ML20056D606

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Spes Sys Description
ML20056D606
Person / Time
Site: 05200003
Issue date: 12/17/1986
From: Cattadori G, Rigamonti M
AFFILIATION NOT ASSIGNED
To:
Shared Package
ML20056D594 List:
References
SIET-NT-032, SIET-NT-032-R01, SIET-NT-32, SIET-NT-32-R1, NUDOCS 9308170156
Download: ML20056D606 (188)


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{{#Wiki_filter:_ LT 5 PES 5YSTEM DE5CRIPTION G. Cattadori, M. Rigamenti This work, part of ENEA's LWR Safety Research Program, ) was performed in the frame of ENEA - SIET contract ( rr.ilestene HE/AB 36) 9308170156 930813 PDR ADOCK 05200003 ^ PDR N

5PE5 5YSTEM DESCEIFTION G. Cattadori, M. Eigamenti This work, part of ENEA's Lk'R Safety Research Program, was performed in the frame of ENEA - SIET contract ( milestone NE/AB 36)

I REV. PAGE N. ISSUED AUTHOR APPROVED SIET NT-032 Mb#' 1 180 17/12/85 } l Distribution list SIET ENEA G. Cattadori P. Ficara TERM /RISIL (2 copie) GP. Gaspari G. Pala::1 TERM / DISP C. Medien G. Petrangeli DISP /SER M. Pe::ani G. Saponaro DISP /SER/CORIC R. Ravetta G. Sgalambro DISP /ACO/PROCS M. Rigamenti M. Vignolini ERM/FIP/SISREF F. Rossi ENEA/ TERM /RISIL/ Arch. SIET/ Arch. I

-fl n - b .i 6 i f ? '. t s C0NTENTS ' F . 1 m t. W ' F f s Nomenclature.............................................. 1 . l l Abstract.................................................. 4 I 1. Introduction.............................................. 5 j a 2. SPES characteristics and functions........................ 7 3. Description of test apparatus............................. 13 3.1 S P ES l oc a t i on............................................ 13 - [ 3.2 SPES gencral. data..........................'.......... 13 i 3.3 Primary coolant system.................................. 13

'3.3.1 Power channel pressure vessel....................... 14 x3.3.2 Pcwer channel rod bundle............................ 15

<a.3.0 _r-s ur i n e r........................................... 17 3.3.4 Primary recirculation pumps........................... 18 l r 3.3.5 Primary coolant loop piping.......................... 19- -3.3.6 Steam generator tube bundle.......................... 21 i i3.4 Secondary coolant system................................ 22-t 't 3.4.1 Steam generator....................................... 23 3.4.2 Secondary piping system.............................. 26 3.5 Emergency core cooling system........................... 27 3.6 PCS charging and letdown lines.......................... 28' f e 3.7 SPES supplement systems................................. 29 b M p 7 - 1 f t I h

r - ? ) 6 . ) I . t ' i L 1 a i = 1 i I l i .i Contributcrs : l l 1 i The SFES control and data acquisition system specifications has been written by Dr. F. Rossi; the graphic part of the report has i been' performed by Mr. E. Gabbi I 1 i f 6 ? . i p 1 i -l 'f - i i b 4 . h E s n w

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3.8 Valves............................................... 30 3.9 Component and piping thermal insulation............. 31 4 Blowdown system.....-.................................. 32' 5. Instrumentation....................................... 33 J, b 5.1 Thermocouples and thermoresistances................. 34 5.2 Flowmeters......................................... 35 .I 5.3 Fluid level sensers................................. 35 l v 5.4 Absolute and differentici pressure trasducers....... 35 t 1 5.5 Power meters................... ..................... 36 5.6 densitemeters.................................. 36 6. Control and data acquisition system................... 37 'j t 6.1 Programmable logical controller. PLC................ 37 6.2 Process control system............................... 38 6.3 Supervisory computer.............. .................. 38 j 6.4 Data acquisition sucsystem.......................... 39 i -r t 2 Appendix "A" - Prirary piping layout..................... 148 .6 Appendix "B" - Secondary piping layout.................. 162 Appendix'"C" - Emergency and auxiliary piping layout..... 175 j 3 i i r i, i T i ) h h I B h . i, l ? II

LIST OP TAELES ~ 3.2/1 Comparison of SPES and PWR characteristics.................... 41 /2 Volume comparison between SPES and PXE-PUN.................... 42 /3 Main facilities for safe ty research........................... 43 3.3/1 Materials o f PCS majer components............................. 44 {; t 3.3.1/1 Power channel pressure vessel data.......................... 45. .i 't /2 Power channel volumes, cross flew areas'and metal weights... 46 3.3.2/1 Power channel rod bundl e data................................ 47 3.3.3/1 Pressurizer main data....................................... 48 p 3.3.4/1 Primary recirculation pump characteristics................. 49 /2 Nominal data of the pump sealing system..................... 50 s 3.3.5/1 Main features of the primary piping......................... 51 l /2 Hot leg-1 characteristics................................. 52 j /3 Hot leg-2 characteristics.................................. 53- /4. Hot leg-3 characteristics................................... 54 /5 Loop seal-1 characteristics................................. 55 L /6 Loop seal-2 characteristics................................ 56 /7 Loop seal-3 characteristics................................. 57' /8 Cold l eg-1 charac teristics................................. 58 /9 Cold leg-2 characteristics................................... 59 i /10 Cold leg-3 characteristics................................. 60 j /11 Downcomer characteristics.................................. 61 /12 Surge line chara cteris tics.................................. 62 ? I t i k I e l l I r III L

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? I I 3.3.5/13 Oore bypass and downcomer-upper head bypass characteristics. 63 ..i f /14 Spray line characteristics................................. 64 j 3.3.6/1 Steam generater tuce bundle data............................ 65 - I l /2 Steam generator U-tube bundle geometrical data.............. 66 I 1 /3 U-tube measured lengths.................................../. 67 3.4.1/1 Steam generater general data ...............................,.68 t /2 Steam generator thermalhydraulic data....................... 69 /3 Steam generator volumes, cross ficw areas and weights....... 70 l ~f 3.4.2/1 Secondary piping system general data........................ 71 t' i /2 Secondary piping system characteristics..................... 72 l 3.5/1 Accumulator and surge line general data.....-.................. 75 l /2 Injection pump and HPIS/LPIS characteristics................... 76 l 3.8/1 Air actuated control valve specifications.................... 77 i i* /2 Air actuated isolation and relief valve specifications........ 78 /3 Safety valve specifications................................... 79 I s /4 Hand actuated contro and isolation valve specifications...... 80 la /5 Non return valve specifications............................... 81 i 3.9/1 Thermal insulation thic kness.................................. 82 5/1 Summary of SPES measurements.................................... 83 i /2 Acronyms of instrumentation tags................................ 84 l /3 Experimental measurement tag list.............................. 85 /4 Piping instrumentation location................................. 101 5.2/1 Venturi tube specifications................................... 103 ? i /2 Ori fi ce nozel e s peci fi cati ons................................. 104 s- } l 5 J I e r 1 I IV j i i

~ ^! i .' i ,.1 .t .f LIST O' F FIGUPE5 l t B t E 3.1/1 General view of SPES inside the "Emilia" power statien....'... 105 -i /2 Plan view of SPES main components.............................. 106 r j /3 Elevation view of SPES main components....................... 107 i 3.2/1 SPES schematic flow diagram................................... 108 l 3.3.1/1 Power channel pressure vessel.............................. 109 f /2 Power channel pressure vessel lower section................ 110 r /3 Power channel pressure vessel active zone.................. 111 /4 Power channel pressure vessel upper section.................'112 l ? /5 Detail'of drilled plate between upper plenum and upper head'.113 .l /6 De tail o f core s"eport plate............................... 114 t 3.3.2/1 Powe r channel rod detail................................... 115 f /2 Rod bundl e spac er de tail.................................... 116 >i /3 R od bundle wall thermocouples location '..................... 117 -1 i 3.3.3/1 Pressurizer cross section.................................. 118 /2 Pressurizer spray no::le detail............................ 119 I 3.3.4/1 Primary recirculation pump cross section................... 120 l, /2 Primary recirculation pump H-0 characteristics............. 121 /3 Pump speed-flowrate theoretical curves..................... 122 /4 Primary pump mechanical seal arrangement................... 123 l 3.3.5/1 Power channel d o wnc ome r.................................... 124 l l /2 Sketch of primary piping / loop-l.......................... 125 /3 Ske tch of primary piping / loop-2.......................... 126 /4 Sketch of primary piping / loop-3.......................... 127 j /5 Sketch of downcomer....................................... 128 1 r i l s I i V -j I a

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3. 3. 5/6 5 ketch of surge line piping............................... 129 1

/7 Loose flange detail.........................-.............. 130 l 3.3.6/1 Steam generator tube bundle instrumentation............ ;.. 131 j 3.4.1/1 Steam generator general arrangement....................... 132 [ /2. Steam generator lower section.............................. 133 i t /3 Steam generator upper section............................. 134 i /4 Steam generator tube bundle supporting cage............... 135 t /5 Steam generater riser cross section and spacer grid....... 136 P /6 Steam generator dryers.................................... 137 I 3.5/1 Accumulator cross section................................... 138 I 5/1 SPES system loop 1 instrumentation........................... 139 l /2 SPES system loop 2 instrumentation............................ 140 /3 SPES system loop 3 instrumentation........................... 141 i /4 Power channel rod bundle instrumentation...................... 142 i /5 Power channel measurement arrangement......................... 143 l /6 Pressurizer measurement arrangement........................... 144-r /7 Steam generator measurement arrangement....................... 145 j i 6/1 Data acquisition and control system........................... 146 6.2/1 Process control diagram..................................... 147 f Appendix "A" t t ? Al Hot leg n.1.................................................... 149 ] A2 Hot leg n.2.................................................... 150 A3 Hot leg n.3.................................................... 151 ti L ? e 4 VI 4 l i v. ,_,r

E f 1[ E I. 'E t A4 Loop seal n.1.................................................. 152 + A5 Loop seal'n.2.................................................. 153 A6 Loop seal n.3.................................................. 154 i A7 Cold leg n.1................................................... 155 i AB C o l d l e g n. 2................................................... 156 A9 C o l d l e g n. 3................................................... 15 7 f A10 Surge line.................................................... 158 v All Core bypass................................................... 159 f A12 Downcomer upper head bypass................................... 160 r i i '4 A13 Pressurizer spray line........................................ 161 I i I Appendix "B" ? [ i El M a in s t e am l ine n.1............................................ 163 l 4 B2 Main steam line n.2..................................... ....... 164 j t B3 Ma in s te am l i n e n. 3............................................. 16 5. B4 Main s team l ine he a de r......................................... 166 - k B5 Fe e dwa t e r l i n e n.1............................................. 167 B6 Fe e d wa t e r l in e n. 2............................................. 168 E7 Fe e dw a t e r l ine n. 3.............................................. 16 9 i BB F e e dwa t e r h e a d er............................................... 170 -l E9 Steam dump...................................................... 171 i B10 Preheater line................................................ 172 4 Bil Pre he a te r byp as s.............................................. 173 i.> B12 Emergency feedwater lines......'............................... 174 I i i l I . t t + .I 1 1 I t i 5 VII i: 1 .--n.

... ~. e 1 6 b .i. I, 'l r Appendix "C" C1 Emergency lines from IP-1...................................... 176 l C2 Accumulater n.1 surge line............................'......... 177 f C3 Accumulator n.2 surge line .....................................,178= s, C4 Accumulator n.3 surge line...................................... 179 I t i C5 Charging and letdcwn line...................................... 180 i t - 1 6 i I f .t f s t I .7 I - + 4 l i t - o ? ? l ) ? -j r F I ';I t } - i t i . I i I i P I i . ij I . J .VIII . 1 1 1 e '.I

.- ~.. 1 .4; i . l I N O M E N C L-A T U R E. t .i t - i i AIS accumulator injection system BAF bottom of active fuel-EP bypass / booster pump l 3V ball valve SW butt welding CL cold leg CPU central-process unit CV check valve CVCS chemical and volume control system D deaerator., diameter i DC downcomer . ) ? CD drag disk -t* ECCS-emergency core cooling system i ETWL emergency feedwater lines i EFWS emergency feedwater system j i EP emergency pump EFL emergency pump line ET emergency tank - l i ETL emergency tann line 707 flow centrol valve l FP feed pu=p TWL feedwater line f HCV hand control valve l HE heater exchanger HL hot leg i 1 I . i i I

...~. _. .t i a i i l s I i HPIS high pressure injection system l HV hand valve ID inner diameter L length { LCV level control valve LDL letconwn line .i LM large male l r F LP leveel pump '} LPIS low pressure injection system LR long radius LS locp seal LVDT. low voltage displacement trasducers r' MSL main steam line i CD outer diameter c, P power -r PC power channel e PCL pressurizing and charging line PCS primary coolant system + PCV pressure control valve PHL preheater line r PLC programmable logical controller i PORV power operated relief valve i PR pressurizer t PV pressure vessel R radius i RAM random access memory. i RF raise face RP recirculation pump l 2

9 I ..s F RT - reservoir tank. I t RTD thermoresistance RTJ ring type joint SAD data acquisition system SBLOCA small break loss'of coolant accident i SC steam condenser SCS secondary coolant system SDL steam dump line SG steam generator SL surge line- ~ i l SS steam s,eparator { l SV safety valve l SW socket welding i TAT top of active fuel TC thermocouple [ F TCR heated thermocouple TCV temperature control valve-f V volume WSL water spray line j X-steam quality l l e ~! .I q .k 1 ? -i h i I 3 1, a i, k

1 s .j J i 1 ABSTRACT t ~- 1 I i This document provides the infermation together with all the [ necessary data for an exaustive analysis of the experimental results to be obtained on the SPES experimental facility. The information concerns. i t - SPES system descriptien ; i t - process and measurement instrumentation ; f - basic data for computer code inputs ; 1 - data processing system. j ' I ~ t i . I ? i t t o i r 5 t ~ l I r ~ t i I r i 4 1 1 i e i t 4

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1. INTRODUCTION i

i ~! The approval in 1981,of the National Energy Plan which foresees : { i the costruction of FWR's power stations for an overall power of i 6000 MWe convinced ENEA ( Comitato nazionale per la ricerca e lo sviluppo dell'energia nucleare e delle energie alternative) to j undertake an experimental programme in the_ safety field in the I frame of which the design and the costruction of an integral i facility simulating the italian FWR is the first main geal. -{ i Such a facility named SPEE : Simulazione Pwr per Esperienze di 1 Sicurezza ) and whose construction started at SIET ( Societa' Informa:icn1 Esperienze Termeldrauliche ) in Rarch 1983.has the I following aies: I - to maintain and to increase knowledge in the field of safety i related technology; - to supply experimental results for accident analysis codes: - to evaluate the effects of the operator interventien on the '!( plant; l 1 - to test possible plant modifications. The SPES is designed to simulate thermal-hydraulic phenomena 4 peculiar to SELOCA's and cperational transients by having the same loop number as the reference reactor by maintaining the prototypical component elevations and by scaling core power and i volume 1/427. t i i f

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. i .? ih ( t -v The report describes the SFES system philosophy, design and t costruction the whole instrumentation and data processing,and .[ t gives all the geometrical and physical data for safety ecmputer code inputs. i f The SPES facility has attracted world interest; in particular ENEA and USNBC (United States Nuclear Pegulatcry' Commission) i have finaliced a cooperation contract regarding the exchange cf h computer codes and experimental data. I r 't I i i k i I i k 1 l L -I - I 4 I i I f 4 a ? i I i ~I l i 1 4 t 6 i - i

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2. SPES CHARACTERISTICS AND FUNCTIONS.

