standoffs prevent a suspended or dropped fuel assembly from coming close enough to fuel stored in the rack to result in a k eff greater than 0.95, even for maximum enric hment fuel. Nonetheless, criticality analyses were performed with a mislocated fuel assemb ly on the exterior of the temporary fuel storage rack, and showed that the soluble boron r equirement for this accident is 359 ppm.
Eight 1-1/2 inch diameter cooling holes (two per face) are located approximately six inches below the bottom plate supporting the fuel assembly. Each spent fuel assembly will be kept sufficiently cool by natural convection cooling water flow. (EC-18742, R304)
Structural stresses determined by combining the dead load with OBE seismic loading do not exceed the AISC allowable stresses. Structural stresses determined by combining the dead load and SSE seismic loading do not exceed 90 percent of yield stress or critical buckling stress of materials, as applicable.
The rack is designed to maintain its integrity after the impact of a fuel assembly dropped from the
maximum height of fuel lift.
WSES-FSAR-UNIT-3 9.1-9 Revision 305 (11/11) 9.1.3 FUEL POOL SYSTEM (SPENT FUEL POOL COOLING AND CLEANUP SYSTEM) 9.1.3.1 Design Bases
The Fuel Pool System is designed to: (DRN 99-1097, R11; 03-2063, R14;05-968, R14) a) remove the decay heat produced in the fuel fr om 2441 discharged fuel assemblies. The nominal reactor power to determine actual decay heat pr oduced from fuel assemblies discharged into the fuel pool is provided below:
Cycles 1 through 11 3390 MWt. Cycles 12 and 13 3441 MWt Cycle 14 and up to 2441 Assemblies 3716 MWt (DRN 99-2519, R11; EC-8477, R305) b) remove the decay heat produced in the fuel from a full core offload placed in the spent fuel pool after reactor shutdown, in addition to the dec ay heat from 2,224 previously discharged fuel assemblies (approximately 23 previous refueling batches). This is conservative because there will never be more than 2,104 assemblies in st orage. With one fuel pool pump operating and administrative controls in place that align the spent fuel pool cooling heat exchangers in parallel and limit the number of assemblies that may be offloaded based on time after shutdown, the maximum spent fuel pool temperature will not exceed 140 F meeting the normal maximum heat load temperature requirement. Refer to Figure 9.1-21. The fuel pool cooling loop is designed to seismic Category 1 requirements. The assumed single failure for a full core discharge is the failure of a divisional electrical bus whic h renders only one component cooling water pump and one fuel pool cooling pump available. (EC-8477, R305)
c) remove the decay heat produced in the spent f uel from approximately 108 assemblies of a core placed in the spent fuel pool after reactor s hutdown in addition to the decay heat from 2,332 previously discharged assemblies (approximately 24 previous refueling batches). With one fuel pool pump operating, and administrative controls in place that limit the number of assemblies that may be offloaded based on time after shutdown, the maximum spent fuel pool water temperature will not exceed 140 F. Refer to Figure 9.1-22. The assumed single failure for a partial core discharge is the failure of a divisional electrical bus which takes out a redundant train of cooling water pumps. (DRN 99-1097, R11, 99-2519, R11;05-968, R14)
d) remove soluble and insoluble foreign matter from the spent fuel pool water and dust from the pool surface through use of the purification portion of the Fuel Pool System. This maintains the fuel pool water purity and clarity, permitting visual observation of underwater operations.
e) minimize the continuous radiation dose levels in working areas around the fuel pool to less than 2.5 mrem/hr. by maintaining at least 23 ft of wate r over the stored spent fuel assemblies. This also ensures that the offsite dose consequences due to a postulated fuel handling accident are acceptable. To ensure the water level is mainta ined in the spent fuel pool, a seismic category I makeup system is provided from the condensat e storage pool. A backup system is also provided with a seismic category I makeup water source, the refueling water storage pool. Also, all connections to the spent fuel storage pool are made so as to preclude the possibility of
siphon draining the pool. (DRN 99-1097, R11) (DRN 03-2063, R14)
The thermal-hydraulic analysis is given in Reference 2. (DRN 99-1097, R11)
WSES-FSAR-UNIT-3 9.1-10 Revision 305 (11/11) 9.1.3.2 System Description
The piping and instrument diagram of the Fuel Pool System is shown in Drawing G169. The system process flow data is shown in Table 9.1-1.
9.1.3.2.1 Fuel Pool Cooling Loop (DRN 99-1097, R11;00-691, R11-A; EC-8477, R305)
The cooling portion of the Fuel Pool System is a closed loop system consisting of two half capacity pumps and one full capacity heat exchanger. (The back up fuel pool heat exchanger will be available for use when the fuel pool heat exchanger is out of service and may be used to supplement heat removal during core offloads.) The fuel pool water is drawn from the fuel pool near the surface and is circulated by the fuel pool pumps through the fuel pool heat exchanger, where heat is rejected to the Component Cooling Water System. From the outlet of the f uel pool heat exchanger, (and/or backup fuel pool heat exchanger), the cooled fuel pool water is returned to the fuel pool at elevation +36'6". The cooling system is controlled from the CP-2, Reactor Control Panel. Main control room alarms for high fuel pool temperature, high and low liquid level in the fuel pool, low fuel pool pump discharge header pressure and high radiation in the fuel pool area are provided to alert the operator to abnormal circumstances. (DRN 99-1097, R11;00-691, R11-A; EC-8477, R305) 9.1.3.2.2 Fuel Pool Purification Loop (DRN 99-1097, R11)
The clarity and purity of the water in the fuel pool, refueling cavity, and refueling water storage pool are maintained by the purification portion of the Fuel Pool System. The purification loop consists of the fuel pool purification pump, ion exchanger filter and strainers. The purification flow is drawn from the pool at elevation +40'6". A basket strainer is provided in the purification line to the pump suction to remove any relatively large particulate matter. The screen size is 1/16 in. holes. The fuel pool water is circulated by the pump through a filter which removes particulates twenty microns or smaller in size, then through an ion exchanger to remove ionic material, and finally through a wye type strainer, which prevents resin beads from entering the fuel pool in the unlikely ev ent of ion exchanger retention element failure. A connection to the refueling water storage pool provides makeup to the fuel pool through the purification loop. In addition to purifying the spent fuel pool, t he refueling water storage pool and refueling cavity are also provided with connections to the purification loop.
Fuel pool water chemistry is given in Table 9.1-2. (DRN 99-1097, R11) 9.1.3.2.3 Component Description
The major components of the Fuel Pool System ar e described in this subsection. The principal component data is summarized in Table 9.1-3.
a) Fuel Pool Heat Exchanger
The fuel pool heat exchanger is a horizontal she ll and tube design with a two-pass tube side. A slight pitch, three degrees above the horizontal, is provided for complete draining of the heat
exchanger. The component cooling water circulates through the shell side. The internal wetted surface (tube side) is stainless steel.
b) Fuel Pool Purification Filter
The fuel pool purification filter is located upstr eam of the fuel pool ion exchanger to remove any particulates in the pool water. The nominal filter rating shall be 20 microns or smaller. Filters of reduced nominal rating will be used as required to maintain visual clarity in the fuel pool sufficient to verify fuel inventory. Due to possible buildup of high activity in the filter, the unit is designed and installed to provide for removal of the contaminated element assembly with
remotely operated handling equipment. The filter drains to the drain collection header in the Waste Management System. The internal wetted surface is stainless steel.
WSES-FSAR-UNIT-3 9.1-11 Revision 14 (12/05)c) Fuel Pool Ion Exchanger The fuel pool ion exchanger removes ionic matter from the water. Mixed bed resin is used withthe anion resin converted to the borate form and the cation resin in the hydrogen form. The units are provided with all connections required to replace resins by sluicing. The ion exchanger contains a flow distributor on the inlet to prevent channeling of the resin bed and a resin retention element on the discharge to preclude discharge of resin with the effluent. The internal
wetted surface is stainless steel. d) Fuel Pool Purification Pump Suction Strainer The fuel pool purification pump suction strainer prevents any relatively large particulates (>1/16in.) from entering the purification pump. The internal wetted surface is stainless steel. e) Fuel Pool Ion Exchanger Strainer The wye strainer removes resin fines from the purification flow. Blowdown is directed to thespent resin tank in the Waste Management System. The internal wetted surface is stainless
steel.f) Fuel Pool Pumps There are two fuel pool pumps installed for parallel operation. Under normal operatingconditions one pump is operational. The fuel pool pump(s) may be infrequently secured to allow work to be performed in the spent fuel pool or to allow maintenance to be performed on the Fuel Pool Cooling System. The pumps are provided with mechanical seals. To increase seal life and reduce maintenance, the seals are cooled by circulating a portion of the pump discharge flow to
the seals which returns to the pump suction. The seals are provided with leakoff vent and drain
connections. The internal wetted surface is stainless steel. g) Fuel Pool Purification Pump The fuel pool purification pump is used for purification and skimming operations. Mechanicalseals minimize shaft leakage. To increase seal life and reduce maintenance, the seals are cooled by circulating a portion of the pump discharge flow to the seals which returns to the pump
suction. The seals are provided with leakoff vent and drain connections. The internal wetted
surface of the pump is stainless steel. h) Refueling Water Pool Purification Pump The refueling water pool purification pump takes its suction from the refueling water storage pool and discharges into the fuel pool, or back to the refueling water storage pool after passing through the fuel pool ion exchanger. Mechanical seals minimize shaft leakage. The seals are cooled by circulating a portion of the pump discharge flow to the seals which then flows to the pump suction. The internal wetted surface of the pump is stainless steel.
WSES-FSAR-UNIT-3 9.1-12 Revision 14 (12/05)i) Refueling Canal Drain Pump (DRN 99-1097, R11) The refueling canal drain pump is used for draining the refueling canal, and spent fuel caskdecontamination pit. This pump discharges into the fuel pool. Mechanical seals minimize shaft leakage. Seals are cooled by circulating a portion of the pump discharge flow to the seals which then flows to the pump suction. This cooling increases seal life. The internal wetted surface is
stainless steel. (DRN 99-1097, R11)j) Refueling Cavity Drain Pump The refueling cavity drain pump is a non-safety, centrifugal type and horizontally mounted pump.It draws suction from the refueling cavity and discharges water to the refueling water storage pool. This operation is needed during post refueling operation when the water in the refueling cavity has to be completely drained. In case, however, the water chemistry does not permit draining of refueling cavity water directly to the RWSP, the operator has the option to first purify this water via the fuel pool ion exchanger and then discharge to the RWSP. The refueling cavity drain pump is designed to meet these requirements. The internal wetted surface of the pump is
stainless steel. (DRN 99-1097, R11)k) Piping and Valves All the piping used in the Fuel Pool System is stainless steel with welded connectionsthroughout, except for flanged connections installed at the suction and discharge of the pumps, at strainer housings and at locations required for hydro testing. All the valves in the Fuel Pool System are stainless steel, 150 lb. class.
l) Backup Fuel Pool Heat Exchanger This heat exchanger is a horizontal shell and tube design with a two-pass tube side.Component Cooling Water circulates through the shell side. The internal wetted surface (tube
side) is stainless steel. (DRN 99-1097, R11)9.1.3.2.4 Instrumentation Requirements 9.1.3.2.4.1 Temperature Instrumentation a) Fuel Pool Temperature Fuel pool temperature indication is provided locally and a high temperature alarm is actuated inthe main control room to warn the operator of a system malfunction. b) Fuel Pool Heat Exchanger Inlet Temperature Local indication of heat exchanger inlet temperature (tube side) is provided. This indication, inconjunction with the heat exchanger outlet temperature, will serve as a measure of heat
exchanger performance. c) Fuel Pool Heat Exchanger Outlet Temperature Local indication of heat exchanger outlet temperature (tube side) is provided. This indication, inconjunction with the heat exchanger inlet temperature, will serve as a measure of heat
exchanger performance. 9.1.3.2.4.2 Pressure Instrumentation WSES-FSAR-UNIT-39.1-13a)Fuel Pool Pump Discharge PressureThe discharge pressure of each fuel pool pump is indicated locally.b)Fuel Pool Pumps Discharge Header PressureA discharge header pressure switch for the fuel pool pumps serves to actuate a low pressurealarm in the main control room to warn the operator of system malfunction.c)Fuel Pool Purification Pump Suction PressureThe suction pressure of the fuel pool purification pump is indicated locally. This indication, inconjunction with the purification pump discharge pressure gage, will serve as a measure of purification pump performance.d)Fuel Pool Purification Pump Discharge PressureThe discharge pressure of the fuel pool purification pump is indicated locally. This indication, inconjunction with the purification pump suction pressure gage, will serve as a measure of purification pump performance.e)Purification Filter and Combined Ion Exchanger Strainer Differential PressureThe differential pressure of the purification filter and the combined ion exchanger and outletstrainer is indicated locally. Periodic readings of these instruments will indicate any progressiveloading of the units.f)Refueling Canal Drain Pump Discharge PressureThe discharge pressure of the refueling canal drain pump is indicated locally.9.1.3.2.4.3Level Instruments a)Fuel Pool LevelThe fuel pool water level is monitored by a level switch. This switch actuates a high and a lowalarm locally and in the main control room to warn the operator of a system malfunction and trips the pumps. This satisfies a requirement of Regulatory Guide 1.13 (3/71) that monitoringequipment be provided to alarm locally and in a continuously manned location if the water level inthe fuel pool falls below a predetermined level.
WSES-FSAR-UNIT-3 9.1-14 Revision 14 (12/05)9.1.3.3 Safety Evaluation All connections to the spent fuel storage pool are made so as to preclude the possibility of siphon draining of the pool. Any leakage from the Fuel Pool System is detected by reduction in pool water inventory. Makeup to the spent fuel storage pool is from the seismic Category I refueling water storage pool and/or the condensate storage pool. The refueling water pool purification pump, which provides makeup from the refueling water storage pool has a capacity of 150 gpm which exceeds normal system leakage and evaporation losses. The component cooling water makeup pumps provide makeup from the condensate storage pool and have a capacity of 600 gpm, also exceeding normal system leakage and evaporation. This design satisfies the requirements of Regulatory Guide 1.13 (3/71) for a seismic Category I makeup system and backup source of makeup water. A sump, with adequate capacity, is provided to collect system leakage. A high level alarm is provided to annunciate in the main control
room when a high sump level is reached. (DRN 99-1097, R11; 03-2063, R14)The failure of portions of the spent fuel pool cooling systems, or of other systems not designed to seismic Category I standards, which are located close to essential portions of the system, will not preclude essential functions. The failure mode and effects analysis is presented in Table 9.1-4.