[ ti t The SPES integral test facility is a scale model of the italian f i PWR ( Westinghouse 313 type, 3 loops 2775 MWth core power ) aiming at the simulation of the thermal-hydraulic phenomena t following SBLOCA's and operational transients occuring in the reference plant. i In particular, SPES system simulates - the whole primary circuit; f r - the secondary system restricted to: . steam generator secondary side, . main feed water lines downstream the isolation valves, j . main steam lines upstream the turbine stop valve; I I - the most significant auxiliary and emergency systems: . charging and letdown systems, i . safety injection systems (HPIS, LPIS, accumulators, EFWS) . steam dump. _} t i t f ? P D s P ) J t I 7 l 1

m__.-. 'i f .: I 1 The SPES main characteristics are: ~! f - fluid water both in the primary and' l in the secondary circuit'

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-l - loop number 3 ~j ( I I - design pressure. MPa 20 (primary circuit) l t ) 10 (secendary circuit) - design temperature, 'K S38 (primary circuit) 583 (secondary circuit) .f f - nominal power ! electrical heating), MW 6.5 l ), - maximum power, MW 9 II - scaling 1: 1 (elevation) .f-t 1: 427.3 (volumes) ? The scaling ratio has been used as a general philosophy in f scaling fluid volumes, flowTate, power and cress flow areas j 'I I b 'I i 8 ~I i

-. ~. i i h together with other-criteria which concern the preservation, in any SPES component, of the following parameters : f i - fluid thermodynamic conditions ( pressure and enthalpy )- f - power-to-flowrate ratio ; i ' i - transit time of the fluid ; 't I - heat flux. Further scaling criteria were applied to design the individual t SPES components; for example in the components, with fluid flowing l t'l vertically the elevations have been preser"ad to cotain a good i I reproduction of natural circulation phenomena. On the contrary., i in the components where the prevailing flow direction is d horizontal, the Froude numcer conservation has been imposed to t preserve, as much as possible, the flow pattern transition in ? horizontal tubes. f The particular scaling criteria for the main components of the ~ l i SPES loop are now described. 4 + l VESSEL DOWNCOMER i - Vertical elevations are preserved. h f Observations: the downcomer geometry is tubular to obtain the minimum pressure drop distorsion compatible with the volumetric l I criterion and the elevation preservation. f i r i e 3 h 9 -i 4 r

i I I i POWER CHANNEL - Vertical elevations are preserved; ? - the bundle geometry (red pitch and outer diameter) is preserved. t } Observations the vertical elevations are preserved only between j the inlet and outlet nozzles of the fluid, because the lower j i plenum and upper head elevations have no influence on the natural circulation phenomena. ) PRIMARY COOLANT PUMPS 't i 1 - The nominal head is approximately preserved ; .j l - the coastdown behaviour is reproduced. I 1 l i i Cbservatiens : the nominal head may be slightly different in I comparison with the PWR pumps due to some small distorsions in the i i loop pressure drops ; the coastdown behaviour (flowrate transient f with loss of the electric power) is reproduced by providing a suitable flywheel on the pump shaft.Furthermore in particular i i cases (i.e. small break with pumps on) a procedure to establish ~ the pump speed which reproduces the same head and flowrate across the pump nas been defined. .l c b I l f R l 1 l 1 -10 i 1 I .\\

-. ~ h i 'f s f I t STEAM GENERATORS - l 1 i f - Vertical elevations are preserved both in the primary and in the i f secondary side ; I - the bundle geometry (tube pitch, diameter and thickness) is preserved. ] r ~ t Observations: the vertical elevations in the secondary s'ide are { preserved just below the tcp of the primary steam separator; indeed, the steam dome elevation has no influence on the natural -i { circulation phenomena. l N 1 J - MAIN LOCP PIPING i - The Froude number is preserved, f l ) i 4 { Observations; in the pump suction piping (loop seal) it is impossible to preserve simultaneously the volume, the lowest elevation of the tube and the Froude number. The elevation is very .l t important in small break transients because of the loop seal I l clearing phenomenon. Therefore, two different loop seal j ( geometries will be available: the first one will preserve volume and elevation and the second one will preserve volume and Freude i number. Either of these geometries will be used according to the i phenomena expected for each test run. l 1 J l i i l ) l j 1 11 J i

.m i 7 ? FRESSURITER t

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- The elevation of the nominal water level is preserved ; j - the level swelling phenomenon will be reproduced.' 7 Observations: the level swelling phenomenen can occur in the pressurizer because of the flashing of the liquid here ' contained or cecause of a steam inflow from the primary circuit; this -{ phenomenon has a significant influence on the quality of the fluid discharged.through the pressurizer relief and safety valves. I 1 The preservation of the level swelling has been obtained by i imposing the average void fraction in the SPES pressurizer equal to the ?WR one, for similar thermal-hydraulic conditions; the void n fraction has been calculated acccrding to the Wilson model for .h j bubble rise velocity. .( In the future, however, it will be possible, if necessary, to substitute enis pressurizer vessel with a full height one. d SAFETY INJECTION SYSTEM i 'I t - The accumulator nominal water level is preserved. I Observations: concerning the safety injection pumps (HPIS and I i LFIS), an external circuit will supply the cold legs with the correct flowrate for a given pressure in the primary system. f i i i i + h i t i t 9 12 l 5

!I 1 l 3. DESCRIPTION OF TEST APPARATUS i ? 3.1 SPES location 'i .\\ i. The SPES facility is located at the SIET-Piacenza Laboratories i and is built inside the "Emilia" oil fired power station as shown in l l Fig.3.1/1' (general view). Fig.3.1/2,3 give the plan and elevation h schematic views respectively. i t 5 3.2 SPES general data The schematic flew diagram of SFES is shown in Fig.3.2/1 l Tabs. 3.2/1 + 3.2/3 give the comparisen of tne SFES main characteristics with respect to Ph'R-PUN (the reference plant) and to other safety experimental facilities. i' 3.3 Primary coolant system 'l 4 The primary coolant system (PCE) censists of a simulated reactor I (a pressure vessel centaining an electrical heated rod bundle, the .l "ccre"), primary loep piping, coolant pumps, steam generater U-tube. bundles and a pressurizer. l f l i [ J i t [ t b i 1 5 'h 4 13 .t

. __ ~_ ? Major components of PCS, made of materials listed in Tab.3.3/1,- are described below in detail. Emergency and auxiliary-systems for PCS are decribed in sects. 3.5 and 3.7. f I i 3.3.1 Power channel pressure vessel l l The pressure vessel (PV), heusing the electrically. heated core j and other internals, is shown, in Fig.3.3.1/1. It consists f: - a lower section, the lower plenum (Fig.3.3.1/2) + - a intermediate secticn, the active :ene (Fig.3.3.1/3) - an upper section, the upper plenum and the upper. head (Fig.3.3.1/4)-' i -The PV characteristics are given in Tab.3.3.1/1. i The lower plenum consists of a cylindrical chamber connected to the PV active zone through a tube which holds the nozzles for core coolant inlet and for core bypass. A nozzle is provided at the 4 bottom of the lower plenum to house a sealing device for the outside protruding rod bundle. [~ The PV active zone, having an inside octagonal cross secticn, is built by assembling eleven end flanged sections; electrical insulation and fluid sealing are guaranteed by "klingerity 400" gaskets. + /99I [ r I i ? I f 14 f

t I r Loose flanges, thermally insulated by klingerit rings and sleeves, are used to assembly the end flanded sections to reduce heat f losses from PV wall. -i The upper section is composed of two cylindrical parts flanged one to another (the upper plenum and the upper head); the two { sections are separated by means a drilled plate. Fig.3.3.1/5. The I upper plenum is flanged to FV active zone and holds, in between l i flanges, a proper rod bundle support plate, Fig.3.3.1/6.The upper plenum also holds the three hot leg no::les and the core bypass e upper nq::le. ~! The upper head holds twa no :les for downcome_r / power channel bypass. I The PV geometrical (volumes, cross sectien areas) and physical (masses) data are given in Tab.3.3.1/2. 3.3.2 Power channel rod bundle I The PV core consists of an electrically heated bundle of 97 rods reproducing, in the active zone, the same geometry (rod pitch, rod I i outside diameter and lenght) as the 17x17 PWR-PUN bundle. I The main features of spes core are summarized in Tab.3.3.2/1. The rods Fig.3.3.2/1, are screw fixed at their top to a support i i plate which also acts as a power lug and are kept fastened and i I evenly spaced by suitable grid spacers. Fig.3.3.2/2. The eleven I i spacers are located along the bundle: the top spacer on upper i unheated zone, seven spacers on active zone and three on lower unheated zone. The distances between the spacers are shown in Fig.3.3.2/3 i k i 15 i

~; f f 1 i The axial power profile is uniform for all the rods; radially within the rod array the profile is also uniform anyway local hot spots can be simulated by means of three rods (hot rods) with a c peaking factor of 1.19. f Twenty rods are instrumented, each with 4 thermocouples (K type, t Inconel 600 clad,1 mm CD) induction brazed to the inside rod wall at different axial location as sketched in Fig.3.3,2/3. 1 Tsod bundle volumes, cress flow areas and metal masses are reported -i in Tab.3.3.1/2. a l ? r 'i 1 i e i t i I i g P O 7 3 i i b f i -? r I i i 16 j

f ~ l 3.3.3 Pressurizer-t i The pressurizer, Fig.3.3.3/1, controls primary system pressure during normal and transient plan r,eration and consists of a f cylindrical end flanged vessel equipped with immersion type electrical heaters, spray system, relief and safety valves, no::les for f pressure, temperature and level instrumentation. The pressurizer is cennected to one PCS intact loop (hot leg-2) by means of 1" SCH BO surge line, see 3.3.4, phat will be equipped i ? with a turbine flewmeter: the pretsurizer surge line can also be connected to the PCS broken loop (het leg-3). ? A 1/2" SCE 80 spray line connects the PCS (cold leg-1) to pressurizer tcp (spray nc::le, Tig.3.3.3/2), providing primary coolant for pressure centrel. This line is equipped with an crifice i 2 g device and an air operated valve to measure and to control the- /{lIf spray water flourate. The pressurizer main data are given in Tab.3.3.3/1; surge line and l spray line characteristics are given in Tabs.3.3.5/12,14. e A power operated relief valve (PORV) and two safety valves are provided at the tcp of the pressurizer. i l The POEV and the first safety valve are preperly scaled and designed to reprcduce the operation behaviour of PWR-PUN valves: in t a f particular the cetual final design should assure the required e ] actuation times and the blowdown parameters as already t experimentally checked. The discharge line lay-out will be defined depending on test. I i l r f i b I 17 i r----4 ,-w,,,-_p-,

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-~ I l .) l 1 The second safety valve has a set pressure corresponding to 1 -the PCS design pressure and discharges to the atmosphere directly. Six electrical ~ heaters (3.8'KW each one) have been j installed on the external surface of the pressurizer for heat i losses compensation (see fig. 5/6). i 1 1 3.3.4 -- Primary recirculation pumps li Three recirculation pumps (one per loop) drive primary coolant j I into the power channel to remove the core generated heat. These pumps are centrifugal-single stage-vertical shaft type. The rotational speed can be changed in the continuos range +/- 190 % of nominal value (with fluid in two-phase ) i conditions) and the speed variations can be programmed by means of a motor driven regulator. The pumps are designed both for the f t initial transient conditions in normal operation-and as. tool for f operators to influence power channel cooling. i The inside volume is quite similar to the scaled PWB-PUN pump volume and the total inertia is scaled to obtain a' good simulation-( in coast-down transient. } The pump main characteristics are given in Tab. 3.3.4/1 ; I Fig.3.3.4/1 shows the pump cross section assembly. The theoretical pump characteristic head-flowrate, at different speeds, is reported in Fig.3.3.4/2 together with some experimental check points obtained during pump acceptance tests. 4 Rotational speed-flowrate theoretical curves are shown in Fig.3.3.4/3,- they will be experimentally checked later on. a l 18 l I I s 1 l t

The three pumps ar'e connected to common centrali:ed auxiliary ^ systems providing bearing lubrication and seal flushing. The pump seal is a triple mechanical seal comprising of a double seal and back-up tandem seal Fig.3.3.4/4 and Tab.3.3.4/2; it has the actual valuable benefit to guarantee :ero fluid injection into primary circuit. The inner seal (high pressure seal), installed on the pump shaft between the barrier fluid and the primary fluid, is designed to assure zero leakage under whichever normal and transient (i.e. LOCA) conditions.The intermediate seal is designed to leak towards,the cuter seal so to reduce wear and heat generation. The outer seal (low pressure seal) guarantees zero leakage from the sealing circuit to the environment. The sealing system was successfully tested: the seal was found to i perform very well under normal and emergency conditions. 3.3.5 Primary coolant loop piping SPES primary system. Fig.3.2/1, is composed of three equal loops connected in parallel, each one including the following lines: - hot leg, connects the PC outlet to the SG inlet; - loop seal, connects the SG outlet to the RP suction; - cold leg, connects the EP discharge to the downcomer inlet. j j The otner PCS lines (common to all the loops) are: ) - PC downcomer, connects the three cold legs to PC inlet; i - surge line, connects the pressurizer to hot leg 2, 3 ; l I i l 19 i 4 --1

- core bypass, simulates the PWR core flow bypass; - PC upper head bypass, simulates the PWR flow leakage from DC inlet to the upper head of the vessel. - pressurizer spray line for primary pressure control Tab.3.3.5/1 summarizes the characteristics of PCS piping. The PC downcomer design is shown in Fig.3.3.5/1. The lay-out of each other line is shown in appendix A. The single pipe. data (length, volume, cross area, metal surface-and weight) are reported in Tabs.3.3.5/214 with reference to Figs. 3.3.5/2+6 The entire piping system is made of stainless steel, Tab.3.3/1; other materials are censidered (carbon steel) for loose flanges bolts and nuts or items not directly in contact with primary coolant. The Icose flange details are shown in Fig.3.3.5/7. O 20 l I 1

h i I f I f 3.3.6 Steam generator tube bundle i .T t The steam generator (SG) primary side consists of a tube i, bundle and the inlet / outlet plena. The SG tundle includes 13 Inconel 600 U-tubes assembled in a square array, spaced by means of seven broached grids and welded to the tube sheet. The tute material, inner / outer diameter and active average lenght are the same of these cf ?hR-PUN SG as well as the spacer cross section geometry. Tube bundle data are reported in Tab.3.3.6/1.2. f / Two tubes are instrumented and precisely : .g - tube No.13, equipped with three pressure taps for the measurements of primary coolant pressure and pressure drcp along U-tube i i I ) - tute No.8 equipped with five 0.8 mm sheated thermocouples protruding inside the tube (primary fluic temperature measurement) { and with five 0.5 nm OD sheated thermocouples brazed onto outer tube wall (secondary side tube wall temperature measurement). i i The measurement arrangement is the same for each SG tube bundle. i the instrumentation details and elevations are shown in Fig.3.3.6/1. I The tube lenghts have been measured en the assembled bundles: the i as buiat values are given in Tab.3.3.6/3. l e f t l l i 'l a r

)

t I I e 21 i i ..m= e

3.4 Secondarv ecolant system Secondary coolant system (SCS) is designed to partially simulate the PWR-PUN secondary coolant system (see chapter 2) and consists of the following components: - steam generaters - steam condensing system - steam separator and demerater - booster and feed pumps - feedwater pre-heater - coolant piping system and valves - emergency feedwater system (EFWS). Steam generaters, scaled piping and EFWS are described in detail below, the other components are a part of an early SIET facility (IETI-4). 22 i

l l i I i 1 .i 3.4.1 Steam gererator i i The SPES plant has three identical generators (SG) that allow l the transfer of the thermal power from the prinary to the secondary circuit. Each' one of the SG consists of the following parts. t .,i - the pressure vessel - the tube bundle t i - the steam separator j - the dryers i - other internals t. The Fig.3.4.1/1 shows the SG general arrangement. f Tabs. 3.4.1/l,2 summarize the 50 characteristics. Volumes, cross flow areas and metal weights of the various parts are given in Tab.J.4.1/3. The SG vessel is composed of the following sections: i i i - the bottom plena (primary side) I - an intermediate section (tube bundle side) including the two { external downcomers } ~~. r - an upper section including the separator and the dryers

[

The details of these items are shown in Fig.3.4.1/2,3. t The primary plena, having a flat bottom with the inlet / outlet nozzles, are flanged to the intermediate shell. -l The intermediate section is a tall cylindrical vessel that houses the U-tube bundle, see sect.3.3.6, together with its supporting i cage. i 'i I f 23 ?

f + -t The bundle cage, Figs.3.4.1/4,5, includes seven spacer grids' .l ? and suitable filler slabs so to form a' unique item'which keeps t i centered' the bundle inside the vessel and reduces the secondary * .i! coolant flow area to the correspondent one of 13 tubes in FWR-FUN ' l i-5 SG (Westinghouse mod. F). A dividing plate. (2.2 m height) separates the hot / cold rene of e the SG riser and avoids the mixing of the water coming from the [ l two external downecmers. l l A butterfly valve is located downstream of.the tube bundle, j. inside the vessel, Fig.3.4.1/3, for a pcssible future j investigation of SG instabilities; in this zone the vessel cross I section area is reduced by means a cylindrycal. filler. f i The two external.downcomers connect the upper'downcomer to the l bottom of the riser they are simply realized by means' of 2 i tubes, Fig.3.4.1/1. An expansion joint (a telescopic sleeve provided with a stuffing sealing box) is assembled to these-tubes to allow their thermal expansion indipendently of the SG vessel i expansion. Two Venturi tubes are'provided to measure the. recirculation mass ficwrate. i The S_G upper section, Fig.3.4.1/3, consists of a cylindrical I 1 vessel, flanged to the intermediate vessel, with a large dome at the top. This section presents the normal feedwater no::le and the main steam line no::le. t i i t l f f I i i 't .i i 24

4 f i i The internals of the upper vessel are : the whole separator cyclon type (stand pipe, swirler, water discharge annulus, steam crifice), Fig.3.4.1/3 ; i the dryers, Fig.3.4.1/6 ( - the feed water therus with 10 J-nostles, Fig.3.4.1/3 y h t f f E t L I 4 B f t a e e i 25 1 i f n

.i l 3.4.2 Secondary Piping System i SPES secondary piping system includes the following lines : t 1 - the main steam lines (MSL 1-2-3) with a Venturi tube (steam flow - [ measurement), n.2 safety valves, the PORV and the main steam isolation valve ; - the main steam header (MSL-0) with the flow control valve and the isolation valve ; t - the preheater line (PHL) with the flow control valve, an orifice no::le (steam flow measurement) and the isolation valve ; i - the steam dump line (SDL) with the flow control-valve, an orifice no::le (steam flow measurement) and the isolation valve ; l - the normal feedwater lines (FWL l-2-3) with two control valves f f (for automatic and manual water flow regulation), an orifice i t nos:le (water flow measurement) and the isolation valve ; -f i - the normal feedwater hesder (FWL-0) with an orifice no le for water flow measurement ; - the preheater bypass (EP-03) with the flow control valve and the 4 i isolation valve ; f a - the emergency feedwater header (EFWL-0) with two step valves..the [i contro_1 valve and an orifice no::le (water flow measurement) -f - the emergency feedwater lines (EFWL-1-2-3) with the step valve, [ the check valve and an orifice no::le-(water flow measurement). Tab. 3.4.2/1 summarizes the characteristics of SCS piping. The lay-out of each line is shown in Appendix B. The single pipe j l data are reported in Tabs. 3.4.2/2. The whole piping system is made of carbon steel. s l k l 26

m s 7 i ~ i 3.5 Emergenev core cooline system 5 P I I SPES ECOS consists of : 1 - accu =ulator injection system (AIS) { t - high/ low pressure injection system (HPIS/LPIS) i i The AIS includes three accumulator tanks, Fig.3.5/1 nitrogen y pressurized up to a maximum of 6.9 MPa, connected to PCS cold legs l l by mean's 1" surge lines provided with check valves. [ T The surge line lay-out for each loop is shown in Appendix C. Tab.3.5/1 gives the accumulator and surge line' general data. An electrical immersien type heater (3KW max power) located at the bottom of accumulaters keeps the emergency fluid temperature at abcut 50'C.Each accumulator is provided with a safety valve (6.86 MPa set pressure). } HPIS/LPIS are physically the same system and are connected to the { .6 accumulator surge line (a check valve avoids the reflux flow). I 1 A volumetric injection pump (max pressure 20 MPa) allows to l reproduce the flow-head characteristic of HP and LP injection system ? pump of PWR-PUN by means of a suitable regulation system ( The HPIS/LPIS lay-out is shown in Appendix C. l Tab. 3.5/2 gives the injection pump and HPIS/LPIS characteristics. l q !'I i i i i i 27 l .i r

t i 'l i I 3.6 PCS charcine and letdown lines- ^ i An high pressure auxiliary system controls the primary coolant 'l volume in the SPES facility and partially simulates the PWR-PUN 'i Chemical and Volume Control System (CVCS). ) It consists of two lines : i l - the charging line,1/2" SCH S0, etsinless steel, that'provides 'f hot water ( 543 'K) to cold leg-2; f t - the letdown line.1/2" ECH 80, stainless steel, that connects f the loop seal-2 to the SPES separator. t I Ibe lines include process and instrumentation equipments: -i - a volumetric pu=p (the charging pump) l l - a counter-current surface heat exchanger L; L - hand and control valves I - orifice for mass flowrate measurements 1 1 The detailed lay-out of the charging and letdown lines is / I t reported in appendix C (Fig. C5) ~ I I f-j j - i ![ 'k t j a s ? 1 i 28 l,

s i k i 1 i 3.7 SPES surplement-systems I SPES facility needs fer its operation a lot of supplement systems (electrical power, instrument air, valve air, cooling water.etc) i which form the auxiliary system bay common to all SIET facilities. j The power supply system supplies electricity to: I power channel - heaters of pressurizer, accumulaters, liquid metal heating system i - pumps and valves - centrol room apparatus, i h i i I b r t .l )-: i Li i .l ) l t l I 4 i h' 1 e i 29 i i

~ i m i i t 2 3.8 Valves t! The specifications of the SPES valves are reported in the i following tables: - Tab. 3.8/1: air operated centrol valves - Tab. 3.8/2: air operated isolation and relief valves (ball valves) - Tab. 3.8/3: safety valves t - Tab. 3.8/4: hand operated control and isolation valves t - Tab. 3.8/5: non return valves The valve identificatien tag is referred to Fig.6.2/1 ' t >i I f e [ 1 i i 4 i J t P ? h i i a ? . i a d 1 1 0 30 e.., ...w.-- ..n...