Although it is unlikely that all cooling could be lost to the spent fuel storage pool, it would take
approximately 2.89 hours0.00103 days <br />0.0247 hours <br />1.471561e-4 weeks <br />3.38645e-5 months <br /> for the bulk pool temperature to rise from 152°F to 212°F. This is based on a
full core offload discharged starting three days after reactor shutdown. The corresponding heat load is
51.5 x 10 6 Btu/hr. This time period allows sufficient time for the operators to intervene and line up an alternate source of replenishing the pool inventory and removing the decay heat. (DRN 99-1097, R11; 03-2063, R14)9.1.3.4 Inspection and Testing Requirements Each component is inspected and cleaned prior to installation into the system. Demineralized water is then used to flush the entire system. The system is operated and tested initially with regard to flow paths, flow capacity, and mechanical operability. Instruments are calibrated and alarm functions are
checked for operability and setpoints during testing. Data is taken periodically during normal plant operation to confirm heat transfer capabilities, purification efficiency, and component differential pressures.
In-service inspection will be performed during the plant life in accordance with ASME Code Section XI as discussed in Subsection 6.6.2.
WSES-FSAR-UNIT-3 9.1-15 Revision 306 (05/12) 9.1.4 FUEL HANDLING SYSTEM
9.1.4.1 Design Bases
9.1.4.1.1 System
The Fuel Handling System is designed for the handling and storage of fuel assemblies and control element assemblies (CEAS) and for the required assembly, disassembly, and storage of reactor internals. As appropriate, the fuel handling equipment includes interlocks, travel limiting features, and
other protective devices to minimize the possib ility of inadvertent damage to a fuel assembly and potential fission product release, resulting from either mishandling or equipment malfunction.
The refueling water provides the coolant medium dur ing spent fuel transfer. The spent fuel pool is provided with a cooling and cleanup system which is discussed in detail in Subsection 9.1.3.
All spent fuel transfer and storage operations ar e designed to be conducted underwater to insure adequate shielding during refueling and to permit visual c ontrol of the operation at all times. The Fuel Handling System also provides for the disassemb ly, handling and reassembly of the reactor vessel closure head.
The general arrangement of the Fuel Handling System is shown in Figure 9.1-5.
9.1.4.1.2 Fuel Handling Equipment
The principle design criteria for the fuel and CEA handling equipment (refueling machine, fuel transfer equipment, spent fuel handling machine, and new fuel elevator) are as follows:
a) For nonseismic operating conditions, the bridges, trolleys, hoist units, hoisting cable, grapples and hooks conform to the requirements of Cr ane Manufacturing Association of America Specification #70 (1975). All other components meet the requirements of "Manual of Steel Construction", American Institute of Steel Cons truction, 7th Edition (1970) through Supplement
- 3.
b) For seismic design, the combined dead loads, live loads and seismic loads do not cause any portion of the equipment to disengage from its s upports and fall into the pool. The dead weight, live and SSE seismic loadings are combined in calculating material stress.
c) Grapples and mechanical latches which carry fuel assemblies or CEAs are mechanically interlocked against inadvertent opening.
(EC-35729, R306) d) External fasteners and parts used in equipment over the refueling or spent fuel pool are provided with a locking mechanism or a restraint, e.g. lockwire, thread sealant, or other suitable restraint. (EC-35729, R306)
WSES-FSAR-UNIT-3 9.1-16 Revision 306 (05/12) e) A positive mechanical stop prev ents the fuel from being lifted above the minimum safe water cover depth and will not cause damage or distortion to the fuel or the refueling machine when engaged at full operating hoist speed.
f) The fuel hoists are provided with load measuring devices and interlocks to interrupt hoisting if the load increases above the overload setpoint and interrupt lowering if the load decreases
below the underload setpoint.
g) In the event of loss of power, the equipment, and its load will remain in a safe condition.
h) Equipment remaining within the containment are capable of withstanding, without damage, the internal building test pressure.
i) Interlocks are provided to ensure the readi ness of system components, to simplify the performance of sequential operations, and to limit travel and loads such that design conditions will not be exceeded. In no case are interlocks us ed to prevent inadvertent criticality or the reduction of the minimum water coverage for personnel protection. No single interlock failure
results in a condition which will allow equipment malfunction damage to the fuel or the reduction of shielding water coverage. Where requir ed, redundant switches, mechanical restraints and physical barriers are employed.
j) The fuel handling and CEA machines do not fall within the definition of an overhead or gantry crane as described in OSHA Subpart N, Ma terials Handling and Storage, of 29CFR1910, Section 1910.179. However, considerable im portance has been attached to meeting the standards as well as operator, equipment, and facility safety.
9.1.4.1.3 Containment Polar Crane and Cask Crane
The containment polar crane is designed as a seismic Category I structure with a main hook capacity of 200 tons and an auxiliary hook capacity of 30 tons.
The primary function of the polar crane is to remo ve the reactor vessel head and place it in its stored position. (EC-14275, R306)
The Fuel Handling Building cask crane is designed as a seismic Category I structure with a main hook capacity of 125 tons and two auxiliary hooks, each with a capacity of 15 tons. T he primary functions of the cask crane are to place the new fuel into the new fuel storage racks, transfer the new fuel to the new fuel elevator and move the empty or loaded spent fuel transfer casks between the cask storage area and the rail bay. (EC-14275, R306)
(EC-14270, R305)
For the two cask crane auxiliary units and polar crane normal operating conditions, the bridges, trolleys, hoist units, hoisting cable, and hooks conform to t he requirements of Crane M anufacturing Association of America Specification #70 (revised 1975 Edition).
All other components meet the requirements of "Manual of Steel Construction", American Institute of Steel Construction (July 1970 Edition). Shop welding is in accordance with the requirements of AWS D1.1-1975 edition.
The Fuel Handling Building cask crane main tro lley has been upgraded with ASME NOG-1 to meet all qualifications for a single-failure-proof crane. T he upgraded crane meets the single-failure-proof criteria of NUREG 0554 and NUREG 0612 as applicable for the modi fication of an originally non single-failure-proof crane. The crane upgrades included a new replacem ent single-failure-proof main hoist & trolley designed and qualified in accordance with the appropria te requirements of ASME NOG-1. The retained cask crane bridge conforms to the requirements of Crane Manufacturing Association of America Specification #70 (revised 1975 Edition). Shop welding is in accordance with the requirements of AWS D1.1-1975 edition. (EC-14270, R305)
WSES-FSAR-UNIT-3 9.1-17 Revision 307 (07/13)
For seismic design, the combined dead loads and se ismic loads do not cause any portion of the equipment to disengage from its supports. The dead loads and seismic loadings are combined in calculating material stress.
(EC-44151, R307)
The crane assemblies and their supports are designed to safely withstand horizontal seismic loads acting simultaneously with vertical seismic loads. Vert ical seismic loads are c onsidered to act upward or downward to give the most severe combination. T he acceleration coefficients are considered to act at the dead load center of gravity of the cranes and tro lleys. Normal loads are defined as the dead load of crane and trolley. The bridge girder limit switch trip plate on the north end of the Fuel Handling Building crane is installed non-seismic. (EC-44151, R307)
All parts of both cranes are designed to resist the maximum stresses caused by any of the following conditions of loading:
a) dead load + live load + impact (15 percent of rated hook load)
b) dead load + live load + lateral thrust (10 percent of weight of loaded trolley) or longitudinal thrust (10 percent of max wheel loads)
c) rated breakdown torque of motors (275 percent of rated load)
d) collision with wheel stops
e) dead load (trolley at centerline span) + operating basis earthquake
f) dead load (trolley at centerli ne span) + design basis earthquake
For conditions a, b, d, and e members shall be desi gned in accordance with the basic allowable stresses of CMAA Spec. #70 (Revised 1975 edition).
For conditions c and f stresses shall not exceed 90 per cent of the elastic limit of the material.
(EC-14270, R305)
For a detailed description of the Cask and Polar cr anes, see Subsections 9.1.
4.2.2.14 and 9.1.4.2.2.15 and Tables 9.1-6 and 9.1-7. (EC-14270, R305)
9.1.4.2 System Description
9.1.4.2.1 System (EC-14275, R306)
The Fuel Handling System is an integrated system of equipment, tools and procedures for refueling the reactor. The system provides for handling and storage of fuel assemblies from receipt of new fuel to transfer of spent fuel to a dry storage cask or fr om a dry storage cask to the spent fuel pool. The equipment is designed to handle the spent fuel underwater fr om the time it leaves the reactor until it is placed in a canister for storage at the ISFSI. Underwater transfer of spent fuel provides a visually
transparent radiation shield, as well as a cooling m edium for removal of decay heat. Boric acid is added to the water in the quantity required to assu re subcritical conditions during refueling. (EC-14275, R306)
WSES-FSAR-UNIT-39.1-18Revision 10 (10/99)The major components of the system are the dual masted refueling machine with fuel and CEA handlingmasts, the fuel transfer equipment and the spent fuel handling machine. The refueling machine moves fuel assemblies into and out of the core and between the core and the transfer equipment. The CEA handling mast is used to move CEAs from one fuel assembly to another. The fuel transfer equipment moves the fuel between the Reactor Building to the Fuel Handling Building through the transfer tube.
The spent fuel handling machine handles fuel between the transfer equipment, the fuel storage racks in the spent fuel pool, and the spent fuel shipping cask.Special tools and lifting rigs are also used for disassembly of reactor components and are included in therefueling system. Major tools and servicing equipment required for refueling are listed in Table 9.1-5.
The major components of the Fuel Handling System are pictured in Figure 9.1-5. The seismic category and safety class are listed in Table 3.2-1.Where possible in the design of this equipment, mechanical stops and positive locks have been providedto prevent damage to or dropping of the fuel assemblies. In the design of the refueling machine, positive locking between the grapple and the fuel assembly is provided by the engagement of the actuator arm invertical channels in the hoist assembly. Relative rotational movement and uncoupling is not possible even with inadvertent initiation of an uncoupling signal to the actuator assembly. Therefore, failure of anelectrical interlock will not result in the dropping of a fuel assembly.For the Refueling Machine, the fuel hoist will stall at a load less than the allowable fuel assembly tensileload. The CEA Hoist will stall at a load less than the combined weights of a fuel assembly, CEA, and intervening Hoist components, such as the CEA hoist box and grapple assemblies.The following list identifies and defines the function of the interlocks contained in the fuel handlingequipment. Visual displays are not provided to directly inform the operator that an interlock is inoperative. However, in most cases a redundant device has been provided to perform the same function as the interlock or to present information to the operator allowing him to deduce that an interlock has malfunctioned.9.1.4.2.1.1Refueling Machine The following identifies and describes the functions of the key interlocks in the refueling machine.
a)Refueling Machine Hoist InterlockInterrupts hoisting of a fuel assembly or a CEA if the load increases above the overload setpoint.The hoisting load is visually displayed so that the operator can manually terminate the withdrawal operation if an overload occurs and the hoist continues to operate.b)Refueling Machine Hoist InterlockInterrupts hoisting of a fuel assembly or a CEA when the correct vertical position is reached. Amechanical up-stop has also been provided to physically restrain the hoisting of a fuel assembly or a CEA above the elevation which would result in less than the minimum shielding watercoverage.
WSES-FSAR-UNIT-3 9.1-19 Revision 301 (09/07) c) Refueling Machine Hoist Interlock
Interrupts insertion of a fuel assembly or CEA if the load decreases below the underload setpoint. The load is visually displayed so that the operator can manually terminate the insertion operation if an underload occurs.
d) Refueling Machine Hoist Interlock
Interrupts lowering of the hoist under a no-load c ondition when installing a fuel bundle or a CEA. The weighing system interlock is backed up by an independent slack cable switch which
terminates lowering under a no-load condition.
e) Refueling Machine Translation Interlock
Denies translation of the bridge and trolley while the fuel or CEA hoist is operating. An additional circuit is provided which, after initiation of a hoisting operation, requires that a
separate switch be actuated before normal operati on of the translation drives is possible.
f) Refueling Machine Hoist Interlock
Hoisting movement is denied during translation of the bridge and/or trolley. No backup or additional circuitry is provided for this interlock.
g) Refueling Machine Translation Interlock (EC-5000082257, R301)
Denies motion of the bridge and trolley with the spreader extended. T he underwater TV system can be used by the operator to determine whether the spreader has been raised, and a light on the control console indicates whet her it is withdrawn or extended. (EC-5000082257, R301) h) Refueling Machine Mast Anticollision Interlock
Stops translation of the bridge and/or trolley w hen collision ring on either mast is contacted and deflected.
Redundant switches are provided to minimize the possibility of this interlock becoming inoperative and slow bridge and trolley speeds ar e mandatory for movement of the refueling machine in areas other than its normal travel route which might contain obstructions. Travel
limits also restrict running t he mast into the pool wall.
i) Refueling Machine Hoist Speed Interlock
Provides restriction on maximum hoisting speed.
During insertion and withdrawal, the change in hoist speed can be monitored by observation of the hoist vertical position indicator. A c hange in the sound of the hoist will accompany the change in hoist speed. (EC-5000082257, R301)
When a fuel assembly is in a clear water area, the Refuel Machine Hoist can be operated in various speeds including maximum hoist speed. (EC-5000082257, R301)
WSES-FSAR-UNIT-3 9.1-20 Revision 301 (09/07) j) Refueling Machine Translation Interlock
Denies translation of the bridge and trolley wh ile they are over the core area and the upender, unless one hoist is at the up limit. Additiona lly, for operations between the core area and the upender, bridge and trolley translations are denied unless both hoists are at the up limit.
(EC-5000082257, R301)
(EC-5000082257, R301) 9.1.4.2.1.2 Transfer System
The following identifies and describes the functions of the interlocks in the transfer system.
a) Transfer System Winch Interlock
Terminates winching of the fuel carriage through the transfer tube if the load increases above the overload setpoint.
The winching load is visually displayed so that the operator can manually terminate the transfer operation if an overload occurs and the interlock fails. An overload is indicated by a light on the control panel and by an audible alarm.
b) Transfer System Winch Interlock
Prevents the winch from actuating with an upender in a vertical position. If this interlock fails and a transfer signal is initiated, winching will be terminated when the load increases above the
overload setpoint.
c) Transfer System Upender Interlock (EC-5000082257, R301)
Rotation of the upender is denied while the refue ling machine is at the upender station, unless the refueling machine hoist is at the up limit wi th a fuel assembly grappled or at a specified elevation with no fuel assembly grappled. (EC-5000082257, R301)
Failure of this interlock while the refueli ng machine is at the upender station will allow an upending signal by the transfer equipment operator at the station only to initiate rotation of the fuel carrier by the upender. In the event that th is signal is erroneously initiated and the interlock fails while the fuel assembly is being lowered fr om or raised into the refueling machine, the upender will distort the fuel assembly. However, the criterion which prohibits failure of more than one fuel assembly will be met.
d) Transfer System Upender Interlock
Rotation of the upender is denied unless the fuel carrier is correctly located for upending.