3.9 Comeenent and picing thermal insulation SPES main components and piping are thermal insulated by means rock wool. The insulator thickness is indicated, for each part of the plant, in Tab. 3.9/1; components and piping not indicated don't have thermal insulation. Thermal conductivity of the insulator material is about 0.05 W/m'K. l i I 31 l

i t t

4. SLOWDOWN SYSTEM

[ l The SPES blowdown system consists of a break unit, blowdown h t piping and a break flow s:crage tank (catch tank) for fluid mass [ measurements. The break locations foreseen for SPES transients are the following: i - cold leg j - het leg i - loop seal i - bottom vessel - tcp pressurizer - feed line - steam line i The break unit includes a break area simulation orifice, a break i simulatien valve (air operated ball valve) andaspoolpiece(ff- ) densitometer, turbine flowmeter) for two phase flowrate measurements. The catch tank device includes a steam condenser and a tank to t collect the outlet fluid. i. The blowdown system is now under design, details of the system shall be presented later on. l. e 'l 1 i i ? 1 h i h 4 + 1 32 I l

T i l 5. INSTRUMENTATION i i 4 This section describes the instrumentation to measure the plant process quantities and all the thermodinamic parameters of interest for the understanding of transients phenomena and plant global response. Above quantities concern both direct quantities (absolute and differential pressure, temperature, voltage, etc.) and derived j quantities ( void fraction, mass velocity, quality, etc). [ Differents methods are foreseen to measure the above parameters: .l . Pressure - pressure transmitters .i . Differential pressure - differential pressure transmitters . Temperature - thermocouples (TC) ? i . Liquid level - differential pressure / heated thermocouples [ . Density - (( densitometers /pressuretransmittersandTC , Velocit'y - turbines / drag disks / differential pressure across crifices, venturi tubes . Void fraction - densitometers / void fraction probes . Fluid mass - catch tanks .i . Flow pattern - differential pressure transducer / heated thermocouples The overview of the whole instrumentation and its relevant location on eacn loop of the SPES is presented in Figs. 5/1,2,3 I and Tab. 5/1. i 1 I i 33 i l

i i i ? t The flow sheet explanation (measurement tag, graphics etc.) can ) be find in Tab. 5/2. i i Tab. 5/3 report the measurement list with : [ t - the identification tag i - the instrument - the accuracy i - the response time I i - the range - the location i Fig. 5/4 shows a detail for temperature instrumentation of the t power channel rod' bundle. 'I Details of instrument location are given in the following items: l 0 f - Fig. 5/5 for power channel vessel ; .I - Fig. 5/6 for pressuriser ; - Fig. 5/7 for steam generator'; f I - Tab. 5/4 referred to appendix figures for SPES piping t

l 5.1 Thermocouples and thermoresistances j

n The temperatures of the fluid, structures and piping, and core j heater rods are measured by using: I } \\ - ungrounded sheated thermocouples, type K Cromel-Alumel. 0.5-2.mm l l OD, for temperature measuring range 273 f 1533 'K ; -l i h f f 3 i l l'l 34 ~--

l l l l t i - idem, type T copper-constantan 2 mm OD, up to 643 'K ; i - RTD thermoresistance type PT 100 (DIN 43760) 100, range 273:-923 'K - j i ' I i 5.2 Flowmeters The flowrate of single phase fluid (water, steam) is measured by j using different primary elements : calibrated orifices, venturi -f t tubes ans full flow turbine. Venturi tube and orifice nozzle specifications are given in Tabs.5.2/1.2 respectively. l Two-phase flow is measured by means of spool-pieces which are l cogposed of a full flow turbine, a drag disk and densitometer. ' s i 5.3 Fluid level sensors Liquid level in single phase or cellapsed liquid level in two- { phase are measured by differential pressure transmitters. i' Heated thermocouple probes are also foreseen to measure the travelling mixture evel in two phase flow. 5.4 Absolute and differential pressure transmitters j i Absolute and differential pressures are measured by means of [ i piezoresistance type transmitters combined with a microprocessor. f I ? I l l t ~ 35 j i i -e, +- - - _ _,, -

l i J l i 1 i and digital-analog convererter. These transmitters which allow automatic compensation cf the output signal for temperature and l static pressure changes, are charactericed by high accuracy and j wide span adjustement. j 5.5 Power meters l Electric power to rod bundle is measured by a digital voltmeter l detecting everall voltage drep across a set of 5 shunts in parallel. For immersion type heaters power is measured by wattmeters. f densitometers 5.6 I t Three beams and one beam type f\\densitometersareusedto measure single and two-phase fluid density, inside hot leg and i break line respectively. f All{densitometerswhichuseCS137sourcesandsodium-iodine j scintillation detectors, measure the attenuation of fSradiation through the pipe wall and fluid giving the fluid average density {f\\ within the -ray beam. densitometers are foreseen to be used both as a single l 4 instrument and coupled with turbine and/or drag. disk to form the. ] 1 spool piece for two-phase flowrate measurement. 4 i i i i I i I l J 36 . i, f

i

k l

l-;

6. CONTROL AND DATA ACCUISITION SYSTEM i

r I The schematics in Fig.6/1 show the arrangement of SPES control i and data acquisition system.It consists of four main components: - the Programmable Logical Contro'11er (PLC). - the process controller system i i - the supervisory computer - the data acquisition sub-system j -i i i 6.1 Programmable logical controller. PLC I t b The PLC includes : j 4 i - CPV with 32 Kb of progrcmmable RAM - n.1 color graphic display - n.2 I/O units (n.1 remote) for n.200 logical I/O signals l .i the functions of PLC are the following : 1 s - monitoring alarms and security signals from field instruments (by I I means_of graphics display)- - controlling the right sequence of actions performed by plant operators - safeguarding the integrity of every component of SPES -{ pumps. SG.PC,etc.) - programming transients during tests -i -l i i i: 37 I

-t e .i L 6.2 Process control system The process control system includes n.15 programmable multi-loop 8 controllers for the total number of n.42 regulation loops. Set [ ~ t points and loop parameters may be set by the supervisory computer at any time during experimental tests. .I The main control loops concern the following parameters, Fig. 6.2/1 : r 1 - primary circuit pressure (pressurizer) - pressurizer level t - primary recirculation pump head l - steam generator level p - secondary circuit pressure f - feedwater temperature '{ - feedwater flowrate I - HPIS/LPIS pump flowrate -[ [ { - EFWS flewrate I i 6.3 Supervisory computer r The supervisory computer is a DEC VAX 11/730 with the foll' wing f o features. i E I t i I CPU, 2Mb of RAM memory l 'I 6 i ti 38 i I

i t 1 MASS STCRAGE. n.121 Mb hard disk . n.10 Mb removible disk I i FERI.:MERALS . n.2 colcr gra:nic vicee terminals . n.2 printers . n.1 digital plotter I -....AML,L,,.. - m.J. n. w s e.4 a.i..,..+- n nu . interface aca ter for D. A. networn r Computer has t.wo relevant func:: ns: - sucervising the process cent-01 system either.n nominal er p transient concitions - collecting anc stcring measurements fr:m the D. A. suesystem t 3eni rice monit: ring programs cisplay precess variables on video terminals sne plot trencs on ;rinters er digital pictter. t Off-line cata processing pr:vides reperts, picts, diagrams and I. stat ::::s :: the tes: analisys. l 6.4 sta a: uisitten suesvstem t ~he 2.A..sutsystem e:nsis s f n.12 smar: secu siti:n un :s e r .inxec ::gerner ty a hign spee: local networn an: it previces n gnal : nca:::ning anc analeg-to-21:i;;tal nversien. '{ F l 9 i l l ..s h t t S 1 e d

~ t A l i 'I Measurements acquired are trasmitted to the host computer via the k optical fiber link. i i The main features of the system are the following: t - n.512 input channels (available at present) =. - max data logging rate (all channels), 5000 reading /s [ samoling rate programmable en single channel and modificable .l b during acquisition l - A/D converter resolution 12 bits i -- max A/D conv_ertion frequency 10 Hz f k l i i ? 'I i [ .i i ? i l l l ~ I t I l I

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40 ~! 1 'I f; .l .i

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.~ ...... ~, ,. ~... .i .I 1a COMPONENT MATERIAL COLE POWER CHANNEL ~ active section vessel SA 312-TP 316 ASTM .f loose flanges SA 182-F12 ASTM i ~ bypass tubes SA 312-TP 304 ASTM l l downcomer SA 312-TP 321' ASTM I 'I A upper plenum SA 312-TP 316 ASTM j lower plenum SA 312-TP 316 ASTM .i .i red active section SB 163-Inconel 600 ASTM rod cold section Cu ~[ \\ .l 9 PRESSURIZER r pressure vessel X 2 CrNiMo-N 1713 UNI 7500 surge line SA 312-TP 321 ASTM i 4 ? vessel end sheets A105 + AISI 304 plating ASTM i [ ( 1cese flanges A 105 ASTM , PRIMARY COOLANT PUMP I / pump body (bearing side) A IS2-F 6 NM UNI' pump body (seal side) A 743-CA 6 NM UNI j impeller A 743-CA 6 NM UNI j shaft A 276-410 UNI I g l STEAM GENERATOR 1 s inlet / outlet plena SA 182-F 304 ASTM [ t s f tube bundle SB 163-Inconel 600 ASTM a PIPING i I generally SA 312-TP 304 ASTM cold legs SA 312-TP 321 ASTM venturi (pump suction) SA 312-TP 316 ASTM Ioose flanges A 105 ASTM f TABLE 3.3/1 Materials of PCS major componenets I 'g I h 3 r

~-.- -~ .: j t -- pressure, MPa i nominal 15.5 ll 1 design 20.0 - temperature. 'K inlet 563.8 l outlet 599.4 t design 638.0 - flowrate, Eg/s l downcomer outlet .31.14 core bypass 1.36 .l downcomer cypass 0.57 { - overall height,m 10.85 i - net inner volume (without nozzles) m3 0.1937 r - nozzles ID,mm l . hot leg 66.7 , downcomer 92.0 1 core bypass' 42.8 . downcomer bypass 24.3 - elevation, m- . bottom vessel (inside surface) -7.145 1 downcomer nozzle -6.351 core bypass lower nozzle -5.598 i BAF -5.112 j l TAF -1.452 . core bypass upper nozzle -0.688' l . downcomer inlet ' -0.100 . hot leg nozzle 0.000 = . downcomer bypass nozzle 1.872 'I . vessel top (inside surface) 3.156 [ - vessel material AISI 316 i I TABLE 3.3.1/1 - Power channel pressure vessel data 1 45 'I i I

POWEll CllAfiTIEL CilARACTEltiSTICS _ _ _ - - = _ _ - riescription elevation cross section bundle cross section nren volume ' weight mm mm2 dm3 kg i lower plenum -7302/-G685 circular yes 98333 42.40 737-(vessel) -6605/-5198 circular yes 11270 18.70 27 (bol ting) 9197 (spacer) i n te rmerli a t e -5198/_1088 octagonal yes 9644 39.70 541 (vessel) t section 7571 (spacer) 794 (loose flanges 329 (bolting) upper seetion -1088/+1372 circular no 19607 48.60 791 (vessel) +1372/+3156 circular no 27465 48.80 rod bundle weight (including power plate and grids)

239 Kg 57 - ( bol ti ng)

ToTAt. / / / / 198.2 3276 _= . = _ _ _. . _. _ = =. including nozzle volumes TABLE 3.3.1/2. Power channel volumes, cross areas and weights. i l CD ___ U

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u o s /o w e* o me/ a o o - i r gl m l l s r d l r - t r mp n s o a d a e pF x rK a 1 uA a u id e e - / e d r nd oe w 2 r r d r rd m rh o n sD s mc ,d o h h. p a o d e a om / l o r / e a r - t t 3 d r r et d r m*/ir/ e mt r l n n a c x n ,u*

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a u a/d o o g a t d ie ce t h ml r a pF a n mrl e t t 3 i t o nt t o ci a e v pA p i i w at s s h at d sh t nt p e uT s m x oi a = p p E e t a o i i o pl o al x e = u u - L n mf ah - B .p mt u e s1 r d A T l j l l l( l llltlli:lL

i-fluid saturated water /steem - water vol./overall vol.(nom. level) 0.61 - pressure, MPa / temperature, 'K . nominal 15.5/618 . design 20.0/638 - PORV set pressure, MPa 16.2 - SV-1 set pressure, MPa '17.2 - SV-2 set pressure, MPa 20.0 - PORV discharge flowrate (15.2 MPa,x = 1), Kg/s 0.196 * - SV-1 discharge flowrate (17.2 MPa,x = 1), Kg/s 0.376 ** - spray water max flowrate, Kg/s 0.08 - heater number, proportional /back-up 1/2 - heater max power (each), KW 13 - overall volume, dm3 95.4 - vessel inner diameter / wall thickness,mm 134.5/12.8 - l - height, m 6.796 - end connection ID, mm . surge line 24.3 . PORV 15.7 . SV-1 21.0 . SV-2 42.8 . spray system-13.8 I - elevation from PC HL nozzle, mm .j . vessel top 16525 . nominal water level -13885 . vessel bottom 9729 TABLE 3.3.3/1 - Pressurizer main data experimental data with ID crifice = 3.2 mm (three PORV simulation) experimental data ID orifice = 4.5 mm 48 l l .J

(s e B 'l ~ l .' t - design pressure, MPa 20 ? design temperature, 'K 638 < t i nominal conditions i t , suction pressure MPa 15.3. .t . temperature, 'K 564 f . capacity,'Kg/s 10.6 l . head, m 77 . t I* rotational speed, rad /s 335 e . rated torque, Nm 59.7 . power, KW 2.0 . efficiency, f. 40 . i . NPSHr, m 2.6 l{ - speed regulation range, rad /s -628,+628 q l - maximum power, KW 50 - suction diameter, mm 66.7 i - discharge diameter, mm 66.7 - inside fluid volume, dm3 4.3 - global inertia, Kgm2 3.5 l [ + TABLE 3.3.4/1 - Primary recirculation pump characteristics ll t s'$ , k ? i I T i l ) l t .f t 49 t

lI l!1l l 1' @O 6 ) p m u p e l g n i s a r o. e _ y t t _ r a _ a d w _ m e i r d ) _ r r e8 _ p e f z _ g e 4 i 3 1 8 3 3

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5 0 0 alip i ( 4 4 5 . u r _ r o1 e( 0 0 00 5 m 1 1 1 1 n i d e t m n s ie e y v s t e g t' n n i a a a l t P P - a s M M - e n s o 7 2 c p n n m y a a u h h p l l t t = e n e s s h i s s _ t t e e a l l f m o o l l t a a a _ u e e t _ a s s a d _ t e e m_ a a p h h l P P et t t a M M k n n e s s i i. si s s m el s i s o o _ o r a / n r r _ N u e g s e a c e _ s s K / -_ u r a n t 1 a s e e m e =l 1 / e e t t t = a P P 2 0 g rh a e a a a v eD D / g i P i r 4 1 K pt i 2_. ( d a d M d -_ a u a a 1 n s e k e e s m_ g e o s m a m m h sh h n t i o r r r e r r r v r r r c et t 3 at r e e el e e e p e e e u rii i h r c c nt t nt t nt t s p w w e s w e a n n ul n n ul n n u i u oj iI oaii oaii o D nP e e A l l f T D ... s... s f i m_ a a s_ lllllIr