WSES-FSAR-UNIT-39.1-21Revision 8 (5/96)Failure of this interlock: (1) with the fuel carrier in the transfer tube, allow the upender to rotatewith no effect on the carrier or fuel bundle, and (2) with the fuel carrier partially in the upender, attempt to but not be successful in rotating the carrier since a mechanical lock prevents premature carrier rotation.e)Transfer Tube Valve InterlockContacts are provided in the control system of the transfer system which, when connected to alimit switch on the transfer tube valve, will prevent movement of the fuel carrier unless the valve is fully opened.If this interlock fails with the valve partially closed, the fuel carrier will contact the valve andwinching will be terminated by an overload signal. No damage to the fuel assembly will result since the fuel assembly is enclosed in the carrier.9.1.4.2.1.3Spent Fuel Handling MachineThe following identifies and describes the functions of the interlocks in the spent fuel handling machine.a)Spent Fuel Handling Machine Hoist InterlockInterrupts hoisting if the load increases above the overload setpoint. Since the spent fuelhandling tool is manually controlled by the operator, failure of the tool to move or reduction in tool speed as a result of an overload will be observed by the operator if the interlock becomes inoperative.b)Spent Fuel Handling Machine Hoist InterlockInterrupts lowering if the load decreases to cable slack.Since the tool is manually controlled, a slack cable condition can be visually determined by theoperator and lowering terminated.c)Spent Fuel Handling Machine Translation InterlockProvides speed restriction on bridge and trolley translation unless the load is in the full upposition, at which time fast speed is allowed.If this interlock fails, the mandatory slow speed restriction is removed. However, since thetranslation speed controls are infinitely variable, the operator can run at slow speed when theinterlock malfunction is recognized.d)Spent Fuel Handling Machine Translation InterlockWith the computer running, zone switches and encoder position feedback protect against runningthe load into walls or the gate of the storage area. Without the computer, only the zone switches provide the protection, WSES-FSAR-UNIT-39.1-22Zone switches protect against running the load into walls or the gate of the storage area.No backup or additional circuitry is provided for this interlock. However, the operator has directvision of the tool and the attached load so that translation can be terminated if an interlock fails to operate.e)Spent Fuel Handling Machine Translation InterlockHoisting movement is denied during translation of the bridge and/or trolley. No backup oradditional circuitry is provided for this interlock.9.1.4.2.1.4New Fuel Elevator The following identifies and describes the functions of the interlocks in the new fuel elevator.
a)New Fuel Elevator Hoist InterlockStops the elevator motor should the cable become slack.If this interlock fails the operator can stop the elevator motion from the spent fuel handlingmachine console.b)New Fuel Elevator Hoist InterlockPrevents raising of the elevator with a fuel assembly in the elevator box. This interlock is abackup for the administrative control which precludes the placement of a spent fuel assembly inthe new fuel elevator.9.1.4.2.2Components 9.1.4.2.2.1Dual Mast Refueling Machine The refueling machine is shown in Figure 9.1-6. The refueling machine is a traveling bridge and trolleywhich is located above the refueling pool and rides on rails set in the concrete on each side of the refueling pool.Motors on the bridge and trolley position the machine over each fuel assembly location within the reactorcore or fuel transfer carrier. The hoist assemblies and grappling devices are raised and lowered by cables attached to the hoist winches. After a fuel assembly or CEA has been raised into the refueling machine, the refueling machine transports the fuel assembly or CEA to its designated location.The controls for the refueling machine are mounted on a console which is located on the refuelingmachine trolley. Coordinate location of the bridge and trolley is indicated at the console by digital readout devices which are driven by encoders which are coupled to the guide rails through rack and pinion gears.
WSES-FSAR-UNIT-39.1-23 Revision 11-A (02/02)
During withdrawal or insertion of a fuel assembly or a CEA, the load on the hoist cable is monitored at theconsole to assure that movement is not being restricted. Limits are such that damage to the assembly is
prevented.Locking between the grapple and the fuel assembly or the CEA is provided by the engagement of thegrapple actuator arm in axial channels running the length of the fuel or CEA hoist assemblies. Therefore, it
is not possible to uncouple even with inadvertent initiation of an uncoupling signal to the actuator assemblies. The drives for both the bridge and the trolley provide close control for accurate positioning, and brakes are provided to maintain the position once achieved. In addition, interlocks are installed so that
movement of the refueling machine is not possible when the hoist is withdrawing or inserting a CEA or a fuel assembly. After operation of the hoist a console mounted interlock button must be actuated to allow
movement of the bridge or trolley.(DRN 00-691)
For operations at the core, the bottom of each hoist assembly is equipped with a spreading device to alignthe surrounding fuel assemblies or CEAs to their normal core spacing to assure clearance for fuel assemblies being installed or removed. An anticollision device at the bottom of each mast assembly prevents damage should the mast be inadvertently driven into an obstruction, and a positive mechanical up-
stop is provided to prevent a fuel assembly or a CEA from being lifted above the minimum safe water cover depth. A system of pointers and scales serves as a backup for the remote positioning readout equipment.(DRN 00-691)
Manually operated handwheels are provided for bridge, trolley and winch motions in the event of a powerloss. Manual operation of the grappling device is also possible in the event that air pressure is lost.
9.1.4.2.2.2 Transfer CarriageA transfer carriage as shown on Figure 9.1-5 conveys the fuel assemblies through the transfer tube. Twofuel assembly cavities are provided in the fuel carriage to reduce overall fuel handling time. After the
refueling machine deposits a spent fuel bundle in the open cavity, it only has to move approximately one ft.
to pick up the new fuel assembly which was brought from the Fuel Handling Building in the other cavity.
The handling operation in the Fuel Handling Building is similar. The dual cavity arrangement permits both fuel handling machines to travel fully loaded at all times. Fuel assemblies are placed on the transfer
carriage in a vertical position, lowered to the horizontal position, moved through the fuel transfer tube on the
transfer carriage, and then restored to the vertical position.Wheels support the carriage and allow it to roll on tracks within the transfer tube. The track sections at both ends of the transfer tube are mounted on the upending machines to permit the carriage to be properly positioned at the limits of its travel. The carriage is driven by wire rope cables connected to the carriage
and through sheaves to its driving winch mounted on the operating floor of the Reactor Building.The load in the transfer cables is displayed at the master control console. An overload will interrupt thetransfer operation. Manual override of the overload cutout allows completion of the transfer. The supports
for the replaceable rails on which the transfer carriage rides are welded to the 36 in. diameter transfer tube.
The rail assemblies are fabricated to a length which will allow them to be lowered for installation in the
transfer WSES-FSAR-UNIT-39.1-24Revision 13 (04/04)tube. No rails need be installed in the valve on the spent fuel pool side of the transfer tube.
9.1.4.2.2.3 Upending MachineAn upending machine as shown on Figure 9.1-5 is provided at each end of the transfer tube. Each consists of a structural support base from which is pivoted an upending straddle frame which engages the two-pocket fuel carrier. When the carriage with its fuel carrier is in position within the upending frame, the
pivots for the fuel carrier and the upending frame are coincident. Hydraulic cylinders, a ttached to both the upending frame and the support base, rotate the fuel carrier between the vertical and horizontal position as required by the fuel transfer procedure. Each hydraulic cylinder can perform the upending operation alone and can be isolated in the event of its failure. A long tool is also provided to allow manual rotation of the fuel carrier in the event that both cylinders fail or hydraulic power is lost.
9.1.4.2.2.4 Fuel Transfer Tube and ValveA fuel transfer tube extends through the containment wall. During reactor operation, the transfer tube is sealed by means of a blind flange located inside the containment. Prior to filling the refueling pool, the blind flange is removed. After a common water level is reached between the refueling pool and the spent fuel pool, the transfer tube valve is opened.
The procedure is reversed after refueling is completed.
The 36 in. diameter transfer tube is contained in a 48 in. diameter penetration (Figure 3.8-5) which is sealed to the containment.
The transfer tube and penetration sleeves are sealed to each other by welding rings and bellows-type expansion joints.The transfer tube valve is attached to the spent fuel pool end of transfer tube. The manual operator for the valve is designed to allow for movement of the valve due to thermal expansions and still permit operation.
The valve stem extends above the spent fuel pool water level and is designed for manipulation from within
the Fuel Handling Building.
9.1.4.2.2.5 Fuel Handling Tools Two fuel handling tools, as shown on Figure 9.1-7, are used to move fuel assemblies in the spent fuel pool area. A short tool is provided for dry transfer of new fuel, and a long tool is provided for underwater handling of both spent and new fuel in the spent fuel pool. The tools are operated manually.
9.1.4.2.2.6 Reactor Vessel Head Lifting RigThe reactor vessel head lifting rig is shown in Figure 9.1-8.(DRN 03-1341, R13)
The lifting rig, used in conjunction with the polar crane, is composed of a removable three-part lifting frame and a three-part column assembly which is attached to the reactor vessel closure head. The column assembly supports the six hoists for handling the hydraulic tensioners, the studs, washers and nuts. It links the lifting frame with the reactor vessel head.(DRN 03-1341, R13)
WSES-FSAR-UNIT-39.1-25Revision 9 (12/97)9.1.4.2.2.7Reactor Internals Handling EquipmentSeparate lifting rigs are used to remove either the upper guide structure or the core support barrel fromthe reactor vessel.The core support barrel lifting rig, shown in Figure 9.1-9 is provided to withdraw the core support barrelfrom the vessel for inspection purposes. The upper clevis assembly is a tripod-shaped structure connecting the lifting rig to the polar crane lifting hook. The lifting rig includes a spreader beam providing three attachment points which are threaded to the core support barrel flange. This is accomplished manually from the refueling machine bridge. Correct positioning of the lifting rig is assured by attached guide bushings which mate to the reactor vessel guide pins. The upper guide structure lifting rig isshown in Figure 9.1-10. The lifting rig consists of the core support barrel lifting rig and a structural framework of three column assemblies providing attachment points to the tipper guide structure.Attachment to the upper guide structure is accomplished manually from the working platform. Correct positioning is assured by attached bushings which mate to the reactor vessel guide pins.The integral in-core instrumentation hoist connects to an adapter that is manually attached to the in-coreinstrumentation support plate. The incore instrumentation is then lifted by the crane hook. The upper clevis assembly, which is common to this and to the core support barrel lifting rig, is installed prior to lifting of the structure by the crane hook.9.1.4.2.2.8Spent Fuel Handling MachineThe spent fuel handling machine as shown on Figure 9.1-11 is a traveling bridge and trolley which rideson rails over the spent fuel pool, refueling canal, and cask storage area. Motors on the bridge and trolley position the machine over the spent fuel assembly storage racks, the new fuel elevator and the upending machine. An auxiliary crane is used to transfer new fuel- from the new fuel storage racks to the new fuel elevator. The spent fuel handling machine hoist assembly contains a grappling device which, whenrotated by the actuator mechanism, engages the fuel assembly to be moved. Once the fuel assembly isgrappled, a cable and hoist winch raise the fuel assembly. The machine then transports the fuel assembly from the upending machine to the spent fuel storage racks (spent fuel) or from the new fuel elevator to the upending machine (new fuel).The controls for the spent fuel handling machine are mounted on a console which is located on the spentfuel handling machine trolley.Coordinate location of the bridge and trolley are indicated at the console and by a pointer and targetsystem.During withdrawal or insertion of a fuel assembly, the load on the hoist cable is monitored to assure thatmovement is not being restricted. Set points are such that damage to the assembly is prevented.Positive locking is provided between the grappling device and the fuel assembly to prevent inadvertentuncoupling. The drives for both the bridge and the trolley provide close control for accurate positioning, and brakes are provided to maintain the position once WSES-FSAR-UNIT-39.1-26achieved. In addition, interlocks are installed so that movement of the spent fuel handling machine is notpossible when the hoist is withdrawing or inserting an assembly.Manually operated handwheels are provided for bridge, trolley and winch motions in the event of a powerloss.The spent fuel handling machine is designed to seismic Category I requirements.
9.1.4.2.2.9New Fuel Elevator A fuel elevator, as shown on Figure 9.1-12, is utilized to lower new fuel from the operating level at the topof the refueling canal to the bottom of the canal where it is grappled by the spent fuel handling tool. The elevator is powered by a cable winch and fuel is contained in a simple support structure whose wheelsare captured in two rails. New fuel is loaded into the elevator by means of a crane and the new fuel
handling tool.9.1.4.2.2.10Underwater TelevisionA closed circuit television system, as shown on Figure 9.1-13, monitors the fuel and CEA handlingoperations inside the containment. A camera is mounted on both the fuel and the CEA hoists so that the fuel assembly or CEA can be sighted prior to and during grappling and removal from the core.The system may also be used to initially align the refueling machine position indication system with theactual core location of the fuel assemblies. A portable monitor is provided at the refueling machine control console. Each camera, if required for remote surveillance or inspection, can be removed from its mount and handled separately.9.1.4.2.2.11Fuel Sipping Equipment A sipping system tests irradiated fuel assemblies for cladding defects. This system consists of bothpermanently mounted components on the refueling machine and a portable control console that is set onto the refueling machine trolley when a sipping test is to be performed.
WSES-FSAR-UNIT-3 9.1-27 Revision 306 (05/12) 9.1.4.2.2.12 Hydraulic Power Unit
The hydraulic power unit, as shown on Figure 9.1-16, provides the motive force for raising and lowering
the upender with the fuel carrier. It consists of a stand containing a motor coupled to a hydraulic pump, a pump reservoir, valves and the necessary hoses to connect the power package to the hydraulic cylinders on the upender. The valves can be aligned to actuate either or both upender cylinders. The hydraulic fluid is demineralized water.
9.1.4.2.2.13 Refueling Pool Seal (DRN 02-176, R14)
A watertight permanent cavity seal ring (PCSR), as shown on Figure 9.1-17 has been installed between the reactor vessel flange and floor of the refueling pool specifically for the refueling operation. The PCSR has six hatches, which can be opened to provide access for activities within the Reactor cavity.
Double O-ring seals act against the PCSR and the removable hatches. A welded flexure ring is provided on the reactor vessel seal ledge and the ref uel pool embedment ring. The flexure ring design permits relative displacement (due to a SSE) between the vessel flange and the pool floor while still maintaining a watertight seal even under a 24 ft. head of water. Provisions are made to test the seals for the removable hatches after in stallation and before flooding the pool. (DRN 02-176, R14)
(EC-14270, R305)
(EC-14270, R305) 9.1.4.2.2.14 Cask Crane (EC-14275, R306)
A 125 ton capacity cask crane is provided to handle the spent fuel transfer cask in the Fuel Handling Building. The crane transports the spent fuel cask to and from the rail bay. (EC-14275, R306)
(EC-14270, R305)
The crane is provided with two control stations, an 11 button motorized station controlling the main hoist and the east and west monorail hoists, and a radio control system which controls all crane functions.
Both systems are arranged so that they may be br ought into the cab. The main hoist pushbutton pendant control is suspended from the bridge and supported from a motorized messenger track so that the pendant can be placed at any position along the length of the bridge. The pushbuttons are spring
loaded to insure automatic return to "OFF" position w hen buttons are released. The radio control is such that it can be operated from any point on the operating floor. (EC-14270, R305)
The crane is provided with bridge and trolley track type limit switches Both tra ck type limit switches are warning devices designed to give a warning light on t he pushbutton station when traveling to within 9 in.
of rail stops. The mechanical backups for the tr ack type limit switches are the bridge bumpers and trolley chocks (bumpers).
Bridge spring bumpers are attached to each end of each truck arranged to engage crane bumper stops.
The design required that they be capable of stopping the crane, traveling at full speed, with no load and power off, with a peak deceleration of 6.1 ft. per second within the maximum deflection of the springs (2
1/4 in.). The crane is provided with four WSES-FSAR-UNIT-3 9.1-28 Revision 305 (11/11) compression spring chocks, one mounted on each end of each bridge girder to limit the trolley travel.
The chocks are welded to the girder top plate on the outside of the rail and strike the trolley side below the wheel bearing retainer. These chocks also f unction as end stops after maximum spring deflection has been reached. The basis for the no load, power off design for both bridge and trolley is Paragraph 4.14 of CMAA Specification #70. Effects of swinging of the load (pendulum effect) upon sudden stopping of the crane has been evaluated.
Geared upper and lower limit switches are provided for the hoisting and lowering motions. The geared limit switches open the "HOIST" circuit when the bo ttom block reaches a preset upper limit and open the "LOWER" circuit when the bottom block reaches a preset lower limit. The limit switch assembly is driven by the hoist drum, and is actuated after a predetermi ned number of drum revolutions. The hoist limit switch automatically resets when the bottom block is lowered below the preset upper limit. In addition, the hoisting motion is restricted by a weight-operated limit switch. When the bottom block approaches
its preset upper limit, it contacts the reset counterweight. Continued upper movement of the bottom block lifts the counterweight, rotating a sheave whic h opens the normally closed contacts of the limit switch. This stops the hoist motor and applies the motor brake.
(EC-14270, R305)
The main hoist cable consists of 8 parts of redundantly reeved 1 5/8" diameter rope of Python super 8V EEIPS steel rope, with a minimum safety factor of 10 to 1 on the breaking strength, including static and dynamic loads. (EC-14270, R305)
The ropes are of sufficient length so that two full l aps remain on the 42" diameter main drum at the lowest position of the hook.
(EC-14270, R305)
(EC-14270, R305)
WSES-FSAR-UNIT-3 9.1-29 Revision 305 (11/11)
A number of other existing cr ane features are as follows:
a) Crane Controls (EC-14270, R305)
The crane panels contain protective disconnec t and overload devices, including the main disconnect switch (with provisions for external operation), main contactor, and control circuit fuses. The main disconnect switch is mounted on a panel in a heavy gauge sheet steel enclosure with hinged door interlocked with the main disconnect switch so that the door cannot be opened unless the switch is in the "OFF" position. The same interlock prevents the switch
from being closed until the door is closed.
The main contactor is reset and opened by the "START-STOP" pushbutton.
The control for the main hoist motion is by an AC Flux Vector Drive (FVD
). Control of the hoist motor is accomplished by a microprocessor and feedback system via an encoder. This closed-loop system allows the control to know what the motor is doing at all times, controlling motor
speed as well as output voltage and frequency. If the motor changes its operation without input from the crane control, the control can adjust it s output. This comparison occurs many times per second to ensure high-precision perfo rmance and safe movement of loads.
The control for the bridge and trolley motions is by an AC Variable Frequency Drive (VFD).
Control of the traverse motors is accomplis hed by a microprocessor and the referenced motor parameters. This open-loop system allows the control to monitor and make adjustments to the
motor speed, by controlling output voltage and frequenc
- y. This comparison occurs many times per second to ensure high-precision per formance and safe movement of loads
The FVD and VFD control circuitry is packaged in a cabinet on the bridge which is designed to provide protection against shock, vi bration, and severe environments. (EC-14270, R305)
All control and resistor wiring and all festoon and pendant cables are capable of passing the flame test as specified in IEEE 383-1974.
b) Crane Drive Assemblies:
(EC-14270, R305)
Bridge is driven by means of two (2) 7 1/2 HP electric motors mounted on the crane girder and each is connected through shafting and gearing to one of the wheels on the end truck. The driving and control mechanism is so designed and c onstructed that the crane shall not get out of line and the travel will be steady and free from vibr ation or rocking in any part of the structure while operating under any specified conditions.
(EC-14270, R305)
WSES-FSAR-UNIT-3 9.1-30 Revision 305 (11/11)
(EC-14270, R305)
The trolley is driven to two 3 HP electric motors mounted on the trolley frame and each is connected to one drive wheel on each side of the tr olley through gearing. Each trolley motor is mounted to a driving wheel. (EC-14270, R305) c) Crane Motion:
The crane is capable of raising, lowering, hol ding in any position and transporting a proof test load of 125 percent of rated load without damage or distortion to any crane part. The crane and each hoist will operate within the following tolerances:
- 1) With hook carrying 100 percent of rated load with all hoist brakes properly adjusted and operating normally, it will be possible to control the vertical movement within 1/4 in. When in the inching mode, the auxiliary hooks c an be controlled within 3/4 in.
- 2) Motion of the bridge and trolley will be controll able to within 1/4 in. under all conditions of loading.
The crane motions, have the following maximum speeds at capacity loads: (EC-14270, R305) a) Main hook hoisting - 5.0 ft./min.
b) Auxiliary monorail hook hoisting - 25 ft./min.
c) Bridge travel 50 ft./min.
d) Trolley travel 50 ft./min. (EC-14270, R305) d) Crane Braking System:
- 1) Bridge Travel: Electrically released, spring-set, friction shoe type brake with capacity at least equal to full operating torque of the bridge drive.
The brake will operate when motor controller is in "OFF" position, when main power supply switch is in "OFF" position, or in the event of power failure.
- 2) Trolley Travel: Electrically released, spring-set, friction shoe type brake with capacity at least equal to full operating torque of the trolley drive.
The brake will operate when motor controller is in "OFF" position, when main power supply switch is in "OFF" position, or in the event of power failure. (EC-14270, R305)
The main hoist has two electric stopping and holding brakes each of which is capable of holding the load
by itself and one electrical hoist control device.
Electric stopping and holding brakes will operate automatically and be of the electrically released, spring-set friction shoe type, capable of stopping and holding 1.5 times the full rated load when the power is off. The electric hoist control device is a Magnetorque which is connected to the main hoist cross shaft. It will be capable of controlling the lowering speed under all conditions with up to 1.5 times the rated load on hook. No lowering of load
shall occur unless power is applied to the hoist motor in a lowering direction. (EC-14270, R305)
WSES-FSAR-UNIT-3 9.1-31 Revision 305 (11/11)
Each auxiliary hoist has one electric stopping and holdi ng brake, one mechanical load brake. Electric stopping and holding brake will operate automatically and be of a disc type, capable of stopping and holding 1.5 times the full rated load when the power is off. Mechanical load brake is an automatic control device of a disc type, capabl e of controlling the lowering speed under all conditions with up to 1.5 times the rated load on hook. No lowering of load sha ll occur unless power is applied to the hoist motor in a lowering direction.
The dynamic loading effect produced by the deceleration action of the two main hoist brakes is well
within the capacity of the load carrying system. Th is effect represents a small fraction of the impact considered in the girder design.
(EC-14270, R305)
The trolley has been designed with single failure proof features and has been analyzed to ASME NOG-1 standards for single failure proof cranes.
The trolley provides redundant protection against postulated accidents, even during a seismic event. A seismic analysis determined the crane will not drop a Maximum Critical Load on the main hook during an OBE or an SSE. The crane control system is a fail-safe design and safety features are common m ode and single failure proof in mitigating postulated accidents. (EC-14270, R305)
(DRN 00-691, R11-A) 9.1.4.2.2.15 Polar Crane
A 200/30 ton reactor circular bridge crane on a 136'-4" diam eter (center to center of 171 lb. rails) is used inside containment to facilitate c onstruction, to remove the reacto r head during refueling and to remove or replace various equipment during construction. The crane is inac tive during normal plant operation and therefore cannot affect the safe shutdown capability of the plant. (DRN 00-691, R11-A)
The pushbutton pendant controlling the bridge, tro lley and hoist movements is suspended from the bridge to the operating floor and is supported from a motorized messenger track so that the pendant cable can be placed anywhere along the length of the bridge. The pushbuttons are spring loaded to
insure an automatic return to the "OFF" position when the buttons are released.
Weight operated limit switches are provided fo r the hoisting motions. When the bottom block approaches its preset upper limit, it contacts the reset counterweight.
Continued upper movement of the bottom block lifts the counterweight, rotating a sheav e which opens the normally closed contacts of the
limit switch. This stops the hoist motor and applies the motor brake.
The hoist motor has its torque limited to about 275 percent, i.e., a torque corresponding to a design factor of 2.75. When this torque is reached the mo tor's electrical system is tripped and the brakes engage automatically.
An electronic load indicating device is provided in the bottom block for the main hook. This device is an
integral part of the equipment. This device inco rporates both high and low load alarms. The load readout is at the pendant control. A hydraulic l oad indicating and positioning device between the main hook and the reactor head may be used during refueli ng to provide precise control of linear load movement to within .001 in., and load indication and c ontrol up to 250 tons with an accuracy of 0.5 of one percent.
WSES-FSAR-UNIT-39.1-32The trolley is provided with track type limit switches which are warning devices designed to give awarning light on the pushbutton station when traveling to within nine inches of rail stops. The mechanical backup for the track type limit switches are the four compression spring chocks, one mounted on each end of each bridge girder to limit the trolley travel. The chocks are welded to the girder top plate on the outside of the rail and strike the trolley side below the wheel bearing retainer. These chocks also function as end stops after maximum spring deflection has been reached.The main hoist cable consists of 14 parts of 1 3/8" diam. ropes of extra flexible steel rope with a steelcenter having a minimum of six strands of 37 wires per strand with a factor of safety of 6.8 (breaking strength).The ropes are of sufficient length so that two full laps remain on the 42" diameter main drum at thelowest position of the hook.The double reeving arrangement of the hoist ropes is connected to the main drum with clamps having aminimum strength equal to that of the rope.All trolley components including the drum mounts and sheave housing are designed for angular pulling ofthe hoist ropes.A number of other existing crane features are as follows:
a)Crane ControlsThe crane panels contain protective disconnect and overload devices, including the maindisconnect switch (with provisions for external operation), main contactor, overload relays for each motor circuit, and control circuit fuses. The main disconnect switch is mounted on a panel in a heavy gauge sheet steel enclosure with hinged door interlocked with the main disconnect switch so that the door cannot be opened unless the switch is in the "OFF" position. The same interlock prevents the switch from being closed until the door is closed. The main contactor is reset and opened by the "START-STOP" pushbutton.The control for the main hoist is AC Static Stepless providing variable speed control over the fullrange of hoisting and lowering speeds. Control of the motor speed is accomplished by the comparison of a "reference" signal, representing the desired speed, and a "feedback" signal, representing the actual speed. The resultant "error" causes the control system to call for motoring or braking, depending on the polarity of the error, and the motor runs at the desired speed as called for by the operator. Returning the master controller to the "OFF" position reduces the motor reactor current to zero and simultaneously causes the electric load brake to exert maximum torque. Thus, the motor is stopped by the load brake prior to the setting of the motor brake, thereby preventing overheating and excessive motor brake lining wear.The static control circuitry is packaged in compact functional modules which are designed toprovide protection against shock, vibration, and severe environments.
WSES-FSAR-UNIT-3 9.1-33 Revision 15 (03/07)
The control for the bridge and trolley motions is AC Static Stepless reversing Plugging providing variable regulated torque control for traverse motions. Control of acceleration is accomplished by the comparison of a variable output induction master reference signal with a torque feedback signal, producing an error signal which controls the supply current to reactors in the motor secondary circuitry. The end result is that the motion rate of acceleration or deceleration is
proportionally controlled by the operator.
All control and resistor wiring and all festoon and pendant cables are capable of passing the flame test as specified in IEEE-383.
b) Crane Drive Assemblies:
Bridge is driven by means of two (2) 7 1/2 HP electric motors mounted on the crane girder and connected through shafting and gearing to at least one of the wheels on each truck. The driving and control mechanism is so designed and constructed that the crane shall not get out of line and the travel will be steady and free from vibration or rocking in any part of the structure while
operating under any specified conditions.
The trolley is driven by two (2) 3 HP electric motors mounted on the trolley frame and connected to at least one driving wheel on each side of the trolley through gearing and shafting of a driver
axle.
c) Crane Motion:
The crane is capable of raising, lowering, holding in any position and transporting a proof test load of 125 percent of rated load without damage or distortion of any crane part. The crane and
each hoist will operate within the following tolerances:
- 1) With hook carrying 100 percent of rated load with all hoist brakes properly adjusted and operating normally, it will be possible to control the vertical movement to within 1/8 in.
- 2) Motion of the bridge and trolley will be controllable to within 1/4 in. under all conditions of loading.
The crane motions, have the following maximum speeds at capacity loads:
a) Main hook hoisting - 5 ft./min.
b) Auxiliary monorail hook hoisting - 30 ft./min.
c) Bridge travel 55 ft./min. -
(DRN 06-843, R15) d) Trolley travel 30 ft./min. - (DRN 06-843, R15)
WSES-FSAR-UNIT-3 9.1-34 Revision 303 (06/09) d) Crane Braking System:
- 1) Bridge Travel: Electrically released, spring-set, friction shoe type br eak with capacity at least equal to full operating torque of the bridge drive. The brake will operate when motor controller is in "OFF" position, w hen main power supply switch is in "OFF" position, or in the event of power failure.
- 2) Trolley Travel: Electrica lly released, spring-set, friction shoe type brake with capacity at least equal to full operating torque of the tr olley drive. The brake will operate when motor controller is in "OFF" position, w hen main power supply switch is in "OFF" position, or in the event of power failure.
All hoists have two electric stopping and holding brakes each of which is capable of holding the load by itself and one electrical hoist control device. El ectric stopping and holding brakes for main and auxiliary hoists will operate automatically and be of the electrically released, sp ring-set friction-shoe type, capable of stopping and holding 1.5 times the full rated load w hen the power is off. El ectrical hoist control devices are of the eddy current type. They w ill be capable of controlling the lowering speed under all conditions with up to 1.5 times the rated load on hook.
No lowering of load shall occur unless power is applied to the hoist motor in a lowering direction.
The dynamic loading effect produced by the deceleration action of the two main hoist brakes is well
within the capacity of the load carrying system. Th is effect represents a small fraction of the impact considered in the girder design.