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?' E ? h I.- J E I 0, m 4 4 4 1 1 1 1 1 1 1 1 4 4 4 - 0 0 0 2 2 2 2 2 2 2 2 00 0 - 3 3 3 3 3 3 3 3 3 3 3 33 3. la P P P P P P P P P P P PP P i T T T TT T T T T T T T T T e r p e 2 2 2 2 2 2 2 2 2 2 2 2 2 2 i t 1 1 1 1 1 1 1 1 1 1 1 1 1 1 p a - 3 3 3 3 3 3 3 3 3 3 3 33 3 - A m - A.S A A A A A A - A A A A A A A S S S SS S S S S S S S S U C C C .D D P D 1 2 3 i t 2 - - C - P L L D L 3 P T T C ) 2 - t E E i n - - G ,3 , 3 3 , o - G S 1 L i - S - L - L L L - l H c - - I S C T L l P ,P D. P t - 1 W P E C( e e - G .,) t l I i n n - S t L C C ,PP S S n - ( 1 2 3 1 2 3 1 2 1 ~ i o - l P P L c - CC C G G G t I i P P P S S S I P L I CC l I t C I PD C e) - m3 4 4 4 9 9 9 8 4 8 6 4 93 0 - u m d 3 3 3 6 6 6 0 6 6 5 5 4 1 1 lo( 1 1 1 1 1 1 4 1 l v i h t ) 3 3 6 5 7 5 5 0 1 7 4 36 0 J w g m - 3 3 3 3 3 3 8 3 8 8 2 6 8 2 n m - 8 8 8 7 7 7 4 3 4 8 7 3 7 2 - 82 5 - e( _ 3 3 3 8 8 8 2 2 2 6 1 l 1 2 - d 4- ) m n r e( d r i e g 9 9 9 3 3 3 00 03 4 3 4 3 - n st - t e 8 8 8 0 0 0 3 3 3 4 3 03 i = u m p 1 o a - 8 8 8 6 6 6 7 7 7 1 3 63 2 i 1 p i d - y r a ) m .i, m - i m ~ r ( ~ p le r - - e 6 6 6 2 2 2 00 003 8 3 8 c e - - h i t in e - 6 6 6 9 9 9 9 9 9 2 4 2 4 3 - t m - 6 0 6 4 4 4 5 5 5 9 2 4 2 1 r t a - - f i - - o d - - s - e - r - u 2 3 1 2 3 01 - t 1 2 3 1 g - - - - - - - -. -. CL P P S - e - - L - a L L S 3 L l C D S 1 B W - f o - 1L I I 1S. L l ) t 1 I I C C ^ 1 - n ~ i - a = s - M s a p = ) ) ) y 1 1 2 3 ) ) ) L / ) ) ) ( ( ( 1 2 3 s 5 1 2 3 ( ( g e sd e r n a a n 3 ( ( ( l l l a a a g g g ei p ei - e - g g g e e e e e e ml yhl. 3 o b - n - e e e s n nl l l l l l c e r y - E i l p p pd d d n g e c a - L w r r p r - H .- t t t o o ol l l o o o o o oooo ou o p p - A l l c c cd s c u s - T h h hl

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( e w e e) w w g 8 01 81 3 3 9 2 9 5 9 8 K 2 9 0 3 9 4 7 1 37 8 1 9 - l ( a 3 1 3 1 3 e t 1 v e + m y 3 ) 5 c 0 g e) c2 4 * =- w a m ( f d w 1 4 6 4 1 1 S r( 4 6 2 1 7 7 8 5 9 3 0 9 6 5 5 2 5 9 5 8 u g s a - e - 1 7 9 5 4 5 9 2 4 5 5 2 4 D r 3 2 2 1 4 e O a 1 r w e ) 3 w 0 e) - 3 c2 - ( a m - 3 e 6 5 6 2 4 8 8 7 1 8 _ r _ f d _ 3 4 7 7 2 8 6 8 r( 1 1 e 0 - - u w e _ 2 1 3 5 9 3 8 7 7 1 8 - s n _ 1 1 D r - I a - ) ) I 1 G 5 S g ( ) r 3 - m 0 o l w _ G ad ( t ,= = n( - E r 3 0 3 1 1 9 1 3 3 1 4 g ) 2 9 6 2 1 3 5 9 3 n 2 e e 1 w 3 i / l t m 0 00 0 g 5 r n u 0 4 03 w 1 1 1 n i l o 3 o _ T v _ l e 3 - O b g e I d i v I ) 2 e F w m r m e o d t ( s - 4 4 4 4 4 4 4 4 4 4 i s n _ 8 8 8 8 8 8 8 8 8 8 s d o o - 4 4 4 4 4 4 4 4 4 4 - n e ri - 3 3 3 3 3 3 3 3 3 3 - o r ct - c r c - e e - s f s - i e r m ) ( m ) 5 m s e) _ 4 6 c m - n m _ 1 6 i w S m - ( 1 t i l ( 8 6 = s w - r 0 04 6 3 2 8 3 1 i - eh - 5 4 89 4 4 05 6 0 8 r t t - 6 1 1 8 3 3 9 1 2 9 3 s 0 e - n g - t 6 t w e 1 c - e n -_ w - c e k a l c h r a c a + r s h b c = ) = 7 ) ) - / 7 n 3 5 / i ( 1 e r 5 n oe n ( w 3 e g w h 3 - w i l R . o t z e 3 R. s H 3 a L 3 L . h i z l 1 e e w e e s s o g p0 p p5 p 5 on .t 9 i

  • k i 4 i g4

. s p. o i i w - n F p p* s p p i . i e m l f = g e u ( i F - o m 0 0 0 sd 0 00 s( 0 . e n c n i - t - e 6 6 6 e 6 6 6 e 6 . u ae e e w 1 1 1 g g1 1 1 gk 1 l l il 2 - p - g - n n a n s . a f p p / w i 5 - r - a h h h n rhhh aih . - v el t - c l c c cid e c cl d c l - t e s oe 3 f s s sf s s sf s A - s l p o ol d d T - e s o p n 3 -w n" n" _ O - d 3" "3 3" "3 "3 i i 3 3 a3 3 a3 _ T - u pl si - b E m

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- = 11 O T LEG (2) _ _ _ _ _ _ = description centerline cross internal ID uurface OD nurface metal weight length (mm) section (mm2) volume (dm3) area (dm2) area (dm2) (Kg) =- _ - - - - - _.1 -- 3" flange (Fig. 3.3.5/7) 65 3484 0.23 1.36 1.54 2.8 7.96 .9.0 3" sch 160 pipe 1408 3484 4.90 29.45 39.32 30.1 3" sch 160 90 LR 180 3484 0.63 '3.76 5.01 3.8 I 3" seh 160 pipe *** 833 3484 2.90 17.45 23.27 17.17 3" AflSI 2500 flanges 407 3484 1.42 8.51 47.01 - 84.6 and drag disk washer 3" ANSI 2500 flanges 343 3484 1.19 7.18' 43.97 77.2 3" sch 160 45 LH 90 3484 0.31 1.88 2.51 1.9 3" sch 160 pipe 152 (115) 3484 0.53 (0.40) 3.17 (2.41) 4.24 (3.21) 3.2 (2.5) 3" fIanges 268 3484 0.93 5.61 5.56 7.9 and disk (Fig. 3.3.5/7) 15.94 ** 18.5 -** 3" sch 160 45 LR 90 3484 0.31 1.88 2.51 1.9 TOTAL 3836 13.4 80.3 198.8 258.1 buil t value is shown in brackels-pipe loose fl anges

  • spool piece position l

e inlet plenum nozzle (3" sch 1601=166mm) is considered belonging to SG Bt.E 3.3.5/3 _ llot leg (2) characteristics (referred to Fig. 3.3.5/3) W i x .--.-wre.-.-~w.--s . ~.. v..r -. - -,m w-r ,+ eve,,- .n,w.-. ---w-s e +w .w,, .meve ~.-ev, 4,-v-e. ~w .w- , r t mw -w ww.v.,,-. .v w.v. -,.,,,wr~<v-s,,.,4.r...,,ew.-w.-w#,

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0 1 - T N O d M 0. { l O L t v G M i - 1 . - C I I I i i i j I a i M i l I w I 4 O 1 i a a 1 - 1 O O 14 9 l 4 - I M i v_ C. I O I I t E i = "O 1 O j 1 a: 1 a 1 e cw w w 32 C D CD T c N L 0 .* T N - W C O M CS M vb tc. C- "O CJ E M. b. M. . C. e. O. N. O. N. 5 N. a y , c gg O O OO O ON O-OT C 3 - C M C - 1 -* O I O 4 M 1 - l 1 : 'i I 0 I i I O p i .O I t 4 i C2 -{ ^ i 0 l O I i N I o 1 la. l .J t E i L i 1 I E l e C r 4 'O 4 [ i I w I .= t A 1 i O O

D i

I In C I O N n to L .- -== -.* t') = 0 4 m C a +1 .=e .=.= l C = 1

D N O O ON O O O O ON O

L Ch U L

==.Ch O.CD CD .O O CD I L & t M ** O 0

  • - - O i

o G 8 M CD i l 0 v Ch .CD e .to . O t g .e t 2 f*J i 4 L t a

w 1

i E a 1 ~ c E 2 4 4 I t 1 J ^ f a T C U 1 r o E I C Cn C -~ N =* l C E t it

f) i I

v. - t N I w 4 f L 4 i to M 4 L 1 QJ d 6 'O S C O 5 O 4 O "B O M O C t - C2 O C C C O 5 < N b N 4 M S. to c 4 4 - N -

D I U

I I C C CB N - C N N i I O G Q C .:r. E 6 l 1 i O 1 4 U U 2 Q G E 4 1 L U I I 1 I .O 4 i C M ^ l I O^ C w M i i 1 - 5 w 4 I M N O C i i O C I 3 N I d! 1 1 O I I

  • U M

i O N 1 O l 4 W

  • I O

O l 2 i l i 1 3: 6 M i G C l t i 8 a = = = a to E O ~ C 3 0 C ca 4 .4 V 4 I I i .C i 4 C i 4 - t2 G a-L O aw i 3 0 O -a O C t t O i 4 - - N -O 1 I - 8 3 la. O. 4

c. N O O ' C Ch C 3 0

t2 e i if 8 w 0 N : C - I 4 s i O 10 aI t I a i C O OO O C O O O OO c C ~ 4' C3

=

1 h -I 1 .= t@.2C C) CD CD

C CC :O ID CO LD C I

t.= C -.* b d 8N t t 1. I C 2 t 4 0 t .ll* C " 44 4 L 4 Z.O.C 4 C M I C 1 O 4 i rn I u==. O O u o 9 u u V U - O 8 .J 4 0 - 4 t I O I to 6

0 go (D W CD f4 C tt #J 6 0 1
  • C
    • O to M i M l

e 8

  • O f
  • D C

"5 4 (-= C. O O 4 ) i I 4

: C : : : o: : : : : : 0 I O O-0 O IM i

n 4 i M M C N N N > N N N N N M L i t= .3 a-4 I i 1 1 l CJ l M l 1 1 I to a .C 4-t O.-* N I' 4 e

  • f=

8 O i t 1 ! *C N M 4 O C6 CD C i i C i I 8 1 1 8 lb .= 4

- - - = = - = C0LD LEG (1) n. <lescription centerline cross internal ID surface OD surface metal weight length (mm) section (mm2) volume (dm3) area (dm2) area (dm2) (lig) 1 3" I'lange with reduction 138 3484/2734 0.39 2.59 2.88

  • 3.2
  • and disk (Fig.3.3.5/7) 8.19 **

10.2 ** 2 2 1/2" sch 80 pipe 210 2734 0.57 3.09 4.82 1 2.4 3 2 1/2" och 80 30 (H=190) 100 2734 0.27 1.H4 2.28 1.1 4 2 1/2" sch 80 pipe 195 2734 0.53 3.62 4.48 2.2 5 2 1/2" sch 80 30 (H=190) 100 2734 0.27 1.84 2.28 -1.1 6 2.1/2" sch 80 pipe 1023 ('l030) 2734 2.80 (2.82) 18.96 (19.09).- 23.47 (23.62) 11.7 7 2 1/2" sch 80 90 (H=190) 298 2734 0.82' '5.53 6.H5 3.4 8 ~ 2 1/2" sch 80 pipe 308 (330) 2734 0.84 (0.90) 5.71 (0.11) 7.07 (7.57) 3.5 (3.8) 9 -downcomer nozzle 113 2734 0.31 2.09 2.87 2.5 4 =_- - - = TOTA 1. 2485 6.80 46.07 65.19 41.4 I .== _----= - ------ - --=- - - - As built valtie is shown in brackets pipe loose flange __= TABLE 3.3.5/8 - cold leg (1) characteristics (referred to Fig.3.3.5/2) 4 + E (.D . CD i 1 ? ...-,;...__.-_,--..-..-_.-,.-,...-.L..-.--..._.._--..,_,._-.. . _... _. -, -. _,... -., _, _.. - -. _. _. - - F

C O l. D LEG (2) .-...--__---___-_-_----___-__~____ = - - __=_ ----- n. desc r i p ti on centerline cross internal ID surface OD surface metal weight: length (mm) nect. ion (mm2) volume (dm3) area ( tim? ) area (dm2) (Kg) t 1 3" flange with reduction 138 3484/2734 0.39 2.59 2.88

  • 3.2
  • and disk (Fig.3.3.5/7) 8.19 **

10.2 ** 2 2 1/2" sch 80 pipe 92 2734 0.25 1.71 2.11 1.1 3 2 1/2" seh 80 90 (H=190) 298 2734 0.82 5.53 6.85 3.4 4 2 1/2" sch 80 pipe 37 2734 0.10 0.70 0.85 0.4 5 2 1/2" sch 80 90 (H=190) 298 2734 0.82 5.53 6.85 3.4 6 2 1/2" sch 80 pipe 209 (185) 2734 0.57 (0.51) 3.88 (3.43) 4.80 (4.24) 2.4 (2.1)' 7 2 1/2" sch 80 45 (H 190) 1 19 2734 0.41 P.77

1.42 1.7 8

2 1/2" seh 80 pipe 996 2734 2.72 18.47 22.86 11.4 { 9 downcomer nozzle 113 2734 0.31 2.09 2.87 2.5 . = = - - TOTAL 2330 6.39 43.27 61.68 39.7 .- = - = ---- As built value is shown in brackets pipe loose flange TABl.E 3.3.5/9 - cold le g (2) characteristics (referred to Fig.3.3.5/3) l l l l G (D ~...


=

C0LD LEG (3) n. description centerline cross internal ID curface OD surface metal weight length (mm) section (mm2) volume (dm3) area (dm2) area (dm2) (Kg) 1 3" flange with reduction 138 3404/2734 0.39 2.59 2.88

  • 3.2
  • and disk (Fig.3.3.5/7) 8.19 **
  • 10.2 **

2 2 1/2" nch 80 pipe 122 (110) 2734 0.33 (0.30) 2.26 (2.04) 2.80 (2.52) 1.4 (1.3) 3 2 1/2" sch 80 90 (14=190) 298 2734 0.82 5.53 6.8S 3.4 4 2 1/2" sch 80 pipe 600 2734 1.64 11.12 13.76 6.8 5 2 1/2" set. 80 90 (11=190) 298 2734 0.82 5.53 6.85 3.4 1 6 2 1/2" sch 80 pipe 912 (955) 2734 2.49 (2.61) 16.90 (17.70) 20.92.(21.91) 10.5 (10.9) 7 downcomer nozzle 113 2734 0.31 2.09 2.87 2.5 L TOTAL 2481 6.80 46.02 65.12 41.4 i As built value is shown in brackets l-pipe loose flange - = = _ - TA13LE 3.3.5/10 - cold leg (3) characteristics (referred to Fig.3.3.5/4) i o O J er v e w-i-rw.m,-,,wie,-.w-mw,,rw,wr-. .-w.. w.,.v.. .,w,,w,,ww,,- w.,.+mm,r-. -w y .a.w,,- -,-,-rv anwe,-.e-w+w r-wr.w ew-*re-,--ewe--rw ws oww---- =- r w w w -+w-t ow,+ - -w ww-~e,,-,-----es-i +*w--e.i -e ~,erv e,e.. w-rw-v- ,,,---wiv--*-w,-v-=w---- e, w

m


.-------------------------~~----------------

D 0 WflC O Mis 11 n. description centerline crons internal ID surface OD surface metal weight length (mm) nection (mm2) volume (dm3) area (dm2) area (dm2) (Kg) =------------q-- 1 1" AriS1 1500 flange 76 464 0.04 0.58 5.05 3.7 2 1"/2" ach 80 reduction 105 464/1901 0.12 1.25 1.36 0.6 3 top flange (Fig.3.3.5/1) 43 3x79 0.01 0.41 15.69 27.4 4 upper head 228 3x3901 2.65 8.08 26.33 40.8 5 4" seh 120 flange 525 6648 3.49 15.17 17.06

  • 21.2
  • 29.64 **

46.6 ** 6 4" sch 120 pipe *** 5479 6648 -36.42 158.36 196.74 155.4 7 4" sch 120 90 1.11 2 19 664H 1.69 6.90 8.57 6.8 8 4" sch 120 pipe 117 6648 0.78 3.30 1.20 3.3 9 4" PV flange (Fig.3.3.5/7) 75 6648 0.50 2.17 2.91

  • 5.8
  • 18.5 **

14.3 ** = =---- TOTAL 6887 45.6 197.09 326.05 325.9 pipe loose flange

  • *
  • a turbire flow meter is foreseen

-TABLE 3.3.5/11 - Downcomer characteristics (referred to Fig. 3.3.5/5) a i m e-e w -,--=w,- w w w,,,- o-ww, w i- - iv w -- --w o- --,wy