Redundant crane controls and safety features are not generally provided. However, diverse safety features do provide redundant protection against pos tulated accidents. (Ev en though the crane hoisting system incorporates two brakes, t hey are subject to common mode failure, e.g., cable failure and are not considered here). For this reason, single active failure analysis cannot be applied to these features. The crane control system is a fail-safe design and safety features are common mode and single failure
proof in mitigating postulated accidents. (DRN 00-691, R11-A) 9.1.4.2.2.16 Control of Heavy Loads Requirements (DRN 00-691, R11-A)
(EC-11204, R303)
NUREG 0612, "Control of Heavy Loads at Nuclear Po wer Plants" contains the NRC guidance to ensure that load handling systems are des igned and operated such that their probability of failure is low and appropriate for the critical tasks in which they are em ployed. Waterford 3 has identified the containment polar crane and the fuel handling building cask cr ane as falling under the guidelines of NUREG 0612, and has implemented the NUREG 0612 Phase I guidance for these systems. In Supplement 6 to the Waterford 3 SER (Section 9.1.4 and Appendix 1) the NRC concluded that the Phase I requirements of NUREG 0612 had been satisfied for Waterford 3 with ex ceptions as noted in Technical Evaluation Report (TER) attached to Safety Evaluation for Phase 1. In a May 6, 1986 letter the NRC further concluded that, consistent with NUREG 0612 and G eneric Letter 85-11, the issue of heavy loads handling was complete.
The safety basis that ensures that the risk associated with load-handling failures is acceptably low is
based on: (1) meeting the phase 1 requirements of NUREG 0612, Section 5.
1.1 (See TER) and (2) a load drop analysis that demonstrates t he fuel remains covered and cooled.
NUREG 0612, Section 5.1.1, commonly known as Phase I, consists of seven elements that must be met for handling heavy loads that could be brought in prox imity to or over safe shutdown equipment or irradiated fuel in the spent fuel pool area or containment:
- 1. Definition of safe load paths
- 2. Development of load handling procedures
- 3. Qualifications, training, and specified conduct of crane operators (EC-11204, R303)
WSES-FSAR-UNIT-3 9.1-35 Revision 303 (06/09)
(EC-11204, R303)
- 4. Special lifting devices should satisfy the guidelines of American National Standards Institute (ANSI) N14.6-1978
- 5. Lifting devices that are not s pecifically designed should be installed and used in accordance with guidelines of ANSI B30.9
- 6. Periodic inspection and testing of cranes
- 7. Design of cranes to ANSI B30.2 or CMAA-70
Safe loads paths are defined and controlled as specified in administrative and refueling procedural
guidance. Load handling procedures maintain assump tions from load drop analysis and comply with commitments from NUREG-0612. Crane operators are trained, qualified and conduct themselves in accordance with Chapter 2-3 of American National Standards Institute (ANS I) B30.2-1976, "Overhead and Gantry Cranes." Special lifting devices satisf y the guidelines of ANSI N14.6-1978 with detailed clarification as provided in Technical Evaluation R eport attached to NRC Safety Evaluation for Phase I.
Non-specifically design lifting devic es are installed and used in accordance with the guidelines of ANSI B30.9 with detailed clarification as provided in Technical Evaluation Report attached to NRC Safety
Evaluation for Phase I. Cranes for critical lifts ar e inspected and tested in accordance with Chapter 2-2 of ASME B30.2-1976 with detailed clarification as pr ovided in Technical Evaluation Report attached to NRC Safety Evaluation for Phase I. Cranes used for critical lifts meeting the applicable criteria and guidelines of ASME B30.2-1 and CMAA-70 with detailed cl arification as provided in Technical Evaluation Report attached to NRC Safety Evaluation for Phase I.
To control Reactor Pressure Vessel Head lifts, refue ling procedural controls ar e used to control the lift and replacement of the reactor pressure vessel head.
These procedural controls establish limits on load height, load weight, and medium present under the l oad. These procedural controls: (1) use the guidance and acceptance criteria in NEI 08-05 Industry Initiative on Control of Heavy Loads [refer to Engineering Report WF3-CS-08-00001]; and (2) provide addi tional assurance that the core will remain covered and cooled in the event of a postulated reactor pressure vessel head drop. For reactor Pressure Vessel Head lifts, a load drop analysis a ssumes a head drop of 17 feet through air onto the reactor vessel with a maximum weight of 387, 000 pounds. Refueling procedural controls ensure compliance with load drop analysis assumptions. (EC-11204, R303) 9.1.4.2.3 System Operation
9.1.4.2.3.1 New Fuel Transfer (DRN 00-691, R11-A)
To transfer new fuel from the shipping container, the container covers are removed. The fuel assembly strongback is then raised and locked in the ve rtical position. The short handling tool, attached to the overhead crane, is then locked to the fuel asse mbly, the fuel assembly clamping fixtures removed and the fuel assembly moved from the shipping cont ainer. Any protective wrapping is removed and the fuel assembly is moved over to the new fuel elevat or (or new fuel storage racks). The tool is unlocked from the assembly and the new fuel el evator lowers the fuel assembly. (DRN 00-691, R11-A)
New fuel stored in the new fuel storage racks is trans ferred to the new fuel elevator using the cask crane and the short fuel handling tool. The cask handling crane clearance is shown in Figures 9.1-18 and 9.1-
- 19.
During reactor refueling operations, new fuel is re moved from the storage ra cks using the spent fuel handling machine to transfer the fuel assembly to the upending mechanism. Interlocks prevent the spent fuel handling machine from lowering the fuel assembly unless the upender is in the vertical
position. Once in the upending mechanism, a spent fuel assembly is removed from the other position in the fuel carrier and transferred to a designated position in the spent fuel storage racks.
WSES-FSAR-UNIT-3 9.1-36 Revision 306 (05/12) 9.1.4.2.3.2 Spent Fuel Transfer (EC-14275, R306)
The spent fuel handling machine transfers the assemblies from the storage racks to the spent fuel transfer cask. The cask loading area is connected to the pool by a gate sized to allow passage of the spent fuel handling machine with a fuel element atta ched. The spent fuel transfer cask arrives in a specially built low profile transporter at the l oading area which is serviced by an overhead cask handling crane. The main hoist of the crane transfers the cask to the cask decontamination area.
The spent fuel transfer cask is only handled using the single-failure-proof main hook on the cask handling crane as part of a single-failure-proof handling system, and thus a drop of a spent fuel transfer cask is not credible.
After the fuel transfer cask is serviced and washed, it is transferred to the spent fuel cask storage area.
Positioning the fuel transfer cask into the cask stor age area is a two-step hoisting operation. The first hoisting step sets the cask on a variable elev ation cask staging pedestal (VECASP). The second hoisting step lowers the fuel transfer cask to the bottom of the VECASP in the cask loading pit.
(EC-14270, R305)
The spent fuel assemblies are then transferred under water and loaded into the fuel canister located within the transfer cask using the spent fuel handling machine. Removal of the fuel transfer cask is accomplished by the single-failure-proof main hook on the cask crane.
(EC-14270, R305)
The loaded cask is moved to the cask decontamination area where radioactive material and residual
coolant are removed. The canister containing the spent fuel assemblie s is vacuum dried, backfilled with helium and welded shut. After the cask decontamination and canister sealing are complete, the spent fuel transfer cask is moved to the rail bay where the canister containing the spent fuel assemblies is
lowered into a fuel storage cask that is tr ansported to a concrete pad for storage.
(DRN 02-220, R11-A)
(DRN 02-220, R11-A)
(EC-14275, R306) 9.1.4.2.3.3 Refueling Procedure
(DRN 02-176, R14)
During the cooldown, preparations are begun for the refue ling operation. Refueling operations are initiated with the removal of the missile shield from over the reactor. The control element drive mechanisms (CEDMS) are disengaged from their drive shaft extensions by deenergizing the electromagnets, and the mechanism cabling is disconnected in preparation for head removal. The stud tensioners are employed to remove the preload on the vessel head studs. The nuts and studs are removed and plugs are installed to prevent refueling water from filling the empty stud holes. Two head alignment pins are inserted to assist in subsequent operations. The CEDM cooling shroud is disconnected from its duct work and the vessel vent
line removed. The reactor vessel flange is permanently sealed to the bottom of the pool by means of the refueling pool seal ring with removable hatches. T he removable hatches are installed on the seal ring and leak tested to preclude water from entering the lower portion of the reactor vessel cavity. The reactor head lifting rig is then installed on the head assembly, and by means of the polar crane, the head is removed to its storage location. The polar crane clearance is show n in Figure 9.1-20. Equipment laydown areas inside the containment are shown in Figure 1.2-17. (DRN 02-176, R14)
WSES-FSAR-UNIT-3 9.1-37 Revision 303 (06/09)
During reactor operation, the transfer tube is closed by a manually operated valve in the fuel pool and a double-gasketed blind flange inside the containment.
The flange is removed and the pool is filled with borated water. After a common water level is reached, the transfer tube valve is opened preparatory to refueling.
Provision is made in the refueling pool for the temporary storage of the upper guide structure. After this
is removed from the vessel, the refueling machine hoist mechanism is positioned to the desired location over the core. Alignment of the hoist to the top of the fuel assemb ly is accomplished through the use of a digital readout system and is monitored by closed circ uit television. After the fuel hoist is lowered, minor adjustments can be made to properly position the hoi st if misalignment is indicated on the monitor.
The operator then energizes the actuator assembly wh ich rotates the grapple at the bottom of the hoist and locks the fuel assembly to the hoist. The hoist mo tor is started and the fuel assembly withdrawn into the fuel hoist box assembly so t hat the fuel is protected during tr ansportation to the fuel upender. The grapple is designed to preclude inadvertent disengagement as the fuel assembly is lifted vertically from the core. When the fuel has been withdrawn fr om the grapple zone, positive locking between the grapple and the fuel assembly is established so that uncoupling is prevented even in the event of inadvertent initiation of an uncoupling signal to the asse mbly. After removal from the core, the spent fuel assembly is moved underwater to the transfer area of t he pool. The spent fuel assembly is lowered into the transfer carriage in the refueling pool. If the fuel assembly contains a control element assembly, the CEA hoist mast, transfers the control elem ent assembly to a new fuel assembly.
The new fuel assembly is removed from the ca rriage and moved to the reactor as the upending machine lowers the spent fuel assembly to the horizontal pos ition after which a cable drive transports the carriage on tracks through the transfer tube into the spent fuel pool.
Once received in the spent fuel pool, another upendi ng machine returns the transfer carrier to the vertical position. The spent fuel handling machine tr ansfers a new fuel assembly to the transfer carriage and then removes the spent fuel assembly from the transfer carriage and transports it to the spent fuel rack. The new fuel assembly is carried through the transfer tube to the refueling pool where the refueling machine picks it up and places it in its proper position in the core. The refueling machine is also used to shuffle fuel and CEAs within the co re in accordance with the fuel management scheme.
Wet sipping of fuel assemblies can be conducted, if required, during normal fuel handling operations.
(DRN 02-176, R14)
At the completion of the refueling operation, the transfer valve is manually closed. The upper guide structure is reinserted in the vessel and the incore in strumentation placed in position. The drive shaft extensions are reconnected to the CEAS. The water in the refueling pool is lowered. The head is then lowered until the drive shaft extensions are engaged by the CEDMS. Lowering of the head is continued until it is seated. Then the studs are installed and the head is bolted down, and the transfer tube blind flange installed. The hatches in the permanent re fueling pool seal between the reactor vessel flange and the pool are removed. CEDM and in-core instrument cabling is reconnected.
The cooling ducts are reconnected to the shroud, the vessel vent piping inst alled, and the missile shield placed in position. (DRN 02-176, R14) 9.1.4.3 Safety Evaluation
The Fuel Pool System and the Fuel Handling System are designed to meet the intent of Regulatory
Guide 1.13 (March 1971),with t he following clarification:
WSES-FSAR-UNIT-3 9.1-38 Revision 306 (05/12
) Regulatory Position Comment
C.4 During refueling, the normal ventilation system (no filters) in the Fuel Handling Building is operating. Leakage is suitably controlled by automatic actuations of the emergency system should high airborne radiation occur.
9.1.4.3.1 Cask Handling (EC-14275, R306)
The leaktight partition wall between the fuel ca sk handling area and the spent fuel storage area will ensure that the spent fuel racks remain covered with water if the cask handling area empties completely. The portion of the slab in the spent fuel cask storage area is structurally i ndependent of the spent fuel storage pool slab. Therefore, the impact of the transfer cask on the cask storage area slab will have no detrimental structural effect on the independent fuel storage pool slab.
To preclude possibility of damage to the spent fuel storage area which could affe ct its water tightness, an electrical interlock system is provided; the restrict ed zone limit switch devices and l ogic will preclude crane entrance to subject zone pending location of trolley, so that t he main hoist hook cannot carry a transfer cask such that any part of the cask is over the spent fuel storage area or partition wall. Transfer cask handling will occur only using a single-failure-proof main hook on the cask handling crane, and thus a drop of a
transfer cask is not credible. (EC-14275, R306)
Safety features of the crane include the following:
(EC-14270, R305) a) Main hoist ropes will have a factor of safety of ten and auxiliary hoist r opes will have a factor of safety of six based on rated load and efficienc y of lifting tackle but excluding impact load. (EC-14270, R305) b) All parts subject to dynamic strains such as gears, shafts, drums, blocks, and other integral parts will have a factor of safety of five.
c) Bending stress combined with torsional stress in pins and axles shall not exceed 20 percent of the yield stress of material used.
d) Normal torsional deflection in bridge drive shaft will be limited to 0.03 degrees per ft. at two thirds of rated motor torque or a total movement at wheel circumference of 0.5 in., whichever is more restrictive.
WSES-FSAR-UNIT-39.1-399.1.4.3.2Fuel HandlingA failure mode analysis is not required.
The results of the safety analysis (Chapter 15) demonstrate that applicable dose limits are not exceededas a result of the design basis fuel handling accident. No credit is taken for components or subsystems of the fuel handling equipment to either prevent or mitigate the consequences of the postulated accident.Direct communication between the main control room and the refueling machine console is availablewhenever changes in core geometry are taking place. This provision allows the control room operator to inform the refueling machine operator of any impending unsafe condition detected from the main control board indicators during fuel movement.Operability of the fuel handling equipment including the bridge and trolley, the lifting mechanisms, theupending machines, the transfer carriage, and the associated instrumentation and controls is assured through the implementation of preoperational tests. Prior to the fuel loading, the equipment is cycled through its operations using dummy fuel. In addition to the interlocks described in Subsection 9.1.4.2.1, the equipment has the following special features:a)The major components of the Fuel Handling System are electrically interlocked with each otherto assist the operator in properly conducting the fuel handling operation. Failure of any of theseinterlocks in the event of operator error will not result in damage to more than one fuel assembly.