  • ,,-r,wt-w,vew,w,-

w+,+-e->w+, ew e-www---,,+=e=--r**ve--t,4,vev--vi -e a r*

  • r - v e+-rv=,,*-e_i

-gr-"e-e++ +-+--tw,e+- <-wa-r-'e,,- eace e ,-+vm-+ < =www w.-- w wwi w ,,e=,v<,wre w

e ~ k D W y e e w e e w N T t h g w i t + w e) 5 7 3

5. 4 7 2 83 7 6 _ 8 1

w g v K 1 7 7 7 004 02 02 7 _ 2 - a l ( 1 1 _ 6 w w a t e g m N -w e e e) c2 a m e f d 5 7 4 1 4 G 04 1 6 3 0 1 w 007 4 4 08 5 6 r( 4 2 7 1 u = 1 2 3 2 7 2 4 0 8 -- s a _ 4 0 9 0 e _ 1 4 1 1 3 4 1 D r 1 w 'w O a w v e w e e w e) c2 = A a m 4 4 9 8 6 0 0 8 9 0 4 5 9 _ y f d 2 2 0 75 07 3 5 3 4 3. w e 1 g r( w u 3 1 6 1 01 5 5 1 0 w 1 1 1 w s a 3 2 8 e 0 r i v 1 a w w e E w g l i w I ) 3 I l m ad n( 08 0 7 5 9 1 1 3 9 4 9 4 ) r 2 0 2 0 0 00 3 05 0 4 6 1 e e / _ E t m 0 0 2 0 0 0 0 0 0 0 1 0 5 5 n u _ C 3 w i l o - 4 _ R v = 3 e 1 g 4 F i e S ) 2 _ e. e m _ o s m _ t = ( w s d s n _ 4 4 4 4 4 4 4 4 4 4 4 4 e o o _ 6 6 0 6 6 6 0 6 6 6 6 6 r ri _ 4 4 4 4 4 4 4 4 4 4 4 4 r ct _ e c _ f e _ e s _ r ( s c e) _ i ~ n m = t i m s l ( i w r r eh 4 2 0 2 9 0 6 3 6 6 9 1 4 e t t 2 6 4 5 9 9 0 3 0 9 9 2 t 1 n g 4 1 7 1 1 3 2 7 1 3 1 7 c e n 4 1 3 1 a c e - 1 r n a l _ o h l. c t i e s n o i ) s s ) 5 ) s - p l = e e 5 2 5 e - g g 2 1 2 g - r e n

  • n 1

= 1 n e g a a = H = a _ t r ef ef e( e e( ef . e u l l 1 ( H l 1 m S p p p p3 p p 0 i 0 i 0 0i0i0 w n i i o p0 p0 p9 p1 p9 p0 o 5 5 5 2 i l t 01 0 1 0 0 0 0 0 0 0 1 f 1 p 8 h 8 8 8 8 8 88 8 / 5 I s 1 1 e i r h l ih 4 h h h h h h h S _ n S 3 i i c cf d ct c c c c e c ct L _ 3 s sA sA s s s s s s sA A _ b d T _ r 3 e n" " " " " " a " " " O _ u d T _ t E, 1 1 a1 1 1 1 1 1 l 1 1 1 t D A 01 2 - T n l 2 3 4 5 6 7 8 9 1 1 1

..._m ~ ~ 1 f t 1 C0RE B Y P A S S (*) .i 5 1 - tube size /sch 2" sch 150 i - length, mm .8380 - cross section area, mm2 1439 -l - inner volume, dm3 12.06 - ID surface area, m2 1.129 i I - CD surface area, m2 1.75 - metal weight, Kg 127.2 l I - curve number / type 2/90 (R=190) { 4/45 (R=190) -j i i r l b i D0WNC0NER - UPPER HEAD BYPASS (*)

r

) i I - tube site /sch 1" sch 80 l 5 - length, mm~ 2758 I 5 - cross section area, mm2 464 - inner volume, dm3 1.28 - ID surface area, m2 0.211 } - OD surface area, m2 0.387 - metal weight, Kg 22,2 .j - curve number / type 5/90 R=115 TABLE 3.3.5/13 - core bypass and downcomer-upper head bypass characteristics I i (*) Inlet and outlet no::les are considered belonging to DC and PC } i 63 i r

b e m w a b w iu b w g g q ai i y v i m, eg . y g g q e g xe y y q s 6 i vr h g + g e g .u = = q m d. e g 9 7 e s t e 4 e e g e m M t t e -v ) ) w 0 O p w W 0 0 O -y 8 1 l e = = h R R u c ( ( s Q 0 5 4 0 5 ir W 2 7 1 9 3 9 4 gr 2 2 1 ) I / b 5 9 / / 1 4 7 0 3 3 1 1 0 1 2 1 1 ? f fa = T. m 4 6 s e l ts i ta r e e t v c a = r M a h w c E 2 ie N m t m i 1 l 2 2 I a m m y e 3 e a t g p r r n h t a a K y p a i e e t S e Y c n , r r , / 4 s o e a a t r A / i m h e m t u e e g b 4 e u t e u c l c c i m 1 = = I = z t e o a a e u / + = s t r r 5 W P i , s v f f w n w S h s r u u l e 3 P e g s e s s a v b n o a D D e u i t t r 3 i w t e r t I O m c E. t l c .i 's I B u A r T I 1

y ? 20.0 - design pressure, MPa ( - design temperature. 'K 638 -l - number of U-tubes 13 i SOUARE .1 - array f 24.89 - pitch, mm - outer diameter, mm 17.46 i i 1.02 .} - thickness, mm - tube average length, mm 16742 - tuce active average length, mm 16564 -6 - straight tube average length,mm 8210 ?' - elevation of longest tube, mm 1 8323 I - elevation of shortest tube, mm

  • 8153 t

- elevation of 7 grids (upper edge),mm 1115,2230,3345,4460 i 5575,6690,7805 I - inlet plenum + outlet plenum volume, dm3 7.43 i I - heat transfer area referred to ID, m2 10.43 f - heat transfer area referred to CD, m2 11.81 - primary cross flow area (mm2) 2428 'l 12127 - secondary cross flow area (mm2) - tube material. ASTM SB163 Inconel 600 'i l The upper edge of the tube sheet is considered as reference elevation zero.

    • Sundle zone free of grid spacer and cold / hot zone diaphragm I

TABLE 3.3.6/1 - Steam generator tube bundle data i i .[ t I 65 l -l l r I t )

l 66 Tube R, 2, L, Elevation l j' (mm) Imm) (mm) (mm) l 1 21.5 8132 16331 8153 2 21.5 8132 16331 8153 3 30.4 8157 16409 8187 4 52.8 8182 16529 8234 5 52.8 8207 16579 8259 6 42.4 8231 16596 8273 7 42.4 8231 16596 8273 l 8 42.4 8231 16596 8273 l 9 42.4 8231 16596 8273 j 10 42.4 8231 16596 8273 11 67.3 8256 16724 8323 12 67.3 8256 16724 8323 13 67 3 8256 16724 8323 i d L, = 2Ze + 7t R, i a 2 I l SG tube arrangement I i !se%dM i - ND -d-8 d'-- "sMN Ms"- l oggg4C ~ IiI i TABLE 13.W2 - Steam generator U-tube bundle geometrical data I

?! i 1 tube design mearured elevation elevation (mm) (mm) SG-1 SG-2 SG-3 j '1 8153 8120 8120 8115 '} 2 8153 8120 8120 8115 j 3 8187 8185 8180 8185 '} 4 8234 8230 8230-8225 - { 5 8259 8250 8245 8245 - i 1 l 6 8273 8270 8270 8265 i.i 7 8273 8270 8270 8265 I 8 8273 8270 8270 8265 9 8273 8270 8270 8265 i i 10 8273 8270 8270 8265 l t 11 8323 8325 8320 8315 12 8323 8325 8320 8315 _j 13 8323 8325 8320 8315 I TABLE 3.3.6/3 - U-tubes measures elevations (referred to tube sheet upper edge). i j f 4 h t { 67

i

-] 9 l d l. ~w w or, e

m v ~ i c c m ~ e e w i e e 40 C B l i 3 d r r r5 e n F G G G 0 t 7 6 0 9 0 5 3 2 8 1 4 a 0 8 3 7 8 4 7 1 4 5 4 5 1 5 6 2 6 4 4 0 2 3 1 9 8 l 6 6 1 5 3 8 3 6 3 5 6 2 3 3 7 8 0 0 0 A 3 p 3 7 6 1 1 2 2 S 1 1 5 2 2 2 3 6 4 7 - I l 1 1 1 1 1 A A A A M S e u S S S S T I k - - - - S A c M MM M A i T T T T N a S S S S A A A A a. ta d ~ lareneg ) e d ro w i s ta 3 t .) r m e p e e 2 d e e m n m h s o e s ( d g e m K m e m o e l m m a ', c u a t b e a a I' h a l n t p e u s e s e M e t f o e o o t ei t s t r t r g r mv l b t t el z e s e S u n u) p p el z z v( y et e sD ,d a a ol t z o a s r r a rl Ot i t n nt n u o n nl el ed u r e e h u m e e e i o n e et e g 1 s eb e g ogl m el ml t e l s a s n / l u p m g nt i f e nt p p e r r r n p si s a r 1 e m u a a e ,ni u e o o ei ed el o r e n rh d h yD on y yh t t t ) s yv e vf t s - 4 i l pt e c e rI l / or r s a a a l r m a r s v x rl a mt i a a r r w m a a r r r e r e 3 u n n e a e rl d ed a et m me a ad ai m e e e s al g gb e a nl e el aiib p p e e ri wt p o pl E u et f r o z et n v r r u e e et e r o n p o ei L i i s st b a e e c zf si e p pt s sf st pI i ul sf B e r v e o l a A e e - 1u. h ( T m d d l os n e I

I r - primary side . fluid subcooled water t . pressure, MPa 15.5 . florrate, Kg/s 10.6 . coolant inlet temperature, 'E 599 - secondary side . fluid water /two phase mixture / steam- - i . pressure, MPa 6.7 i . feedwater flowrate, Kg/s 1.21 i . feedwater temperature, 'K 500 . nominal level, m (ref. to tuce sheet top) 12.75 l t . heat removal capacity, KW 2165 l . PORV set pressure, MPa 7.8 . safety valve set pressure, XPa 8.5 . PORV discharge flow-rate (7.8 MPa, x=1), Kg/s 0.24' . SV discharge flow-rate (8.5 MPa, x=1), Eg/s 1.72** i theoretical data with ID orifice = 5.2 mm theoretical data ID orifice = 13.3 mm TABLE 3.4.1/2 - Steam generater thermalhydraulic data 4 9 f 4 69 9 + m

STEAM GENEhATOR CllARACTEHISTICS --_.__._ --____ -- =__---- - _=_ =-- l description elevatlon internals cross section volume weight. l l mm mm2 dm3 Kg l


__.=.

feed water 14352-14352 / 1146 0.20 2.5 ~ nozzle thorus 14314-14390 / 833 0.40 1.2 J-nozzle 14390-14419 / 283 0.01 0.1 i usaiular 16253-14463 / 14162 54.88 283 (vessel) downcomer 4656 (sep. duct) 177.5 (loose flanges) _i 14463-13648 15695 (thorus zone) 20043 -13648-13523 20043/15495 13523-13265 15495 downcomer - 13312-2677 / 1452x2 32.06 421 riser 2648-4878 tubes / fillers 11773 141.30 1456.5 spacers / diaphragm 4408 (spacer) 4878-10974 tubes /fi11ers 12127 spacers 4408 (spacer) 10974-13255 fillers / ~18048 (fillers) but terfly valve 23527 ~ 18385 i separator 13255-16313 / 7088 21.92 40 nti ssm slome. 16H 1-17768 dryern i 4:1H72 1.16. 7 9 1421 (vcuneI) ' f 53.7 (dryer) _=-- TOTAL 387.56 2960 -J TABLE 3.4.1/3 - Steam generator volumes, cross flow areas andl weights. . o -e m

m m a -m%-m-=

  1. ,mes

._,_. -.s. w-wa e ,,m..m_.m_ .-4.. .w. e. ..,ee, -,g-hw v. y.. r e e wt ,i m w r .wp%a .y. ,,r,%,, gd y,., _isg-3 ....w..s-.,yey.- ,s %.p ,,wpg. y,w*' 4+4****-h'w =* -y w+Wevv +

I I I I 1 I i I 1 G r r r r r r r r r l G G G G G G G G G a i 6 6 0 6 6 6' '6 0 6 e r 0 0 0 0 0 0 0 0 0 p e 1 1 1 1 1 1 1 1 1 i t p a A A A A A A A A A m M M M M M M M M M T T T T T T T T T S S S S S S S S S A A A A A A A A A ~ A 4 3 0 / 3 N, 0 0 2 2 / ~ U / 2 L V 4 E 1 / n S 0 I O 1 3 f, 0 I, 2 L n o M. 3 3 I W L l i t 3 / V 0 / I W F. W E e c / 2 B, 2 F i n / 1 0 WI / I, F, 0 E. n e 2 / 0 0 1 F, L 1 l n 1 c G S S G I L L W L L o W S W F P S M M S 1 M F E F ~ / ~ n e) m3 7 7 4 5 2 6 7 5 4 7 8 6 6 u m 1 S. 4 4 4 d l 7 4 ~ o( 2 5 1 v 8 1 7 S 4 1 7 0 4 2 n = h t ) 5 2 2 9 7 1 9 9 9 g m 2 6 4 6 3 4 0 2 2 N n m 6 8 2 8 9 7 1 0 5 e( 9 8 6 4 4 7 6 3 9 2 l 1 2 2 2 1 a ) m m e( 3 d i r 9 3 3 3 4 3 3 s e 4 t t 8 1 3 8 0 0 3 1 1 u e 8 7 4 6 6 3 2 2 1 o m a i d ) m ta m ( a e d = 7 2 0 2 2 3 9 9 l 1 d r ~ i e A st 3 7 9 8 9 9 4 3 3 a A. n e 7 9 5 3 4 4 2 1 1 r w i m e n n 0 e i d g 7 m e 3 t 3 3 / s / / 2 y 2 2 / s 0 / / 1 O 3 g ~ 0 1 1 0 L L n g L L L L I h W W i t P F F p a, S S D W W i B E E M M S F F P i t p r s e y e d r n a a i e d r 1 h n e o d r r c a e e e r e t t S s e h s a a e d s s w w A n a e e e a d d i e n n n p e e / 1 n h i i i y e e l l l l b f f 2 m m p a a m r r r r y y 4 e e u e e e e c c e t t d t t t t n n 3 o s s a a a a e e 1 m w w e e g g E. 1 n n a d d h h r r l + i i e e e e e e e l a a t e e r r m m Ai m m s f f p p e e T n n j

t m ~ d m i = r e d a e h m - a 0 e 8 H H R t L L L 1 3 3 0 s - h 0 3 1 0 0 0 c1 6 3 7 4 9 9 9 -_ n u8 2 / // 4 0 - i 1 1 5 2 3 4 4 4 = - a ~ - m. ~ 3 o t V. I ) S - e - e -- M - v - v l l - m - a - a - o - v v . r - p n f - o o t i S s t a + E. o._ l t = o N = s s i I n o 0 o i 8 t 1 4 R ~ t 1 e c2 6 3 0 1 L 0 c h 7 5 M - n s0 7 4 0 5 L 1 - V - n 8 1 5 8 b9 4 S 8 4 1 00// M _ A - I o "4 - S - c 2 7 2 81 6 b2 m ,4 E - M. L - o T - o - H i R H S - r l l i - t 0 L L L L L M = f S. 8 4 6 0 s - e 5 1 0 5 3 0 5 0 0 5 m e c h 7 5 6 3 9 4 9 9 4 o n i l 1 8 ///// r i t r z c 8 2 1 _ z - s7 4 3 1 2 1 3 1 5 4 1 f -- s . N = o - ( ' l i I n - r r "3 e e A G - t t M - S - a c e a m - h r o - e a r - r h f R ' p c E f m o e D - t e s A - m y u s ~ E. l 1 o g 1 v n i e p h i 2 2 t p m m . M m) m m* s y A = ( e r 2 2 d a 2 2 a m m E a mm u d e3 e r m e3 e l n gp c o g p T r m e e t S. ad a aK y n c ad a aK y e e t i e r r, / h n ,r r,/ S h n c o e a at r c oe a at r e m h e u m h e s s i i / mt u e e gb - N / mt u e e gb l e m cl c ci m e m cl c ci m a 2 z e o a a e u . I z e o a a e u v / + s vf f w n 2 s vf f w n1 2 3 i, = i, st r r A - st r r e h s r u ul e h 4 ~ h s r u ul eL L L e g s e s s a v t e g s e n s a vS 3 S M b n o n t rM M M b n on t r 3 u e r nD D e u ) u e r nD D e u t l ciI O mc E n ci1 O mc L l ( L B A v T

STEAM DUMP (from MSL 0 to isolation valve) tube size /sch 2"1/2 sch 80 - 1enght, mm 26242 - cross section area, mm2 1 2734 - inner volume, dm3 71.74 - ID surface area, m2 4.864 - OD surface area, m2 6.119 - metal weight, Kg' 311.2 _ curve number / type 7/90 1.R i 1/15 LR l _ _ _ _ _ _ _ = = - - -==____- PHEHEATED L1NE i- =- _____ l _ tube size /sch 2" sch 80 - length, mm 7741 - cross section, mm2 1901 FEEDWATEH 11 E A D E H 4 - tube size /sch 2" sch 80 (d - length, mm 24937 - cross section, mm2 1901 'TADI.E 3.4.2/2 (cont'd)

FEEDUATER LINES (from isolatlon valve to GG nozzle) - tube size /sch 1"l/2 sch 80 - lenght, mm 4869 - cross section area, mm2 1140 - Anner volume, dm3 5.55 - 1D surf'ece area, m2 0. 5113 - OD surface area, m2 0.911 - metal weight. Kg 42.2 - curve number / type . FWL 1 3/90 LR p 1/45 LR . FWL 2 2/90 LR '1/45 LH . FWL 3 1/90 LR 1/50 LR PRE 11 EATER BYPASS i - tube size /sch 1" sch 80 - length, mm .10109 - cross sectlon, mm2 464 EMERGENCY FEED WATER SYSTEM' =------ tube size / sch 1/2" urh (10 lenght, mm r q . header (total) 29529 . header (up to stop valve) 14307 . branches'- 3029 cross section, mm2 151 TAlli.E 3.4.2/2 (cont'ti.) . _... -..., -, _. -.. _ _. _,. _. _ -..... _., _... - ~ - _ - -..... ~, _. -... _.. - - _., -, _. _ _, _. _ _. _. _. _ _. _ _ -.... -.

1! 'l i - accumulator tank : i f . number 3 i design pressure, MPa 6.9 'l i design temperature. 'K 623 minimum operating pressure, MPa 4.2 t operating temperature. 'E 323 't . operating water level. % 65 l.: . inside diameter, mm 248 .i i . height, em 2073 volume, dm3 '96 .) ? ^ material ASTM A 312 TP 304 s (, - accumulator surge line - . tube size /sch 1" sch 80 ) . tube cross section, mm2 464 j length, mm f 'I loop 1 6076 t f 1ocp 2 6089 -[ loop 3 6149 -l . material ASTM SA 312 TP 304 q TABLE 3.5/1 - Accumulater and surge line general data -i 'ti .l c I -75 'I t .. I t t a-

.=. l i - injection pump : i . max operating pressure, MPa 20- .l . max massflow-rate, Eg/s 2 . operating massflow-rate j (1.2 MPa discharge pressure) Kg/s 1.71 . i 4 HPIS/LPIS lines . tube size /sch 1" sch 80 . cross section, mm2 464 i length. ~ header (total) 24267' h . t header (up to stop valve) 16864 + branches 2251 I t i i TABLE 3.5/2 - Injection pump and HPIS/LPIS characteristics j 4 i ]- e f e t 4 t i e E i h 'l. 76 1 . [ t i l ~ i . ) i h ~ =.

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1 l ) gs n( - i 8 - s e - o m _._ l i - ct 5555 5 5 5 55 5 5 5 55 5 _ / 1 g m 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 n u i m ni e n pi d d d d d - o m e e e e e t t t t t a a a a a l l l l l p p p p p d dd d d d d 0d d d 00 0 0 e e e e e e e1 e e e1 1 1 1 t t t t t t t 4 t t t 4 4 4 4 a a a a a a a a a a l l l l l l l l l l l l I 1 I I - a - i p p p p p p pG p p pS S S S - r I I I I I - e _ 0 0 0 0 0 0 0 A 0 0 0 A A A A A t 1 1 1 1 1 1 1 / 1 1 1 //// / - a 4 4 4 4 4 4 4 2 4 4 4 2 2 2 2 2 - m 2 2 2 2 2 2 S - I I I I I I I F I 1 I F F F F F - m S S S S S S S - S S S - - - - - E - i I I I I I I I 2 I I I 2 2 2 2 2 f l l - r - A A A A A A A A A A U B ii0 1 _///////I ///I I l l 1 _-V - t 5 5 5 5 5 5 5 5 5 5 - / - L - y - 0 0 0 0 0 0 0 M 0 0 0 M M M h M - d 1 1 1 1 1 1 1 T 1 1 1 T 1 T 1 T _ A - o S S S S S S - b A A A A A A A A A A A A A A A A V - -- s - n - o M M M M. M. M M. I L M. M M. M M. M. M M. n 1 J - F - i _ L L L 1 I L L L I 1 n 1 I I 1 t o F - c d d d d d d d d d d d d d d d d i - e e e e e e e e e e e e e e e e e t 0 - n g g g g g g g g g g g g g g g g n / - n n n n n n n n n n n n n n n n n e f f f f f f f f 1 f f f f f t f i - o a a a a a a a a o a a a a a a a i _ N - c l l l l l l l l 1 l l l l l I l t __ 0 - d c - n e - e p u - D - ) g e - E - n 0 0 0 0 0 v - T - t 0 0 0 0 0 - i 5 5 5 5 5 0 l a - a 1 1 1 1 1 0 v - A - r 000 - - 0 0 0 0 0 0 - 5 0 0 0 " " " 0 " 0 0 0 0 0 0 " 1 l - U - I 5 5 5 2 2 2 5 2 5 5 5 5 5 5 2 - l - S 1 1 1 / / / 1 /1 1 2 1 1 1 / 2" a - T - N 1 1 1 1 b 1 A 3" 2" / ( - C - / 3 3 1 1 1 4 2 2 2 2 31 1 1 e - e - A - z v - i l - s a v R - e e e e e e e ee e e e e e e e t' r r r r r r r r r r r r r r r r e I - e o o o o o o o o o o o o o o o o l - p b b b b b b b b b b b b b b b b l A - y e t l l l l l l l l l l l l l l i l t l l l l l l l l l - e u uuu u u u u u l l l l l l l u u u u u u u d f f f f f f f f f f f f f f f f i - v _ / // / / / / ////////_/ u l t - a l l l l l l l l l l l l l l l l n - v l l l l l l l l l l l l l l l l a a a a a a a a a a a a a a a a o b b b b b b b b b b b b b b b b i t a e l n o i e n - n n i 1 - o e i nkl d i i a e - t l l l l l l l l ek t - c - n - o o o o o o o V V V - u - s u s s s s sl R R t r a a - f - i l i i i ii oO O oV l k b e u i o a r t nP P P R s r "2 e b c - s 1 2 3 1 2 3 0I O a I - s 1 2 3 P - e L L L L L ) L l.b / " I 1 2 r - c S S S W W W S D G G G H H " / i - o M M M F F F M S S S S P P 3 1 1 A = r p 2 / 1 - g A D t. - a // - t 4 4 4 2 2 2 4 4 6 6 0 1 4 J 0 0 0 00 00 0 0 0 0 0 1 - e 1 2 3 1 2 3 0 0 1 2 3 0 0 E, - v - - - - - - - - - - - - - - // l i - V V V V V V V V V V V V V l l - a - D B B D B D D H U B B H i A l v T l.'

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i s l 4@ e _ e la _ t l l l l l l l l l l l i _ s e e e e e e e e e e e r e e e e e e e e e e e6 e _ st t t t t t t t t t t _ t _ s s s s ss s s s s s sG _ a _ e W 'n l n nn n n n n n n n n _ m _ no o o o o o o o o o o6 b b b b b b b b b b b _ y _ i 1 _ d - a r r r r r r r r r r r2 _ o . t a a a a a a a a a a a _ b s c c c c c c c c c c cA n e s d . o wF F l F F F F t F F F F I t i l F t F - t e r l I H t i i R R H I - i t eR I cl _ sf f f f f f f f f f f cl l l l l l 1 l l 1 l l et i n u / ////////// // n o _ d J J J J J J J J J J J J wI H I I T T T T TT T T eT T T T I t I t I t t t o/ e e I I I I I I I i I I i_ ct t _ d l r.......... _ ei sf f f f f 1 f f f f f 1 _ n n cl l l l l 1 l l 1 l l I _ w _ o i. l ) _ f 2 _ m _ _ e m _ 9 2 9 9 9 8 8 8 9 9 9 2 l _ c( _ 5 3 3 3 0 0 0 3 3 3 S '5 i f a 5 5 1 1 1 9 9 9 S 3 u 1 1 1 e 1 i r r - oa - a gn i _ t 1 a _ S _ r' i 0 0 0 0 0 0 0 0 0 0 0 0 0 _ E _ I _ S t 0 0 0 0 0b 5 5 5 5 5 5 0 3_ 1_ 1_ 3 3 3 1 3 V _ N e 3 1 1 1 1_ A l . _ / t "3 "4 "4 "3 1 2 2 2 4 2 2 2 3 _ e u 1 2 A _ z o i V._ s = _ g n i t 0 0 o ~ _ Y a 0 0 n r 9 9 _ T 0 0 9_ 0 _ I t 0 0 " " " 0 0 000 0 0 0 u _ E _ S e 5 5 2 2 2 0 00 0 0 0 0 5 _ F _ A n - 2_ 9_ 9_ 9_ 9_ _ N l 1 /// 6 6 6 2 1 1 1 _ / i - 3" 3" 2" 3 1 1 1 2 _ A _ e 1 2 1 1 1 _ z n _ G _ i _ s _ e _ r _ u ._ ss) 0 4 i e a 2 0 0 0 6 6 6 4 5 5 5 8 8 8 0 _ rP p14 7 0 0 0 0 0 2 8 8 8 1 1 1 0 6 6 8 2 s ( 1 _ t n _ e o _ s i s n t e e a v v c V V V l l i S S S a a f v v i t t t c V e e e i i i nS u u u r r p o n n n c c c a a s i t o o o r r r p p t i i i i i i i s s e _ n a ut t t c cc v n c a a a r _ o l l y y y o e a u rl l l i t - miu u u r r r t r v c mm m a a a ai a i c _. s iiid d d c y l o y s s s n n n u t _ V r o o o m e l _ S aR R R c c c u m f mW W W e e e ci a i - Pi i P P P s s s c r S a l r 1 2 3 a p p1 2 3 1 2 3 i t L ,L 3 2 I Wi R G G CG G G T T T 3 l' P S S S S S S E E E n n / _ g 8 _ a t 3 1 3 6 60 4 4 4 1 1 1 e _ 0 0 00 0 0 0 0 0 0 0 E 01_ v' 0 2 3 1 2 3 2 3 L 1 // B l _ a _ V V V V V V V V V V V A a _ v _ S S S S S S S S S S S T j ) 1 u.

l! L P A r e p cO w -1 t + + e l ~ a.. i e r 6 6 6 6 66 6 6 6 e 1 1 1 1 1 1 1 1 1 t 3 3 3 3 3 3 3 3 3 m a 5 5 5 5 5 5 5 5 5 5 5 5 e m = I I I I I I 0 00 00 0 0 0 I I I 00 0 0 S S S SS S 1 1 1 1 1 1 1 1 S S S 1 1 1 1 y I I I I I I I I I + d A A A A A A A A A A A A A A A A A A A A A v o a b e e 9 c n a s + w m v + r o i. t c = e + n 4 n W W W W W W W W W W W W W W W W W W W W W e o S S S S S S S S S S S S S S S S S S S S S w-c + d + + n =- e 6 e = e 1 g n S i t e _ E a 0 0 0 0 0 0 0 0 w r 0 0 0 0 0 0 0 0 t V 5 0 0 0 00 0 0 5 5 5 5 0 0 5 5 5 0 00 0 t I 1 9 9 9 9 9 09 1 1 1 1 0 0 1 1 1 0 0 0 0 s L S - 6 6 6 6 6 5 6 - - - - 5 5 - - - 5 5 5 5 n 1 1 1 1 1 1 o m N 1 1 1 1 1 1 1 " 2" "2 "2 "2 w A A 2 - - - - - - - 2 2 2 - - / " " " " " " " / / / / " " ///" " '. " - i + / - t l' a -+ V e 1 2 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 2 1 1 e z c i i s f m i + c w D e p N s + w e e A p e + y v 1 l 1 t e e e e e e e e e e e e e e e e e e e e e e b b b b b b b b b b b b b b b b b b b b b a w e o o o o o o o o o o o o o o o o o oo o o v

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l l l l l l l l l l l l l l l l l l l l l 4 gg g g g g g g gg g g g g ggg gggg n la o v i + w t a los ) ) ) ) i e s ) s s s w s s s s s d + a s a a a n p a p p p a y p y y y e b y b b b l w b o 3 2 2 2 r 0 C 0 0 0 t 0 / 1 2 3 n 1 o V 0 V V V c C C C C, = F V L L d 1 C ( ( ( e ( n 01 2 3 L t ( 1 2 3 a w 1 2 3 0 0 03 o 01 0 0 L L L L 0 u e-i t L L L L L L WW W W L L L L l W W W c e l L L L t a S P P T T T P P F F F F W P C C D i c W D B E E E E E E E E E F D P P L P F F F a o d l na l m l w v C g - C D C/D Ia. 5 7 3 /// 1 / 2 2 2 4 1 1 1 7 000 00 6 6 1 0 1 4 0 0 0 / 0 O 1 - 0 0 O 0 0 0 0 0 1 1 1 1 0 0 00 0 1 1 2 3 8 2 3 0 - 01 2 3 0 0 0 - - e - 1 v - - V V - - - - V - - - - - - - V - - V V V 3 a a - l I C Vl I VI I I I l V I I I V C I I IC l C - V C V V C V V I V V V V V C l v - i I II l l I I I I i I I I I II li I I I l II E L e B s A a m T tu = r l t! [

L I l r~ w + w e e, sg u r e w cH n a + s a r l d. a 6 0 6 6 e i r 1 1 1 1 e 3 3 3 3 t 5 h 5 5 5 5 5 5 5 5 5 I 0 e . a 0 O 0 0 0 0 I I I 0 0 0 0 S S S 1 1 1 1 S - m 1 1 I 1 1 1 1 = I I I I y A A A A A A A A A A A A A A A a e d -s o b e m + e s 3 _ s _ n _ o w - i t c = _ e = n W W W W W W W W W W W W W W W n B H D S S S S S S S S S S S U a o c - d = - n e - e + e m - S - s - E i - g + - V - n o w i 0 t 0 t 1 a 0 0 0 0 5 a r e A r 0 0 0 9 1 0 0 5 6 5 0 0 0 0 0 0 0 0 - ) H 9 1 1 1 9 9 9 0 0 0 0 V I 9 1 i 6 6 6 - - - 6 6 6 5 5 5 5 - 2 t S 1 1 1 1 1 1 1 " / "2 "2 t 1 1 1 2 - - - - - - - 2 1 w A / " " " ///" " " " " " " / w w l e 3 J 3 1 1 1 1 1 1 1 i 1 1 1 2 w f z s w . i R - s e er - U - f T. s= e - E - R. e k k k k k k k k k k k k k k m - e c c c c c c c c c c c c c c .= - p e e e e e e e e e e e e e e w - y h h h h h h h h h h h h h h t c c c c c c c c c c c c c c e i f e - e n n n n n n n n n n n n n nt w = - o - v o o o o o o o o o o o o o o. e w w l t t t t t t t t t t t t t t p e - a s n s s s s s s s s s s s s o if w - v l i i i i i i i iiiiiil + p p p p p p p p p p p p p p c s i n m a o w i t o um e e a w g g c r r e e i = a a g n f w h h r i i c c a l c s sh e e i i c e p e d d s h s w i t p pd e m m n v w u u p o l n 1 2 3 p p m a t s e t I.L W 1 I,1 2 3 I 2 3 u i v s l o 2 3 a 1 i L. S S p e w .L L C C n W W 1,L I l a 3 S S F F F T T T P P P C V W l r e.- 1 l c M M M E E E E E E E E E E C F a u w o t t w l s e n r m i = n e t o a o i a t n -e ) ) ) y u 5 w - g ( ( ( l f, l / a 1 1 1 3 3 3 5 3 2 a 8 t 4 1 4 0 00 0 0 0 0 0 0 0 0 0 u 0 O 0 1 1 1 1 2 3 0 00 3 2 3 1 2 3 ?. 3 1 e t 1 v c m. V V V V V V V V V V V V V V V A 'E l o C C C C C C C C C C C C C C C L v ) B AT (

m i .i -t r LOCATION ROCK WOOL THICKNESS (mm) Power Channel . lower plenum bottom 120 . lower plenum upper side 100 i . core not insulated . uppper plenum / upper head 100 Primary Pump 100 Pressurizer 110 j Steam Generator 3 . primary plena 120 . riser vessel 100 . tubular downcomer 70 f . upper vessel 100 .[ . steam dome 80 =i hot leg 100 l' Icop seal 90 I cold leg 100 PC downcomer 100 PC core bypass 100 l PC downcomer bypass 70 PR surge line 80 spray line 70 main steam line 90 j main steam header 90 t steam dump 90 g feedwater header 70 feedwater lines 70 f r preheater lines 70 ) 1 l TABLE 3.9/1 - Thermal insulation thickness { i 3 I 4 -i 82 i h I i I

,I b i r k l _ a 2 5 _ 9 2 3 7 _ 9 3 9 7 7 2 3 4 1 0 8 t 1 o 1 6 1 1 1 1 1 1 1 3 _ y t y w y m W y e t s y d n n a yr 0 G ~ S a 4 / 6 1 3// / / 3 / / / //. 2 C i C l = N E i _ o x _ u _ a y i r l m a e _. _ mt _ 0 _ 7 - o s 1 / 8 r-3// / / / / / / // _ 2 - c y r _ e s w _ s w m _ y _ r m m _ a e _ _ mt 8 1 r. _ i s 3 2 1 3 1 / 4 1 / / 9 3 / 3 _ 6 - 1 _ r y _ p s m w n -w r e s o _ mt ., a a 6 _ _ e r _. / 7 7 1 e e _ 2 5 / 6/2 / / 6 2 / / 9/ 1 ts n _ 1 e _ g _ e ~ r e z e ir u 6 - 7 8 / //1 / /1 3 1 I 3 / 2 n 1 m s e r p _ r l e. _ e n 1 _ w n 1 2 1 S // _ o a 1 1 9 / 2 1 / / // 3 i _ ph. c t n e m e M r l e I u m _ o M - b W W C t s C 1 L L i V. 2 S a - m T. F e . y P P m i s D T A I. 'S E P S ) e f t e a e t n o_ r n a e o w i rt i y o b w a t ) d r l s r o r a r e a f e u I w s e r e m e b t f o) n t l e p m e el t e n w s u r e u k l u e s t w nl f c d ei v r o S s r a o a a e n v m e e p l t s uh eil t r ei o e sl t a - n e et p c rf g s p cl n t c n n - L 1 r r a i u h e a a e a i o o. e l x d r r p rii . A / u p r ef t I c t h m ) t t t - T 5 el i nl t n p o uit u) e s sf p g r e uai ol u t R wR ci a - O _ r ef m n ovf c( opf qP xC oC e st - T _ E u o o - L Tl T ri ei w s eiD n i l l m( f ( e p r,- l t ( rl a pd t s ( - e A - m T