The radiological consequences associated with the activity release from an assembly are discussed in Section 15.7.b)Miscellaneous special design features which facilitate handling operations include: backup handoperation of the refueling machine hoists in the event of power failure; a dual wound transfer system motor to permit applying an increased pull on the transfer carriage in the event it becomes stuck; a viewing port in the refueling machine trolley deck to provide visual access to the reactor for the operator; electronic and visual indication of the refueling machine position over the core; a protective shroud into which a fuel assembly or CEA is drawn by the refueling machine; transfer system upenders manual operation by a special tool in the event that the hydraulic system becomes inoperative.c)The fuel transfer tube is sufficiently large to provide natural circulation cooling of fuel assembly inthe unlikely event that the transfer carriage should be stopped in the tube. The manual operator for the fuel transfer tube valve extends from the valve to the operating deck. Also, the valve operator has enough flexibility to allow for operation of the valve even with thermal expansion of the fuel transfer tube.d)Travel stops in both the refueling and spent fuel handling machines restrict withdrawal of thespent fuel assemblies. This results in the maintenance of a minimum water cover of nine ft. over the active portion of the fuel assembly. The combined shielding effects of the water and handling tools results in a radiation level of 2.5 mr/hr. or less at the surface of the water. The depth ofwater WSES-FSAR-UNIT-3 9.1-40 Revision 306 (05/12
) surrounding the fuel transfer canal, transfer tube and spent fuel storage pool is sufficient to limit the maximum continuous radiation levels in working areas to 2.5 mr/hr.
9.1.4.4 Testing and Inspection Requirements
During manufacture at the vendor's plant, various in-process inspections and checks are required including certification of materials and heat treating, and liquid-penetrant or magnetic-particle inspection of critical welds. Following completion of m anufacture, compliance with design and specification requirements is determined by assembling and testing the equipment in the vendor's shop. Utilizing a dummy fuel assembly having the same weight, center of gravity, exterior size and end geometry as an actual assembly, all equipment is run through severa l complete operational cycles. In addition, the equipment is checked for its ability to perform under the maximum limits of load, fuel mislocation and misalignment. All traversing mechanisms are tested for speed and positioning accuracy. All hoisting equipment is tested for vertical functions and controls, rotation, and load misalignment.
(EC-35729, R306)
Hoisting equipment is also tested to 125 percent of specified hoist capacity. Set points are determined and adjusted and the adjustment limits are verified.
Equipment interlock func tion, and backup systems operations are checked. Those functions having manual operation capability are exercised manually. During these tests, the various operating parameters such as motor speed, voltage, and current, hydraulic system pressures, and load measuring accuracy and set points are recorded. At the completion of these tests the equipment is check ed for cleanliness and foreign material exclusion issues. (EC-35729, R306)
Equipment installation and testing at the plant site is controlled by approved installation procedures and preoperational test procedures designed to verify conf ormance with specification. Each component is inspected and cleaned prior to installation into t he system. Recommended maintenance, including any necessary adjustments and calibrations, is performed pr ior to equipment operation at each refueling.
Preoperational tests also include checks of all contro l circuits including interlocks and alarm functions.
9.1.4.5 Instrumentation Requirements
The refueling system instrumentat ion and controls are described in S ubsection 9.1.4.2. No credit is taken for instrumentation or interlocks on components of the fuel handling equipment to either prevent or mitigate the consequences of the postulated accident.
Therefore, the interlocks described above are not safety related.
(EC-14275, R306) 9.1.5 SPENT FUEL DRY CASK STORAGE WF3 has established an Independent Spent Fuel Storage In stallation (ISFSI) locat ed directly south of the four water storage tanks and just west of the switchyard area. The ISFSI concrete pad has a capacity for 72 vertical spent fuel storage casks.
The PA security fence encompasses the ISFSI site, with 20 ft isolation zones along the inside and outside of the fence. An entrance gate provides for vertical cask transporter (VCT) access to the ISFS I pad, and a man gate is in the fence between the plant and ISFSI areas. The ISFSI is inside the plant protected area.
The Spent Fuel Dry Cask Storage operations at WF3 will be conducted under a general license in accordance with Subpart K of 10 CFR Part 72.
The general license issued by 10 CFR 72.210, "General license issued," authorizes a 10 CFR Part 50 nuclear power plant licensee to store spent fuel at an onsite ISFSI. Subpart K of 10 CFR Part 72 also in cludes 10 CFR 72.212, "Conditions of general license issued under §72.210," which requires the use of a dry cask storage system that is pre-approved by the Nuclear Regulatory Commission, as evi denced by its listing in 10 CFR 72.214. (EC-14275, R306)
WSES-FSAR-UNIT-3 9.1-41 Revision 306 (05/12
) (EC-14275, R306)
The WF3 ISFSI uses the Holtec HI-STORM 100S Version B vertical cask storage overpack and the Holtec MPC-32 multi-purpose canister (MPC), as described in the HISTORM 100 Cask System FSAR (Reference 8) and approved by the Nuclear Regulator y Commission via the HI-STORM Certificate of Compliance No. 1014 (Reference 9).
The MPC provides the confinement boundary for the st ored fuel. The MPC is a welded, cylindrical canister with a honeycombed fuel basket. All MP C confinement boundary components are made entirely of stainless steel. The honeycombed basket, whic h is equipped with neutron absorbers, provides criticality control.
The HI-STORM 100S Version B storage overpack provides shielding and structural protection of the
MPC during storage. The HI-STORM 100S Version B overpack design includes a lid which incorporates the air outlet ducts into the lid. The overpack is a heavy-walled steel and concrete, cylindrical vessel. Its side wall consists of plain (unreinforced) concrete that is enclosed between inner and outer carbon steel
shells. The overpack has four air inlets at the bo ttom and four air outlets at the top to allow air to circulate naturally through the cavity to cool the MPC inside. The inner shell has supports attached to its interior surface to guide the MPC during insertion and removal, and allow cooling air to circulate through
the overpack. A loaded MPC is stored within t he HI-STORM 100S Version B storage overpack in a vertical orientation. (EC-14275, R306)
Section 9.1: REFERENCES (DRN 99-1097, R11; 05-1365, R14-A; EC-5000082411, R 301; EC-18742, R304) 1. Licensing Report for Waterford Unit 3 Spent Fuel Pool Criticality Analysis by Holtec International, Holtec Report HI-2094376, Rev. 0, June 24, 2009. (DRN 05-1365, R14-A; EC-5000082411, R301; EC -18742, R304)
(EC-8477, R305)
- 2. Not used.
(DRN 99-1097, R11; EC-8477, R305) (DRN 99-2519, R11)
- 3. Letter to U.S. Nuclear Regulatory Commission, "Withdrawal of January 22, 1999 Letter Providing Additional Information Regarding License Am endment No. 144", July 23, 1999, Letter No.
W3F1-99-0118. (DRN 99-2519, R11) (EC-5000082411, R301; EC-18742, R304)
- 4. Letter to U.S. NRC Document Control Desk, "Response Request for Additional Information RAI #2 -," W3F1-2009-0022, June 20, 2009.
- 5. Criticality Safety Evaluation of the Waterf ord Unit 3 New Fuel Storage Vault by Holtec International, Holtec Report HI-2083974, Rev. 2, June 24, 2009. (EC-5000082411, R301; EC-18742, R304) (EC-8884, R303)
- 6. Seismic/Structural Analysis of Waterford 3 S pent Fuel Racks by Holtec International, Holtec Report HI-971606, Calculation EC-C98-009.
- 7. Fuel Assembly Drop Accident Analysis for Wa terford-3 Spent Fuel Pool, Holtec Report HI- 961595, Calculation EC-C98-005. (EC-8884, R303)
(EC-8477, R305)
- 8. Limiting Single Failure Thermal Hydraulic Analysis of Waterford 3 Spent Fuel Pool, Calculation ECM98-067.
(EC-8477, R305)
WSES-FSAR-UNIT-3 9.1-42 Revision 306 (05/12
) (EC-14275, R306)
- 9. Holtec International Final Safety Analysis Report for the HI-STORM 100 Cask System, Revision No. 7, USNRC Docket No. 72-1014, Holtec Report No.: HI-2002444, August 6, 2008.
- 10. USNRC Certificate of Compliance No. 1014, Do cket No. 72-1014, Amendment No. 5, for the HI-STORM 100 Cask System, July 14, 2008. (EC-14275, R306)
WSES-FSAR-UNIT-3 TABLE 9.1-1 Revision 305 (11/11)
FUEL POOL SYSTEM PROCESS FLOW DATA (EC-8477, R305)
Fuel Pool Cooling With One Fuel Pool C ooling Pump Running (Parallel Heat Exchangers)
FPS Location* 1 2 3 4 5 6 7 Flow (gpm) 2786 2786 2786 - - - -
Press. (psig) 12 23 16 - - - -
Temp. (F) 130 130 100 - - - -
Fuel Pool Cooling With Two Fuel Pool C ooling Pumps Running (Parallel Heat Exchangers)
FPS Location* 1 2 3 4 5 6 7 Flow (gpm) 4523 4523 4523 - - - -
Press. (psig) 10 35 18 - - - -
Temp. (F) 132 132 109 - - - -
Normal Purification FPS Location* 1 2 3 4 5 6 7 Flow (gpm) - - - 150 150 150 150 Press. (psig) - - - 11 78 50 3 Temp. (F) - - - 120 120 120 120 (EC-8477, R305)
- Refer to Drawing G169 for location of process flow points.
WSES-FSAR-UNIT-3 TABLE 9.1-2 Revision 304 (06/10)
REFUELING AND SPENT FUEL POOL WATER CHEMISTRY
Design Parameters
pH 4.5 - 10.2
Boron (RWSP) 2050 - 2900 ppm (EC-18742, R304)
Boron (SFP) 1900 - 2900 ppm (EC-18742, R304)
Chloride 0 - .15 ppm Cl
Fluoride 0 - .1 ppm F
Ammonia 0 - 50 ppm NH 3
Lithium 0 - 2.5 ppm 7 Li+
Hydrazine 0 - 50 ppm N 2 H 4 Optical Clarity Note (1)
Note (1)
Minimum optical clarity is defined as being able to read fuel bundle lettering which is 3/8" high, 3/16" wide
and 1/16" thick at 25 ft. below the surface of the water with the aid of optical instruments.
WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 1 of 8) Revision 15 (03/07)
PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Design Parameters
Component Parameters Description
Fuel Pool Quantity 2
Cooling Pump Type Centrifugal, horizontal
Design Pressure, (psig) 150 Design Temperature (F) 200 Design Head, (Ft) 76
Design Flow, (gpm) 2000 Normal Operating Temp., (F) 90 - 150 Normal Suction Pressure, (psig) 15
NPSH MIN Available at Design 64 Flow, (Ft)
Motor HP 60 (DRN 06-843, R15)
Fluid, Boric Acid Maximum (Wt. %) 1 (DRN 06-843, R15)
Material in Contact with Liquid Austenitic Stainless Steel
Code ASME Section III, Class 3, 1971/Summer 1972 WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 2 of 8) Revision 15 (03/07)
PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Design Parameters
Component Parameters Description
Fuel Pool Puri- Quantity 1
fication Pump Type Centrifugal, horizontal
Design Pressure, (psig) 150 Design Temperature, (F) 200 Design Head, (Ft) 165
Design Flow (gpm) 150 Normal Operation Temp., (F) 8 90 - 150
Normal Suction Pressure, (psig) 15 NPSH Available at Design 49.2 Flow, (Ft)
Motor HP 20 (DRN 06-843, R15)
Fluid, Boric cid Maximum 1 (Wt. %) (DRN 06-843, R15)
Material in Contact with Liquid Austenitic Stainless Steel
Code ASME Section III, Class 3, 1971/Summer 1972 WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 3 of 8) Revision 15 (03/07)
PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Design Parameters Component Parameters Description Refueling Water Quantity 1
Pool Purifi-cation Pump Type Centrifugal, horizontal
Design Pressure, (psig) 100 Design Temperature (F) 200 Design Head, (Ft) 170
(DRN 06-843, R15)
Design Flow, (gpm) 150 (DRN 06-843, R15)
Normal Operating Temp. (F) 90 - 150 Normal Suction Pressure, (psig) Atmos.
NPSH Available at Design Flow, (Ft) 31 Motor HP 15
Fluid, Boric Acid Maximum 1.5 (Wt. %)
Material in Contact with Liquid A-296 CF 8M-316 Stainless Steel
Code ASME VIII 1973 Winter 1975 addenda WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 4 of 8) Revision 15 (03/07)
PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Design Parameters
Component Parameters Description
Refueling Canal Quantity 1
Drain Pump Type Centrifugal, horizontal
Design Pressure, (psig) 100 Design Temperature, (F) 200 Design Head, (Ft) 100
Design Flow, (gpm) 200 Normal Operating Temperature, (F) 120 Normal Suction Pressure, (psig) Atmos.