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!\\ i n mu t t t e e e l l l t t t u u u e e o e e o e e o e ed d/ e ed d/ e ed d / mmm ii t d d i i t d d i i t o o o d d i i s s eii s s eii s s et t t l t t t s s s s l s s l d d n d d n d d n o o o t t l l i t t l l it t l l i bb b ooo o o o oo o o oo h h c c ehh c c eh h c c e S. S S. d d d l L l r r r ri r r r rir r r ri/// e e e e s e e e e s e e e e st t t w p p w w p p w w p p w c e e o p p o y o p o y o p p o yi ) l l u ul rl u ul r1 u ul rt t t ._ n l o a a a u u u i e e e c m e e e e m e e e e m ooo b b b b ib b b b t b b b b i i a u u u u r u u u u r u u u u rG G G p S_ S_ r t t t t pt t t t pt t t t S _ o 2 3 1 2 3 1 1 1 1 1 l 1 1 2 2 2 2 2 3 3 3 3 3 l 2 3 f 1 t _ P i P L L L L L l G G G G G G G GG GG G G G G S. S. S iI t I I L t t I C C C I I I S S S S S S S S S S S S S S S l 1 ) a _ mP _ 0 0 0 0 0 0 0 0 0 0 0 0 0 00 0 00 00 0 0 0 0 0 0 0 uK _ 0 0 0 0 0 0 00 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 7 7 7 m( _ 7 7' 7 1 1 1 1 1 7 7 1 7 1 7 1 1 1 1 7 1 1 i 1 1 1 x e _ 0 0 0 00 0 0 0 0 000 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 a y, m n _ a _ r _ ) ( _ e _ m _ i . t e) _ 0 0 0 0 0 00 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 000 0 s d _ 6 6 6 6 6 6 6 6 0 6 6 0 6 6 6 6 0 6 6 6 6 6 6 6 6 6 6 n m _ 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 o( _ _- p _. s e r o _ t . y P, s r n _ i a a _ l r r _ u g r) _ 1 I I 1 I 1 1 1 1 1 1 1 a 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 r % _... J t a( _ 0 O O O O 0 0 0 0 0O 0 0 0 O 0 0 0 0 0 0 00 0 00 O t n _ _ n _ i / _ e _ m e m e r u s t a _ r r r r r rrr r r rr r rrr rrr r r rrrr rr n e t _ e e e e e e e e e e e e e e e e e e e e e e e e e e e a m n t t t t t t t t t t t t t t t t t t t i t t t t t t t t e _ t t t t t t t t t t t t t t t t t t t t t t t t t t t s l m _ i i i i i i i i i i i i i i i i i i i i i i i i i i i n a = u _ m mm m m mm m m mm m m m m m mmm m m m m mm mm o t r _ s s s s s s s s s s s s s s s s s s s s s s s s s s s c n _ n n n n n n n n n n n n n n n n n n n n n n n n n n n e ts _ a a a a a a a a a a a a a a a a a a a a a a a a a a a e m _- n _ r r r r r r r r r r r r r r r r r. tr r r r r r r r r r m i t t t t t t t t t t t t t t t t t t t t t t t t t i r t i t e p t x n E _ n e _ o m u i t r 3 _ a _ P P P P P P P P P P P P P P P P P P P PP P P P P P P t / _ r s 5 _ i g _ 0 0 0 2 2 2 4 4 4 5 6 7 8 3 5 6 7 8 3 5 G 7 8 3 9 9 9 n _ r a _ 0 0 0 0 0 0 0 0 0 0 0 0 0 00 0 0 0 00 0 0 0 0 0 0 0 i E 1 2 3 1 2 3 1 2 3 1 1 1 1 1 22 2 22 3 3 3 3 3 1 2 3 L _ i t ) B t _ n _ P P P P P P P P P P P P P P P P P P P P P P P P P ' P A ) i _ e _ D D l D D D D D D D D D D D D D D D D D I D D DD D D ( T _ d _ i g ( l lI1[l l l l l{ijlI! ll1'l ll 1 L

i den t i fica ti on inntrument min necuracy response t.ime (*) maximum localion . tag +/- (%) range (ms) range (KPa) _ _ - - - - - - - - - - - - - - - - - ~ ~ - - - - UP 110 P trannmitter O.1 160 0-100 f.S 1-1,5 tiol tom /RP l>P 210 P transmitter O.1 160 0-100 1.5 2-1.S bo t tom / IIP' DP 310 P t ransmi tt er O.1 160 0-100 l.S 3-1.3 bott.om/RP DP 001 P transmitter O.1 160 0-100 DC upper zone DP 002 P transmitier O.1 160 0-100 DC lower zone DP 003 P transmitter O.1 160 0-100 PC inlet DP 001 P transmitter O.1 160 0-100 PC lower plenum DP 005 P transmitter O.1 100 0-100 PC lower plenum j DP 011 P transmitter O.1 160 0-100 PC rod butulle l DP 012 P transmitter O.1 160 0-100 -PC rod bundle } DP 01.1 P transmiller O.1 lho 0-Itki Pt twl bundle f IP 015 P Iransmit.ter O.I 160 0-100 PC upper plenum DP 016 P t ransmi tt er O.1 100 0-100 l'c upt cr head DP 017 P-transmitter O.1 160 0-100 PC upper head DP 018 P transmi tt er 0,1 160 0-100 til.2/WSt.-T junc tion DP 019 P transmitter O.1 160 0-700 WSI. Iower side DP O20 P transmitter O.1 160 0-700 WSI. upper nide-l DP O21 P transmitter O.I 160 0-100 Pit I)P OP.' P IranumiIter O.I 160 0-100 Pit i Di' 023 P tranumiiter O.1 160 0-100 . Pit OP 031 P transmitter O.I 160 0-100 l'il DP O25 P transmitter 0.1 160 0-100 Pil j DP O26 P transmitter. 0.1 160 0-100 PR I DP O27 P transmitter O.1 160 0-100 Pit DP 101 S transmitter O.1 160-0-100 SG 1 riner (*) instrument time constant . TABLE 5/3 (cont'd)

illljli m4 = r r r o o o t t t a s a s a s r r r r r r r r r r r n e a e e e a e e e a e o s p y s s p y s u p y i i e rii e rii e r t r sd r r sd r r nd ac 1 1 1 2 2 2 2 3 3 3 3 o G G GG GG G G G G G l S S S S S S S S S S S = ) a mP uKm( 0 0 0 0 0 0 0 0 0 0 0 i 0 0 0 0 0 0 0 0 0 0 0 1 1 1 7 _ x e _ 1 7 1 1 1 7 1 a g _. - - - - - - - - - - - mn _ 0 0 0 0 0 000 0 0 0 a _ r ) ( e m _ i _ t ) _ e n 0 0 0 0 00 0 0 0 0 0 _ s m 6 6 0 6 6 6 6 6 6 6 6 n( 1 1 1 1 1 1 1 1 1 1 1 op ser e y g - c n - a a - r r - u 1 1 1 1 1 1 1 1 1 1 - a( - 0. 0 0 00. 1 . 0 0 O 0 c) - c% - 0O = -- n - i / - m + r r r r r r r r r r r - t e e e e e e e e e e e tn - n t t t t t t t t t t t a t - e t t t t t t t t t t - n _ m m m m mmmmi i ii t - m i i i i i i i m m m s - s s s s s s s s s s s n - r . n n n n n n n n n n n o - t - s _ a a a a a a a a a a a c n _ r r r r r r r r r r r _-i _ t t t t t t t t t t t e m ) i d t t t n n o n e c o m ( i u t r 3 a S S S S S S S S S S S t / c s 5 i 2 3 4 1 2 3 4 1 2 3 4 n -- f g -- 0 0 0 0 0 0 0 0 0 0 0 i E _ i a _ 1 1 1 2 2 2 2 3 3 3 3 L _ t t ) B _ n - P P P P P P P P P P P A - e _ C D D D D D D D D l D ( T l - d - i ll t !l!ll

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l P02 (Pal 512 I F 120A Pie (P,1 B12 j l C2 P11 (Pal B12 l L 110E P10 (P ) B12 1 i i (P,1 l-5/1-3.5/1 F 220A P20 (Pel P21 (P ) 812 I i L 210E : P20 IPal i. C3 F 320A P30 (P,3 B12 ~ f ( P,1 l-l SM-3.5/11 L 310C P30 (P l i. C4 l l P31 (P l 812 i i i P,1 1-5/3-3.5/1f. t DP=P -P 3 2 , P15 A1 P 10&P P 20&P f P26 A2 i P 30&P ! P3B A3 ! P 0015 l P01 B11 i P 0045 i POS ! B& EE!IE h 'E TABLE SA - Piping instrumentation loation P 3015 P30 B7 P 002A i P01 t B12 P 003A i P05 C5

J 6A.R.4 1-MA5LEIST IW5515E EFERDE ffA5LIBUT TDPERATM IEFEEEE TAG TAP IEEE TA6 - TAP lEIE I ~ T 001P T01 3.3.5/1 RM 001P P02 A10 P03 A10 T 01&P T01 A12 PO4 A10 T 015P T02' A10 P05 A10 T 017P T02 - All RM 003P P6 3.3.5/1 T 020P T01 A10 T 101P T10 A7 ~ P07 3.3.5/1 T 102Pa T11 A7 RM 101P P11 A1 T 102Pb T12 A7 P12 A1 T 103Pa T10 A1 P13 A1 T 103Pb T11 A1 P14 A1 T 10&P T12 A1 RM 201P P21 A2 T 110P T10 A4 P22 A2 T 111P T12 A4 P23 A2 T 121P T01 A13 P24 A2 T 201P T20 A8 i RM 301P P31 A3 T 202Pa T21 AB P32 A3 P33 A3 T202Pbl T22 - A8 P34 A3 T 203Pal T20 A2 RM 302P P33 A6 T 203Pb T21 A2 T 20&P T22 A2 t P34 A6 P35 A6 T 210P T20 l A5 T 211P T22l A5 P36 A6 T 301P T30 A9 i RM 303P P31 A9 T 302Pa T31 A9 P32 A9 T 302Pb T32 A9 P33 -A9 P34 A9 T 303Pa T30 A3 RM 30&P P36 I A3 T 303Ph. T31 A3 P37l A3 T 30&P T32 A3 - l T 310P T30 A6 T 311P T32 A6 T 0015 T02 B4 T 0055 T02 i B9 T 0075 T03 810 T 1015 T10 55 T 1045 T10 B1 T 2015 T20 i B6 T 20&5 T20i B2 T 3015 T301 B7 T 3045 T30 B3 I T 001E l TO1 C1 l r T 001A 701 C5 l T 002A T01 812 l T 011A i T02 C5 i l l TABE W4 (conrd)

m _ ~ _ _ V E N T 11 R I TUBES ___ ______- _ _ = - - _______ = measurement tag location fluid throat throat code ratio diameter (mm) 1 F 110 P 1.S 1 hot water O.489 34.4 ASME F 210 P LS 2 hot water 0.489 34.4 ASME i F 310 P LS 3 hot water 0.489 34.4 ASME F 110 E accumulator line 1 cold water 0.103 7.8 F 210 E necumulator line 2 cold water 0.103 7.8 F 310 E accumulator line 3 cold water 0.103 7.8 F 102 S SG 1 downcomer hot water O.250 21.4 ASME F 103 S SG l-downcomer hot water O.250 21.4 4084E F 202 S SG 2 downcomer hot water O.250 21.4 ASME F 203 S SG 2 downcomer hot water 0.250 21.4 ASME F 302 S SG 3 downcomer hot water 0.250 21.4 ASME s-F 303 S SG 3 downcomer hot water 0.250 21.4 ASME F 104 S MSti I steam 0.073 19.7 F 204 S MSL 2 steam 0.073 19.7 F 304 S MSL 3 steam 0.073 19.7 i F 017 P DP 00 hot water 0.110 14.6 ASME F 014 P BP 01 hot water - 0.137 9.0 TABLE 5.2/1 - Vent uri tube specifications H . O (d E -w wa-e-mee-,e'-- 9,_,-- E w o ,-g e we+* 4 * ,w--ww. -Tw Wsw v-w--r --**et w emTT +- =a**-+e*'-e-*' "+w-e* v"-*-v N-tem *"+-*""'r"T 'e g

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F 121 P WSL hot water 0.084 4 F 001 A PCL hot water 0.047 3 F 011 A LDL hot water 0.047 3 F 001 E EPL 0 cold water 0.489 17 F 120 E EPL 1 cold water 0.169 10 F 220 E EPL 2 cold water 0.169 10 F 320 E EPL 3 cold water O.169 10 F 001 S FWL 0 hot water 0.258 25 Util F 101 S FWL 1 hot water 0.155 15 F 201 S FWL 2 hot water 0.155 15 F 301 S FWL 3 hot water 0.155 15. F 005 S SDL steam 0.662 48 UNI F 007 S. PIIL ateam 0.661 40 Util F 020 A EFWL 0 hot water 0.189 6 F 120 A' EFWL 1 hot water 0.084 4 F'220 A EFWL 2 hot water 0.084 4 F 320 A EFWL 3 hot water 0.084-4 1 TABLE 5.2/2 - Orifice nozzle specifications - s O h 4 --m. ww n m- -ww-w o m ww.- ww.-w e 4,e e v -r-m,v -ee w s eev e wwe-ww w ee-,. ,mw,.- v.m e,w ,e+-+-.--+% - +- ,,m-he rwe,, w-e-r, e e w -t -- u ear 'ev ww ww us-t e-+ --w +--w+=1-aw e-w*,s.. w-ew , e-ww-r e+ s. w + -e +e r ewe + ww m e-s w +w ~e w,,e e.~w w. w +e-w

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i i COLD LEG DC intet I front view ~ PD-7 suttion I Nr v e i@- g- .p '= ,/ COLD LEG V / /* plan view 14 LOOP SEAL b '(3 plan view s' ;' Af @ p from charging line h ( 'T 9 <-) 1) from ECCS W g ~ \\ SG-7 outlet ^ i e +-1 v' i=@ (jD-25 t -W u ht LT: ;

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C lD ~ = \\ ap-2 dischargt_,/ RD-2 surHon i ,_ to fetcown " line LODP SEAL front view l h >} n / *L. ~ ~..~. ~5l.~ D ' wh*6 Venturi flewrneter I t PC eutlet SG-7 outte i e -e HOT LEG I SG-7 inlet 7 N HOT LEG plan view - h i ga to Surce L.me o g ,_hg g SG-7 intet ^ / ,/, ?' / Rt euttet U .__W_stms!* -f g./ i e v b 4 a Fig 33.S/3 - Sketch of primary piping loop 2 \\ treferred to tables 33.5/349) w j t )

l: DC inlet i N i @-9 @-T I i EOLD LEG plan view EOLD LEG cP-3 suctien l h -) front view = w-@ l [ E LOOP SEAL j jj plan view 1 [ h @ ~' i .-____e @~I ~ t from Errs A } b l ?r@ Y % @ ~6" y# = pp.3 distrarg j' I GP-3 suction [ ( f LOOP SEAL front view Venturi flewmeter @ @Y, / _ _u? i j ^ a, \\'I l f M' e 4 SG-3 outlet \\ PC outlet i I / 50-3 intet, HOT LEG front view )4 @/ j n, 7^ C) i $p t HOT LEG pian view \\ { I i' ' ' j\\ @/ f ss.3 intet i L-._ I h; ,i s _5pgpaicpst PC outlet W ^,^ I l j \\ i Fig 3.3.5/4 - Skekh of priwy p&hg loop 3 ) (referred to tables B5/k1M

  • j t

to PC upper head i Ji "n -4 l from COLD LEG - bh l No! f C U 3 8 .c 1 1 8 C O i A turbine flowmeter insertion ) is foreseen [ = l 9 I -- to Power Channel 7 i l Fig. 3.3.5/5 - Sketch of Downtomer (referred to table 3.3.5/11) 1

Pressurizer connection -s O@

= dD zi p

~~' & fi~ i l W ). l 1 1 I h h [,/ =; SURGE LINE plan view i .j k ud l iN @ 100 \\ N Tunbine flowmeter position 'u H Hot leg connection \\ l SURGE LINE I.__! front view m'y \\ \\ (! 2 /. T) 9 hi O l i l Hot leg connection i i Fig. 3.3.5/6 - Sketch of surge line (referred to table 3.3.5/12) \\ 1 i

t i i B 1 a .S i U i ? y .w y/Kl 1 f/ "/, M f I i i A l .B l C l f ML 4 2 3 / L*a 4 2 3 66.G l dio l 'o CL 4 2 3 E.6 dig l "o 't l SL 24.3 53.6 1 'o __ C+ l l g s 3,', G' w-U l u ,7 s l l s ~. t 1 i }l/ 1 c l l I e 8 ~ s l-x E N l i ,i I ~~ ~ lC l 4 l 8 lC l C lE l F l 4 l -* l 1 J h iLss (eirca. co-ecT>j 2" l SSc l '40 l 67 1 24 l.5o j 46 l 4"o l 60.3 l 23 do? , u L 4 7 5 ( Pc )) 3' lfo(4lNo }402 2a l SS l 66.G142S l os I ao i 35 l i )l S' l 234 l MGo i 96 24 i SS l M 6i'26 l69 l 23 l407

ut +2 S (ec

)! W l 29o j 225 422 26.5 l Go l 92 (480 l dia l 55 l 338 j l cc l a.ewoK ~ ) l 4' l 090I 225 422 25.5 l Go .) 2 ldSo I dia i 35 l S5 -l [=c_(Pawum )l 4* I 28S I 225 i Sac ; 33.5 l eo l m2 I <79 1 125 i So l 45 l Oc ( Pt:. N i ] < _ __ a ~ l I Q. ! a-- I N-1 p., l .1 8 C o -i E us 4 2 S s*= 2' l 204 iA60 26 24 es -. l C' 1 2 S 5'=27d eco I46o So 24 55 l l c I L' l < jC l L' M -l N i O lP l .6 l A j i L' 's 6a S l 49.2. lGc.6 ' 126 l SS 23 j oc7 L G:f l 2o* e M 73152 1666: 428 i 75 23 14 7 Mo* I C* l i 4 i Fig. 3.3.5/7 - l.cose flange details l 4 l ) v-

W D O @Dhk NNNNkD TNG N N 8 / /O.. \\ <. ~, m nv I j

, /

i l sa caess secrew e j jb .9 / h 8 't o ,3h h C, ~ ~ t.u. y h l { / / [,/j/,/ sc amt srtTow j [ Tr prearter msTaustwTaw ve, w. ,t 7s k TWre0.5 t l x4 e 1 l TusE Cress strTow I i b rust m t w w = = O i I E E i@ J-f i l@n3 l j i i i nuo u s i I ./ ,/ I _ L __ j 1.] I I l l I! Fig. 3.3.6/1 - Steam generator tube bundle instraentation details'

i 1 Tube R, 2, L, Elevatica (mm) Imm) (mm) (mm) i 1 215 8132 16331 8153 2 215 8132 16331 8153 3 30.L 8157 16409 8187 4 - 52.8 8182 16529 8234 l 5 52.8 8207 16579 8259 l 6 42.4 8231 16596 8273 7 42.4 8231 16596 8273 8 42.4 8231 16596 8273 9 42.4 8231 16596 8273 10 42.4 8231 16596 8273 l 11 67.3 8256 16724 8323 12 673 8256 16724 8323 13 673 8256 16724' 8323 d L, = 2Ze + Tr R, i rJ 5 i i 5 l l SG tube arrangement I i I g ~ I, I li .w ^ -EK3- - $5&$& __.Sh.M.g?__ 1 H,.G.) II I i 1 r TABLE 3.3.W2 - Steam generator U-tube bundle geometrical data i -n

n.17768 ~ m e l A

i
=

j ' T [ 16313 n. 0, $l } =. C u c.14352 p- ~l I j ~i I lf ~ !l i i l1 i ll il i ll j li I II I wi n n

s' c.13255 M'

t ,N-l oi l hs Ni l 3 gl j i hj ~. I 5l C l 1 - ;[ 7= p.E-l 3 ii r. I Ul l l I V y 4, w) b' a y I l l. l 3 1 I R .A f:\\ I iI( ' {f T ll s i i 1 O 3 o l a ji4 4ei r ) e i i \\'4 '\\tt_ bt h. R i s m + k%hlgl I I a e.76&8 i e.76LB I 'l 11 t{ll l ' t;- h il

  • i

[L-T_J l ~i si tt12 4 Fig. LL1/1 - Steam generator general arrangement.