NPSH Available at Design Flow, (Ft) 47
Motor HP 10 Fluid, Boric Acid Maximum (Wt. %) 1.5
Material in Contact with Liquid A-296 CF 8M-316 Stainless Steel
Code ASME VIII 1973 Winter 1973 addenda
Fuel Pool Quantity 1 Ion Exchanger Type Flushable
Design Pressure, (psig) 200 Design Temperature, (F) 250 (DRN 06-843, R15)
Normal Operating Temp., (F) 120 Normal Operating Pressure, (psig) 80 (DRN 06-843, R15)
Resin Volume, Total (Ft
- 3) 36.2 Resin Volume, Useful (Ft
- 3) 32.0 WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 5 of 8) Revision 13-B (01/05) PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Design ParametersComponent Parameters Description Fuel Pool Normal Flow, (gpm) 150 Ion Exchanger (Cont'd) Design Flow, (gpm) 300 Code (Vessel) ASME VIII, Class 3 1968, Summer 1970 addenda Material in Contact with Liquid Austenitic Stainless Steel Retention Screen Size 80 U.S. Mesh Resin Type Anion/Cation Mixed Bed Maximum AP @ Design 15 Flow, (Ft) Fuel Pool Quantity 1
PurificationFilter Type Resin bonded glass fiber and polyester Design Temperature, (F) 200 Design Pressure, (psig) 150 Design Flow, (gpm) 150 Normal Temperature, (F) 90 - 130 Normal Pressure, (psig) 78 (DRN 04-487, R13-B) Maximum Operating Temperature (F) 155 (DRN 04-487, R13-B) Normal Flow, (gpm) 150 Clean P @ 150 gpm, (psi) 5 Loaded P @ 150 gpm, (psi) 25 Removal Rating Absolute (Beta Method) 20 microns WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 6 of 8) Revision 14 (12/05) PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Design ParametersComponent Parameters Description Shell Materials Austenitic Stainless Steel Code ASME VIII 1968/Summer 1970 (DRN 99-1097, R11)
Fuel Pool Heat Exchanger* Quantity 1 (DRN 99-1097, R11) Type Shell and Tube (2 Tube Pass) Code ASME III, Class 3, 1971 Tube Side (Fuel Pool) Fluid Fuel Pool Water Design Pressure (psig) 75 Design Temperature (F) 250 Materials Austenitic Stainless Steel Pressure Drop @ Design Flow (psi) 10 Normal Flow (gpm) 2000 Design Flow (gpm) 4000 (DRN 99-1097, R11; 03-2063, R14)(DRN 99-1097, R11; 03-2063, R14) Shell Side (Component Cooling Water) Fluid Component Cooling Water Design Pressure 150 Design Temperature (F) 250 Materials Carbon Steel Pressure Drop @ Design 15 Flow (psi) Normal Flow, (gpm) 1600 Design Flow, (gpm) 5000 (DRN 99-1097, R11; 03-2063, R14)(DRN 99-1097, R11; 03-2063, R14)
WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 7 of 8) Revision 15 (03/07)
PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Operating Parameters Component Parameters Description (DRN 99-1097, R11; 03-2063, R14)
Fuel Pool Tube Side (Fuel Pool) Normal Cooling Maximum Cooling Heat Exchanger (Cont'd) Flow, (gpm) 2440 3650
Inlet Temp. (F) 140 155 Outlet Temp. (F) 115.7 125.7 Heat Transferred (Btu/hr) 29.1 x 10 6 52.5 x 10 6 Shell Side Component Cooling Water
Flow (gpm) 2768 5000 Inlet Temp. (F) 90 90 Outlet Temp. (F) 111.2 111.1
Performance data assume that 5% of the Heat Exchanger tubes are plugged (DRN 99-1097, R11; 03-2063, R14)
Backup Fuel Quantity One Pool Heat Exchanger Type Shell and Tube (2 Tube Pass)
Code ASME III, Class 1971 thru Summer 1973
Tube Side (Fuel Pool) Fuel Pool Water Fluid Design Pressure 150 (psig) Design Temperature (F) 200 Materials Austenitic Stainless Steel (DRN 06-843, R15) Pressure Drop @ normal flow 6 (DRN 06-843, R15) (psi) Flow (gpm) 1750 Inlet temp (F) 140 (DRN 99-1097, R11; 03-2063, R14)
Outlet temp (F) 120.6 (DRN 99-1097, R11)
Heat transferred 16.7 (BTU/HR) (DRN 03-2063, R14)
WSES-FSAR-UNIT-3 TABLE 9.1-3 (Sheet 8 of 8) Revision 14 (12/05) PRINCIPAL COMPONENTS DESIGN DATA
SUMMARY
Operating ParametersComponent Parameters Description Shell Side (Component Cooling Water System) Fluid Component Cooling Water Design Pressure 150 (psig) Design Temperature (F) 175 Materials Carbon Steel Pressure Drop
@ Normal flow 5 (psi) (DRN 03-2063, R14) Flow (gpm) 2000 Inlet temp (F) 90 Outlet temp (F) 106.8 (DRN 03-2063, R14) Refueling Cavity Drain Pump Quantity One Type Centrifugal, Horizontally Mounted Design Pressure, (psig) 100 Design Temperature, (F) 200 Design Head, (ft.) 100 Design Flow, (gpm) 500 Normal Operating Temp. (F) 120 Normal Suction Press. (psig) Atm.
NPSH Available at Design Flow (ft.) 30 Motor HP 20 Fluid, Boric Acid Maximum (wt. %) 1.5 Material in Contact with Liquid A296 CF8M, 316 Stainless Steel Code ASME VIII 1973, Winter 1973 Addenda WSES-FSAR-UNIT-3 TABLE 9.1-4 (Sheet 1 of 10) Revision 309 (06/16)
FAILURE MODE AND EFFECTS ANALYSIS FUEL POOL SYSTEM
No.
Name Failure Mode Cause Symptoms and Local Effects
Including Dependent Failures
Method of Detection Inherent Compensating Provision
Effect Upon Remarks and
Other Effects (DRN 99-1097, R11, R11)
- 1. Fuel Pool Nozzle Screen Clogged Impurities, Loss of suction for both fuel pool pumps Pressure Indicator, PI 401, 402 visual Screen can be cleaned in a short period of time No Fuel pool cooling when
this failure
occurs. Fuel Pool purification system would
minimize chance of
this failure. (DRN 99-1097, R11, R11) (LBDCR 16-013, R309)
- 2. Fuel Pool pump isolation valve:
3FS-V102 B (FP 203) a) Fails closed Mechanical
- failure, blockage Loss of Suction for one fuel pool pump Pressure indicator, PI 401, 402 Two redundant Fuel Pool pumps Equilibrium temperature
of fuel pool will be increased (LBDCR 16-013, R309) b) Fails open Mechanical Failure No impact on fuel pool cooling, cannot isolate
F.P. pump for repair Periodic Testing Repair N/A (DRN 99-1097, R11)
- 3. Fuel Pool pump Temp.
Strainer 3FS-S108 A, 3FS-S108 B Clogged Impurities, particulate matter Possible loss of suction of one fuel pool pump Pressure indicator, PI 401, 402 Equilibrium temperature
of fuel pool will be increased Fuel Pool purification system would minimize this
failure. It
is a potential
common mode
failure (DRN 99-1097, R11)
- 4. Fuel Pool Pump A,B Complete Failure Mechanical, Electrical
Failure Loss of one fuel pool pump Pressure indicator, PI 401, 402 Two fuel pool pumps Equilibrium temperature
of fuel pool will be increased Possible Low Discharge Pressure
Alarm form PS-403 WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 2 of 10)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects 5.Fuel poolpump dis-charge Pres-sure Indica-tor PI 401,PI 402Fails toindicate correct pressureMechanical,Electrical FailureUnusual Pressure Indicationor erratic pressure indication.Periodic TestingPossible LowDischarge Pressure Alarm from PS-403 N/A 6.Fuel poolpump Isolation valve:
3FS-V103 A (FP-208) 3FS-V104 B (FP-209)a) Fails closedMechanicalFailure,BlockageCentrifugal pump drivingagainst a dead head; High Pressure indication; loss of one fuel pool pump.High pressureindication; valve position indicator.(Locally)Two Redundantfuel pool pumpsEquilibriumtemperature of fuel pool willbe increased.b) Fails openMechanicalFailureNo impact on fuel poolcooling; cannot isolatesection of pipe for repair.Periodic TestingRepairN/A 7.Fuel PoolPump Dis-charge Header Pressure Switch PS 403Fails to function properlyElectrical,Mechanical FailureErratic Pressure AlarmPressure Alarm;Pressure Indicators upstream PI 401, 402; periodic testing.Pressure IndicatorsPI 401, 402 N/A 8.Fuel PoolHeat exchanger temperature indicator TI 404, TI 405Fails toindicate correct temper-atureElectricalFailureErroneous indicationof Fuel Pool Heat Exchanger PerformanceChanges in FuelPool Temp. if Operator Changes Coolant Flow
in Response To Erroneous Indications.Fuel Pool Temp.Indicator TI 420and Alarm N/A WSES-FSAR-UNIT-3 TABLE 9.1-4 (Sheet 3 of 10) Revision 309 (06/16)
FAILURE MODE AND EFFECTS ANALYSIS FUEL POOL SYSTEM
No.
Name Failure Mode Cause Symptoms and Local Effects
Including Dependent Failures
Method of Detection Inherent Compensating Provision
Effect Upon Remarks and
Other Effects
- 9. Fuel pool Heat Exchanger (or Backup
Fuel Pool
Heat Exchanger) a) Cross Leakage Corrosion or manufacturing
defects Leakage of fuel pool coolant to component cooling system.
Radiation sensors in component cooling None b) Decrease in ability
to transfer
heat i) Excessive fouling ii) Blockage
iii) Failure in CCS High Temperature in fuel pool cooling
line. (TI-405)
High Temperature, (TI 405) high temp. alarm if temp. inc. is
significant (TI 420) Two Seismic Category I Makeup sources avail-
able to maintain Fuel Pool Level even if
Boiling occurs.
Equilibrium temp. of fuel pool will be increased.
(DRN 99-1097, R11)
(DRN 99-1097, R11)
b) Fails open Mechanical
- failure, blockage
Mechanical
failure Cannot skim the fuel pool. Decrease in clarity of water
No impact on fuel pool
cooling, or purification
cannot isolate skimmer
for repair Periodic Testing, visual
Periodic Testing Repair
Series Redundant isolation valve
(7FS-V109)
(LBDCR 15-007, R309)
(LBDCR 15-007, R309)
WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 4 of 10)Revision 11 (05/01)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects12.Purificationpump suction isolation valvea) Fails closedMechanicalbinding, operator errorLoss of fuel poolpurification loopLow pump suctionand discharge
pressureRepair valve7FS-V107,7FS-V109 (FP-222)b) Fails openMechanicalbindingNone, valve is normallyopen during system operationHandle positionSeries redundantisolation valve13.Purificationpump suction inline basketstrainer7FS-S151CloggedImpurities, particulate matterLoss of fuel poolpurification loopLow pump suctionand discharge
pressureRepair14.Purificationpump intake and discharge
pressure indicator Pi 411, PI 412Fails toindicate correct valueMechanical,ElectricalfailureErroneous indicationof pump or purificationsystem performanceAbnormal IndicationRepair15.Fuel poolpurificationpumpCompletepumpfailureMechanical,ElectricalFailureLoss of fuel poolpurification loopLow pressureindication atPI 411 and PI 412None RequiredCannot purifyfuel pool untilrepaired16.Fuel poolpurification pump discharge Isolation valve 7FS-V118 (FP-226)a) Fails closedb) Fails openMechanicalFailure,blockage, operator errorMechanicalFailureLoss of fuel poolpurification loop.
Purification pump operating at shutoff head pump damageNo impact on fuel poolpurification system, valve normally open during operation; cannot isolate section of loop for repairHigh Pressureindication atPI 412Handle PositionRepairSeries redundantisolation valve WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 5 of 10)Revision 11 (05/01)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects17.Fuel poolpurification loop sample (7FS-V156),
(FP 227),(FP 235),(FP 247)a) Fails closedb) Fails openBlockage, corrosionSeatleakage, operator errorCannot sample fuelpool purification systemDivert part of fuel poolwater to sample outletNone, Valvenormally closedLeakageNoneLine is capped18.Refuelingwater pool purification pump isolation valve tofuel poolpurification loop 7FS-V126, 7FS-V174a) Fails closedb) Fails openMechanicalfailure, corrosionMechanicalfailure, operator errorCannot provide purificationfor refueling water. Cannotprovide makeup to the FuelPool from the refueling water storage pool.
Divert refueling water to fuel pool OperatorLevel alarm in fuel poolNoneSeries redundantisolation valvePurificationand Fuel Pool make up19.Fuel Poolpurificationloop filterCloggedImpurities, particulatematterLoss of fuel poolpurification loopHigh Differentialpressure readingin PDI 415Parallel Redundantflow path through filter bypass valve7FS-V11620.Fuel Poolpurification loop filter by pass valve 7FS-V116 (FP 229)b) Fails openMechanicalFailure,contamination, operator errorPurification water by passes filter. Loss
of filtrationVery low differen-tial pressure reading on PDI 415None WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 6 of 10)Revision 11 (05/01)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects21.Purification filter isolation valve 7FS-V111(FP 228),7FS-V113 (FP 234)a) Fails closedb) Fails openMechanical failure,blockage, operator errorMechanicalfailure Loss of purificationloop, high pressurereading at PI 412 and low differential pressure reading at PDI 415Cannot isolate filterfor repair; no impact during normal operationHigh pressurereading at PI 412 and lowdifferentialpressure reading at PDI 415 Leakage during replacementParallel Redundantflow path through filter bypass 7FS-V116Series isolation valve Loss of filtrationduring repairValve isnormally openValve isnormally open22.Fuel poolion exchanger isolation valve 7FS-V114(FP 236),7FS-V117 (FP 248),
7FS-V120 (FP 252)a) Fails closedb) Fails openMechanicalfailure, blockage, operator errorMechanicalFailure Loss of circulation ofeither fuel pool or refueling pool water through the purification filters and ion exchangerNoneLow differentialpressure reading at PDI 416NoneParallel ion exchangerby pass path for 7FS-V114, 7FS-V117, and 7FS-V119 failure.
None for 7FS-V120None23.Fuel poolionexchanger differential
pressure indicator PDI 416Fails to indicate correct valueMechanical,electrical failureNo impact on fuel poolpurificationPeriodic testingNone WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 7 of 10)Revision 11 (05/01)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects24.Fuel poolion exchanger a) Lossof flowValve fails closed or strainer clogs, operator error Loss of circulation ofeither fuel pool or refueling pool water through the purification filters and ion exchangerHigh Pump Dischargepressure at PI 412and low differential pressure reading at PDI 416Parallel ion Exchangerbypass pathb) Failsto remove contamin-antsAge andHeavy LoadBuildup of radioactivecontaminants in either the fuel pool or the refueling poolLocal SampleParallel Filterbypass path25.Ionexchanger Y Strainer 7FS-S153 Loss of functionImpurities, particulate matterSame as 24 (a)Same as 24 (a)Same as 24 (a)26.Ionexchanger By-Pass valve 7FS-V121 (FP 251)a) Fails closedb) Fails openMechanicalbinding Operator errorInability to by pass ionexchanger during maintenance,Effective Loss of purifica-tionthrough the ion exchanger for either the fuel pool or refueling pool,until a repair is madeHandle PositionLocal sampleLow Differential pressure indication on PDI-416RepairPurification loopcan be safely shut down until a repair is madeValve Normally closed WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 8 of 10)Revision 11 (05/01)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects27.Isolation valve between Refueling Canal DrainPump andvarious
- systems, 7FS-V137, 7FS-V138, 7FS-V139, 7FS-V140, 7FS-V176, 7FS-V177a) Fails closedb) Fails openMechanical failureMechanicalbinding, seatleakageBuild up of radioactivecontaminants in refueling canal, spent fuel cask
storage area or spent fuel cask decontamination pit.
Drains part of refueling
canal, spent fuel cask decontamination pit inventory to fuel pool.Local sampleFuel pool water levelRepairSeries Redundantisolation valve N/A28.RefuelingCanal DrainPumpisolation 7FS-V127, 7FS-V152a) Fails closedb) Fails openMechanical failureMechanicalbinding, seat leakageSame as 27 (a)Same as 27 (b)Local SampleFuel pool water levelRepairSame as 27 (b)29.Purificationpipinga) Breakupstream of pumpAccidentLoss of purification loopuntil repair is completed.
Possibly some loss of water from fuel pool due to siphoning.Low pool levelalarm (LS-420) ifthere is siphoning.Low pump discharge pressure (PI-412)Siphon breakerholes at EL 40'-6" this is sufficient.Purification can besafely suspended while repair is accomplished.b) Breakdownstream of pumpAccidentPurification pump will tend todrain the fuel pool until the pump
is shutoff; loses suction.Possibly loss of water from pooldue to siphoning from discharge pipe.Low Pool Level alarm(LS-420)The discharge leg extendsonly a short distance below the fuel pool water line.
Therefore siphoning will cease before level drops excessively.
WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 9 of 10)Revision 11 (05/01)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects30.PoolCooling Pipinga) Breakupstream of pumpsb) Breakdownstream of
HXAccidentAccidentPartial draining of fuel pool, lossof cooling.Cooling pump will tend to drainpool until pump is shut off; loses suction. Possible some loss of water from fuel pool due to siphoning from discharge nozzle.Low pump dischargepressure alarm.
(PS-403) Low fuel pool level alarm (LS-420)Low pool levelalarm (LS-420)The pool cooling suctionnozzle extends only a short distance below the pool water line, therefore siphoning will cease before serious draining occurs.
Same as 29 (a)c) Breakbetween pump and HXAccidentCooling pump will tend to drainpool until pump is shut off.
Possible some loss of water fromfuel pool due to siphoning fromdischarge nozzle.Low pump dischargepressure alarm.
(PS-403)
Low fuel pool level alarm.
(LS-420)Same as 29 (a)31.Refueling canaldrain pipingBreakdownstream of pumpAccidentPossibly some loss of water frompool due to siphoning from discharge pipe.Low Pool Level alarm(LS-420)Same as 29 (b)32.ComponentCooling Makeup pumps to poolisolation valvea) Fails closedMechanical failure, corrosionCannot supply fuel pool with ccmakeup water when required.OperatorRepairValves arenormally closed.7FS-V129(FP 243),
7FS-V131 (FP 201b) Fails openContamination,seat leakageSame as 31Low pool level alarm(LS-420)Series Redundant isolationvalve and same as 29 b.
WSES-FSAR-UNIT-3TABLE 9.1-4 (Sheet 10 of 10)Revision 11 (05/01)FAILURE MODE AND EFFECTS ANALYSISFUEL POOL SYSTEMNo. Name Failure Mode Cause Symptoms and Local Effects Including Dependent FailuresMethod of Detection Inherent Compensating ProvisionEffect UponRemarks and Other Effects33.Fuel Poolpump check
valve 3FS-V10B8 (FP-207),3FS-V105A(FP-206)a) Fails closedMechanical failure,blockage corrosionCentrifugal pump driving againsta dead head; high pressure indication (PI 401, 402) loss of one fuel pool pump flow supply leg.High pressure indication;(PI 401, 402) periodic testingNoneEquilibriumtemperature offuel pool will be increased.b) Fails openMechanical failure,seat leakageReverse Flow: through idle pumpPeriodic TestingNoneEquilibriumtemperature of fuel pool will be increased.34.Fuel poolpurification pump check
valvea) Fails closedMechanical failure,blockage, corrosionCentrifugal pump driving againsta dead head; high pressure indication; (PI 402) loss of fuel pool purification loop.High pressureindication; (PI 402)
Periodic TestingNone for 7FS-V110. BypassIX through 7FS-V121 for 7FS-V115 failureCannot purify fuelpool when required7FS-V110(FP 225),7FS-V115(FP 237)b) Fails openMechanical failure,seat leakageNo impact on fuel pool purificationsystem.Periodic TestingNone35.RefuelingCanal Drain Pump line check valve 7FS-V136a) Fails closedb) Fails openSame as 34 (a)Same as 34 (b)Centrifugal pump driving against a dead head.Possible loss of water from pooldue to siphoning from discharge pipe.Periodic TestingPeriodic TestingNoneSame as 29 b.(DRN 99-1097)
WSES-FSAR-UNIT-3 TABLE 9.1-5 (Sheet 1 of 2) Revision 14 (12/05)
MAJOR TOOLS AND SERVICING EQUIPMENT REQUIRED FOR REFUELING FUNCTIONS Quantity 1. R.V. Stud Tensioners 3 2. R.V. Stud Tensioners Pump Unit 1
- 3. R.V. Stud Storage Stand (4 hole) 1
- 4. Lifting Tools for R.V. Studs and Nuts 3
- 5. R.V. Guide Studs 2
- 6. Source Handling Tool 1
- 7. Head Lift Rig Spreader 1 (DRN 03-1341, R13) 8. Stud Tensioning Hoists 6 (DRN 03-1341, R13) 9. Stud Hold Plugs 54 10. Surveillance Handling Tool 1
- 11. Reactor Coolant Pump Stud Tensioner 2
- 12. Reactor Coolant Pump Seal Cartridge Lift Rig 1
- 13. UGS Lift Rig 1
- 14. CSB Lift Rig 1
- 15. Hydraulic Power Unit 2 (DRN 02-176, R14) 16. Pool Seal Hatch Covers 6 (DRN 02-176, R14) 17. CEA Transfer Carrier 4 18. Refueling Machine 1
- 19. Transfer Carriage 1
- 20. Upending Machine 2
- 21. Underwater TV System (2 cameras) 1
- 22. Sipping Console 1 WSES-FSAR-UNIT-3 TABLE 9.1-5 (Sheet 2 of 2) Revision 7 (10/94)MAJOR TOOLS AND SERVICING EQUIPMENT REQUIREDFOR REFUELING FUNCTIONSQuantity23.R.V. Stud Support 54 24.Internals Lift Tie Rod Assembly 125.Containment Polar Crane 126.Cask Handling Crane 127.Transfer System Cable Hook and Wrench 1 28.Spent Fuel Handling Machine 129.New Fuel Elevator 1 30.New Fuel Handling Tool 1 31.Spent Fuel Handling Tool 132.CEA Handling Tool (Short) 133.Reactor Vessel Head Lift Rig 134.Hydra-Set Precision Load Positioner 1 WSES-FSAR-UNIT-3 TABLE 9.1-6 (Sheet 1 of 2) Revision 15 (03/07)
REACTOR BUILDING CRANE DATA
A) BRIDGE (DRN 06-843, R15)
Circular Runway length, ft., in. 419 ft. (DRN 06-843, R15)
Bridge weight, lbs. 376,400 lbs. Bridge span, ft., in. (Diameter) 136 ft. - 4 in.
Bridge motor Hp (2) 7.5 Hp @ 900 RPM Type of wheels Straight thread Number of wheels 8 (DRN 06-843, R15)
Maximum speed, FPM 60 FPM (DRN 06-843, R15)
Type of controls P&H Static Stepless Control Bulletin 562/563 Type of brake 8 in. CDR Type of bumpers None (Circular Crane)
B) TROLLEY
Length of trolley travel, ft., in. 108 ft. - 7 in.
Trolley weight (net) lbs. 127,000 lbs.
Trolley weight (with load), lbs. 527,000 lbs.
Distance between running rails, ft., in. 29 ft. - 0 in.
Trolley drive Hp (2) 3 Hp @ 600 RPM Type of wheels Straight thread Number of wheels 4 Maximum speed, FPM 30 FPM Type of controls P&H Static Stepless Control Bulletin 562/563 Type of brakes CDR 5 in.
Type of bumpers Spring (Chocks)
C) HOIST MAIN AUXILIARY
Lifting capacity, ton 200 ton 30 ton Drum size (pitch circle 42 1/4 in. 26 1/8 in.
diameter) in.
Rope type I.P.S. 6x46 AAA I.P.S. 6x37 IWRC Rope size, in. diameter 1 3/8 in. diameter 3/4 in. diameter Diameter top block 33 in. 22 1/2 in.
sheaves (pitch circle diameter) in.
Diameter hook block 33 in. 22 1/2 in. & 25 in.
(pitch circle diameter) in.
Type equalizer Sheave Sheave Type of hook P&H 646 Forged Forged Type of hook material AISI 4320H AISI 1045 WSES-FSAR-UNIT-3 TABLE 9.1-6 (Sheet 2 of 2) Revision 15 (03/07)
REACTOR BUILDING CRANE DATA
C) HOIST (Cont'd) MAIN AUXILIARY
Hook test load, ton None None Maximum travel of hook, 100 ft - 0 in 100 ft - 9 in Ft., in. (DRN 06-843, R15)
Maximum hoist speed, FPM 6 FPM 30 FPM (DRN 06-843, R15)
Number of parts of rope 14 8 c/c sheaves in highest 64 1/2 in. 84 1/2 in.
position Type of control Eddy Current Eddy Current brakes Type of holding (2) 16 in. SBE (2) 13 in. SBE brake Type of control P&H Static Stepless P&H Static Stepless Control Control Bulletin 562/563 Bulletin 562/563
D) DESIGN LIFE
Number of rated capacity load cycles 20,000 minimum (structural members)
Gearing and shafting fatigue life 10 million minimum (cycles of component loading)
WSES-FSAR-UNIT-3 TABLE 9.1-7 (Sheet 1 of 2) Revision 305 (11/11)
FHB BUILDING CRANE DATA (CASK CRANE)
(EC-14270, R305)
A) BRIDGE Runway length, ft., in. 77 ft. - 0 in.
Bridge weight, lbs. 198,575 lbs.
Bridge span, ft., in. 62 ft. - 8 in.
Bridge motor, Hp (2) 7 1/2 HP @ 1200 RPM Type of wheels Straight Thread Number of wheels 8 (eight)
Maximum speed, FPM 50 FPM Type of controls Smartorque G+S3 AFD Bulletin 427S Type of brake (2) Motor-Mounted Disc Brakes @ 50 FT-LB Type of bumpers Spring
B) TROLLEY
Length of trolley travel, ft., in. 52 ft. - 6 in.
Trolley weight (net) lbs 60,500 lbs Trolley weight (with load), lbs 310,500 lbs Distance between running fails, ft., in. 16 in. 0 in.
Trolley drive, Hp (2) 3 HP @ 1800 RPM Type of wheels Straight Thread Number of wheels 4 (four)
Maximum speed, FPM 50 FPM Type of controls Smartorque G+S3 AFD Bulletin 427S Type of brakes (2) Motor-Mounted Disc Brakes @ 15 FT-LB Type of bumpers Spring (Chocks)
C) HOIST MAIN AUXILIARY (2)
Lifting capacity, ton 125 ton 15 ton Drum size (pitch circle dia.) in. 42 1/4 in. 20 Rope type 6x37 1 5/8 in. 6x37 3/4 in.
Stainless Steel, Stainless Steel, Type 304 IWRC Type 304, IWRC Rope size, in. diameter 1 5/8 in. 3/4 in.
Diameter Top Block Sheaves N/A. 9 1/2 in.
(pitch circle diameter) in.
Diameter Hook Block (pitch 39 in. 15 in.
circle diameter) in.
Type of equalizer Bar/Hydraulic Sheave Type of hook Forged Forged Type of hook material SAE 4340(34CrNiMo6) AISI 1045 Hook Test load, ton 250 ton None Maximum travel of hook, ft., in. 70 ft. 0 in. 79 ft. 0 in. (EC-14270, R305)
WSES-FSAR-UNIT-3 TABLE 9.1-7 (Sheet 2 of 2) Revision 305 (11/11)
FHB BUILDING CRANE DATA (CASK CRANE)
(EC-14270, R305)
C) HOIST (Cont'd) MAIN AUXILIARY
Maximum hoist speed, FPM 5.0 FPM 25 FPM Number of parts of rope 12 4 c/c sheaves in highest position N/A 37 7/8 in.
Type of control brakes Magnetorque Mechanical Load Type of holding brakes (2) 16 in. SBE Disc Type of control Smartorque VG+S3 5 step A.C Bulletin 427V Magnetic (EC-14270, R305) D) DESIGN LIFE
Number of rated capacity load cycles 20,000 minimum (structural members)
Gearing and shafting fatigue life 10 million minimum (cycles of component loading)
WSES-FSAR-UNIT-3 TABLE 9.1-8 (Page 1 of 2) Revision 304 (06/10) (DRN 99-1097, R11)
SUMMARY
OF REACTIVITY PERTURBATIONS FOR STANDARD CONFIGURATIONS
Region 1 Region 2 (DRN 05-1365, R14-A; EC-18742, R304)
Soluble boron (ppm) 85 448 Design basis burnup at 5.0 wt% initial enrichment 0.0 34.1 GWD/MTU Reference k eff (MCNP4a) 0.9246 0.9173 MCNP4a calculational bias, k 0.0012 0.0012 Temperature bias to 80.33 °F (CASMO-4), k 0.0024 0.0029 Burnable absorber depletion bias, k NA 0.0070 Depletion uncertainty, k +/-0.0000 +/-0.0125 Rack tolerances uncertainty, k +/-0.0136 +/-0.0042 Fuel tolerances uncertainty, k +/-0.0032 +/-0.0036 Calculational uncertainty, k +/-0.0014 +/-0.0014 MCNP4a code bias uncertainty, k +/-0.0090 +/-0.0090 CASMO-4 code bias uncertainty, k +/-0.0025 +/-0.0025 Statistical combination of uncertainties, k (1) +/-0.0169 +/-0.0166 Maximum k eff 0.9450 0.9450 Regulatory Limit 0.95 0.95 1. Square root of the sum of squares (DRN 99-1097, R11; EC-18742, R304)
WSES-FSAR-UNIT-3 TABLE 9.1-8 (Page 2 of 2) Revision 304 (06/10)
SUMMARY
OF REACTIVITY PERTURBATIONS FOR REGION 2 CHECKERBOARD CONFIGURATION (DRN 99-1097, R11; EC-18742, R304) 5 wt% U-235 fuel with empty cells Fuel assemblies at
27 GWD/MTU with lower reactivity fuel Soluble boron (ppm) 0.0 524 Design basis burnup at 5.0 wt% initial enrichment 0.0 43.2 GWd/MTU Reference keff (MCNP4a) 0.8256 0.9152 MCNP4a calculational bias, k 0.0012 0.0012 Temperature bias to 80.33 °F (CASMO-4), k 0.0034 0.0025 Burnable absorber depletion bias, k 0.0070 0.0070 Depletion uncertainty, k +/-0.0000 +/-0.0157 Rack tolerances uncertainty, k +/-0.0053 +/-0.0040 Fuel tolerances uncertainty, k +/-0.0029 +/-0.0039 Calculational uncertainty, k +/-0.0014 +/-0.0012 MCNP4a code bias uncertainty, k +/-0.0090 +/-0.0090 CASMO-4 code bias uncertainty, k +/-0.0025 +/-0.0025 Statistical combination of uncertainties, k (1) +/-0.0112 +/-0.0191 Maximum k eff 0.8484 0.9450 Regulatory Limit 1.0 0.95 1. Square root of the sum of squares (DRN 99-1097, R11; EC-18742, R304)