  1. t j

y %. l I s i s 1 2 u z n I-i i s [, a. .h TJ.10780 2 s \\ / t i 4 \\ / V) i I f T, ^ j j -T-1 s s l l l 4 i I c 1 ea n R. b 't il I s 1 i I T e l 'i k. s i I L l I I i e t I i l [ t i I\\!/' ) l :' \\/' _b 23 N N b e173.1 s s i j \\ \\ j N l t { .i i ? N j j o lt l l s i i i I s.y ? I. W,j. g g s n h 3 I J l 4 i I 3 .s i 2 l l 1 s P, l 0 N l [ l s'- y i e l t N N' l I -s l ( l ll I s;-, x l r s p N I s N s n Y \\. Ykkf y n I i I tl N i g s l s l: i i s 1 -~f \\ S ji s ~ ~ T E 4 s 1 o p p q m a Y/ 'h I E r- .A M. l l M M-i. )-Pp l l ry.76&8 i ~, ) ? I.N . QN g% e300 hPj i N) ; l lf [ l j <j // r,',, ~. e320 6 E h 82" est2 t -m :

w.

1--,.q i 4l i y l P

  • ' ~

_.j[_i_ t 8279 i { l l6262I Fig. 3.4.V2 - Steam generator lower section 5 i

3 e50Bx.40 .17768 U i E _I ,,'V F/ E a 42111' o / /, i, ' Sk .k' t d r a'N I vg[ I\\ l /3 INb ,/ .s y n ( y, aE N, \\ .N-A ll ' w A' _. th1L b M221 /, ,- j , / $189. [' l o ~ E j' ~ ~ , j] i 8_ 30* ~ v.- .16313 U I l r i l l C --hv LL[ 2 o a e 1 9 i .i. ~1 I [. I, i f ]'s .I g 30' o S g j' 7 t c } J a 2 - 250

  • E j
eun,

= i l a l +1435. p W t e115 'T* l I e eMr1 = m ~ to ~4:7 I = = s i a ., R \\} g 'j / El / t-- M /j k h, E ~ 1 et ) -. t I .'/'/ ff-a *181 a q / s g ur. - w ,/, N / / SA53 [ m. m i. s l,-_*b _d, h m s i s 13255 g - 4I D AD- ~ %j ' ~~~ l , 1 -T* ensi g 30 les i 13005 U l

I =%

s i j l_ #173'08.! t ~ e 219.1 sh fig 3.4.12 - Steam generator upper section

i e l i. G 1 I a x O M M D sit H i NN Yl ljl tlh i is ai ! 'l' dl ! , I,i A, i i L ,e 7 I i I h j yi n. 4, ,i Vl p' I $lV i J,

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'l 11 a r i a ,f. n l !! l !li ! h .,r @ ill t ,ll : } F414.V4 - Stem generate I l i'- l il I tube budte I 5 spy /b tape f -ia, 4 .-l l i i 'i l ,1l l 4, i ,i 4 t VY W Y = L [

i ,ca f M 8#4 L, t, et i t. / //M t k f ? t* l (* j! --] EG ".x 1 i( 1 j. ,e "g 4 \\ bN' i i N s--Vt2 _, f _ / x- ~ s C y is M 4 's l ID [ l/ l 4 l ) % srl n xn unt 170 t ,un nn n _ n n un l i L i i i L 6 l t N M ' .\\ s fC30G i r h' h "" = 's (, l:c A ,w=

  • t J:

,,%@lh 9 ga li JH ? / A i hi Y ;lL __._ j l i '4 jQT s N,;,;4, - i i A s/ / If>, j / / 8 gf s,*t -n Fig. 3.4.1/5 - Steam generator riser cross section and spacer gkd l e

e 8 t Sect. B-B 40

  1. 428 40 l

l g g a Y i a 4 '3,' // 'l l m m l j l 1 s E l S k h l . bu 4% 60. u \\ j: I / __@25x14 { f i e i s, VIEW from A 9 g, 4,, g b ~ 57,, "l i d 4 0 s - l

a e h x >r _- La a

.y a wt \\v i A 4 b T 20 20 i 30D 3 y

  • 3 _

_2 0_. 20 20 20__2 __20 20__20_ _3 8 i0 _l_ 80 40 160 Fig. 3.4.1/6 - Steam generator dryers

-.~. e. s l-8 i . l. l @] a w i iI 1 \\ _a o s 6L. 9, I-l[ l s, n 4 ) t t

  • D

~ i. i, 0 I i 4 g-I i l -t t i PLAN VIEW l b 2 E 93D-2 l

  • t 4

. wm I j , 4 h,, g" .,e se s l E M-EJ 1N Yi 3 ~ T 4 t b i l . g ] i j ji!E!!!E ~ g-t + f = i E. . g t t v@ g, l l' 'I { 1P 4 6-e 2 I ,i 4 .r s B' i l ll ~ 9 1 1 5 g y t i Fig. 3.5/1 - Accumulator cross section 4 w w ey w ~ I

1 I i -,s /96@@6'N GOGGOOG,\\ /,-G@OGOGGGG.\\ roe, 3i.n.n.92 ,e@ese@ese@e s i / GOOGOO@GGGG ', i .n, e, l -@@ e O @ e @ e e G \\ eOOOG@eOOG i i \\@OOOO@e966@d i g . > (o2ce) g.ii roo, J-e e @ G e O y-3 IlI.32,cg y_gm i, g,.. 3.n. ss..i. n'-+ sect 0 'd j .u,* fw,;),..

5. i..t>.2,.1.

O hat rad 22 g ,.e. u.u.3,.u.s3.,3 4 e i

  • I" rod 31,59.66.,2 X

'"' (lQ) ,.e, 3.n.ss.s,.n l . ast / w 3,. 5.3.n.u.a _ llIlI a \\ "' /,w ,.o 22.23.39.55.s3.,3 g lo.o su I-rod so p 4 Fig. 5/4 - Power channel rod bundle instrumentation f

i i rt g ttAsmD05 9 m TAP TE 8 e nruna E W w P 017P 3006 h DP 017P P, G 3006 A t eno

  • " ?'

P, G 1209 \\l DP 016P P O .1209 t P O g,go DP 015P P 0 0.00 2 I P O -1509 t DP 013P P: O -1509 l P O -2619 i Op m P DP 012P P, G -2619 l P O -3729 i t DP 011P P -3729 l r P, -5209 , DP 005P. P O -$7gt 1 l P O -Site T-i i DP 00&P P, G -5998 I P, G 7044 g DP 003P P O -5990 DP 016P P O -4351 c} Wm s T 016P 3126 T+~ j T 203P 0.00 T 103P 0.00 7 103 T 303P 0,00 7 203 l DP 015P T 012P - 750 I 3fI-T 017P 1 T 003P -4351 T 00&P -70&& l l TW 008P 4 -1&&O T i I:2: m TV 20fP f -1575 L 003P -1629 4 'M i L 002P 1999 M TV attp L 001P -3109 y ee,p t 202P y DP 013P i* ' ' DP=P1-P2 e L C01P

/

i W DP 017P t b 1 i m I i i 1 e DP 011P 1 F 1 i DP 005P DP 003P f e4 M f DP 00&P T m. /- :L a ' 5; 5/5 - Power chawl eranamt T 00tP W l 1 avspeactil

h 'l i i e e77p I i OP 875 g (A515tDUT $ ) IAP l 1 TAG d IIIVAfDi T 0760 p}.. ' Op c?6P E E ' temi . ~ f ow ec5p 2 P 027P- .165DL t c13p DP 027P P, O 16269' N P, O .16504 M) DP 026P P, O 159&9 b@/ P op e75P P O 16269 4 1 DP 025P P, O 15519 ~~ P O 159&9 Te75P/ g P, O 15519 DP 02&P P, O 14075 0 l S__} @ 3,,,,, DP 023P P, O 12631 P O 14075 DP 022P P, O 11187 t mp 4) p, O 12631 i DP 021P P, O + 97&& ( P O 11187 L 010P P, O + 97&& P, O .16501 i t 011P 13229 t 8'0' 7 e7tp g--]@ L 012P 14729 L 013P 15769 N-_1 2!L.122E T 026P +16269 T 025P-15011 M r T 02&P 13753 s t sup / T 023P 12&95 T 022P 11237 T 021P 9979 RM ODSP t ld--1@ t eup - q QP = P, P l -) 2 t22P n l EIDNAL IGHT P1 q]{ se i .t210 .-w- .1810 T e;;p g 1-2540 'O -3 y .3700 -i 2 E- .4670 ( 5440 i.,..ooms to m=== l 1 l ia Fig. 5/6 - Pressurizer measurement arrangement

a -t i f(AS' 00lf O l [ J TAP 'T B&S 1AT. E CD& TIE t='t P 10&s g g w k P 10&P 2123 P '10&S 17713 l OP uts DP 193P P, O + 2123 P O 2123 l . DP 185P P, O 2123 P: O 72&8 -j i l DP 106P P, O .teste I P, O-724 'l DP 197P P Q-7248 P,, O .tette i l DP 108P P, O 7248 j P O 2u3 _j DP 1915 P, O 2668 &c 1 P O 4648 T 7 t N:,ag'\\ OP 1C25 P O-6648 N Pi O 1314: N L uns DP 1035 P, O 1314: P O 17023 \\ DP 1 cts 4 DP 104s P O 17023 c=~~3 P, 9

  • 17713 s

i r t l L 120s P O 136ss P, O .16348 - -,=J .l i-l L 1105 P, O 2668 l 'i e !' a P O .163ts i L 1015 3393 1 P-L 1825 . 3843 j ll. l W 11ts TW tt:5 L 1035 106&g T 15&P 2123 1 1 / T 1945 1830$ i T 185P 2833 TV 1855 + 2233 T 1C55 2898 i I T 1875 l 110 5 l .i T 10&P 6893 T ic7P --4-- 'i TV 1061 . 68f3 s l T 1865 . 6 egg TW st75 s L,b _/ p /h M. l T 197P 18918 N3~ TV 1ets .te,in j } T 1975 .1c:33 g, I i l T 10tP 6893 SL TV 1885 . 64f3 fg ,fg L 123s / l TV 1815 + 2t33 1 i N i l j T tcts 2:33 DP 107P J N DP 106P j h g1g g I J i I TV tits 13258 A I f F 1925 . 1500 l I F. 1935 . 1580 L u?s Qt T #6P -] a ' TW 1065 f' / -I DP=P -P d [I._,F1ers-rte 3s a, 1 2 jl q P3 = upstream tan T cep W #85 e t -j P2 o wnstream tap l l .g DP 100P j { l l N DP icts L 101s, ) J l 1 i T 185P f-T 199P s ' o f,,. w uss i i j w n,s x . !Il 6 ' T wss i 7 #fs '

  1. 1;-

I --ij,j 1 -l + lL l T 10&P 4 i T T1DP 1 DP 105P rc _J ~ g P mP i I 4' j l Fig. 5/7 - Steam generator measurement arrangement l 1

a e l; .E$ i Woca ice m aa aus E 3 y i e e f y a l E I l e a E e g y tg

e; e

I N w5 .N 8 Eni

t

/ D !( Ih / / r!r i / 4, \\ 1j ? n., i g }} / a "l-s = 4 ' 11 E 5 x =- 'E= \\ l w wwts e m g ~- E y5 E j\\ .,. can / /\\ c e ter=d e >c ' o &l i I n v, g g, 11_ v'8 5/ _Ii mi = 8 l m_s! y ' --- s 3 I s-f 1 .m g a \\ E E i in \\ [ [ it j/ f / \\ s // / y-1 g pues A // \\/ il ] \\ t .__ /\\ _ / _J _ 3 r \\ .n ; M5 7e v5 Dl l a $= t 5 W 5 5 [.E_ 9 N e ~w G a A h b I it l E i E Q ww 5 m, 3 5 E II a a s Ii /

a
5 v

o i z l 5 s t de-1 i. B s c g 1 m k u 6 a ~ h,l / e &w. 9cM J/ a I/ / e W30tl ElindWD] r +- 9

SG-1 / s t f4 g A' j "1f'4% A ' % 'D7, I m S s 9 c' Oy nh E! /) g/ s.-. s 9' / 399 ,~ / o '5 '1%>9 i DD [ ("l Nh, t x N 1 2- + k o (*) - Spool piece POSIIIOD gp-94 o of ' ) g '4 g 4 i.:j Vi o 9 1 + q f, 1 e~ >M t I \\ t ? PC e. , '" \\, \\ Fig. A 1 - Hot leg n.1

r t i 1 'I f i i l 9 i I i L s i N SG-2 ) l <= ks i i i q' t ) DD %%%Q i (*) - Spoot piece position g,j, 43 l ~ og i ~L l st p e,, j \\ sp ? >"a v"m % v I 'y 4 I gi, i PC 't

  • 77m !m.

i Fig. A2 - Hot leg n. 2

l J SG-3 xi ( ci,f ' N!51 ~E v N M's~ $ gJ,i / ..x q / $l ci W / O " *1tsy /

  1. p
  2. N s

N / /, e l l l i DD __ /(*) j gy / / (*) - Spool piece position I 8 d i SL fb [ 3 $~' %l /' * % d,$h jV. R / h, mg i i E "%s ^ nem of ~, p4 ^! I j-rg 'e DJ/@g/#m kgg, " J== pc 4 s

== / / Fig. A3 - Hot leg n. 3

l SG-1 '# , Ro d / N9, / N .41 Y, ] / /'4 a g-a . cb a / y w / ) /x

  • 1r,

s '!rm l I j = E' @o i l RP-1 i I f .;5 m I t ~ //S \\, 4 o a g a: a s 0' I i M N I 4/ Nsy m E A. ~ __N q l N wm Fig. A4 - Loop seal n.1

i

SG-2fgj

>\\ r ',A "i t ' Ei s N s t>y N 'R fi N l ~ N x N N 2, 2l 3 8 h l 0 / RIN T' ep o ~;'N Si7 I R i RP-2 S h g j / \\L- / ,,VG y/ ofgi,e 4 \\ o'>,7 N 4, y / c>' l ~ / s x. h 'Y "j g LDL V f y x' y . on, s of Fig. A5 - Loop seal n.2

I SG-3 l l %, '.' ^ ' % ~ / $h' vO sp /', A x,: f f f& RP-3;L / ,+ 4 w h / (Ja* o '~i A/ 8' 8 n 2 i e gx,+ ~ 'N, "4 g ? A g. ? ',g 'sh a

i *~

of ., i' / x - a*> ' b l q. s w a l o / \\;'g < f/ s 'Ny FIN. A6 - Loop ggg, g_3 1 i

+ of.av a is s s / / / eg e s e, Si l '[ \\ I e s 1 9 s e ni >vu os ,_____,.\\,. g l , \\ N l a CL w / s / e s a / W i i l 1 1 i cn i ) N ( \\ OA y h of s-g . o: w' \\ i m \\ a. 'u N' ~ + e l \\/ n: J g ) L/1 3 = \\ \\ \\ Fig. A 7 - Cold leg n.1

i x \\ \\ [4 \\ \\ \\ v \\6 g\\ \\ Ti il \\ x s $ 's\\s

  1. 1\\

~w~~~Lf,' syo gr /? / al / l i \\ f 9b / N t Egyalgyta .~.

  • 9 e

.s \\ \\ ~~ 21 {g m. \\ ( . 8 ,/m, t gya y e,,,\\. ./ r. s .\\ %/ ~1 4 / / fi A8 ' Cold te9 O 9

E g/.-.a 7 eu / /_. _O / y g_. /e 21 l sca f,, cc : SCd j' g/ ece p, tre i 1 2/ ~/ cu v scd / O wi l l C i 1 / l' i / / i = 4 (i \\ s \\ \\ \\ { \\ NI $\\ \\k ca N s w / s \\ / \\ 7 \\ i s, aW e \\ \\ \\ P / 'W OE.L ~ ~ ,' 9 .j f =~ L / A x e/ l 2; D, i 1 Fig. A9 - Cold leg n.3 2

I I e A )s-h s u (s'of r,A a " l lPR i; pi / I oki/*N 1 E .4 A l l i l @l # ' j o -Rctof n ,,+ 'h \\, qf' p J / d E, / / / o, p '/ f O,',, / y," Y, -}g4.& s f*4 .i HL-2 1 J-1 1 lJ i Fig. A10 - Surge line i S

k .l .i t i f fc /[ d i N f PC 4 ~ \\ 23 T i f'/ JI g N e% $8 j 7 / f l ~ m. \\ ? C v ?- \\ y /n jf Y I 1/ l 19'"l j f w 8 sx j j l '*9'N t f i 2\\ < pc l d / i I f /gg su ,/_ 1 F@. A11 - Core bypass .] 1 j i

-j \\ s \\ PC \\ i 7)f 0 h \\ -s \\ x R 'k y \\ \\ 'O \\ 4 \\ \\ N. \\ \\ q \\ \\ k N \\ \\x \\ d ' N% \\ tad b; at .Q \\ S %O 's'W 4 \\ x i i~ \\ 2 M \\ \\ i i Fig. A12 - Downtomer upper headbypass t

+ I 40 co - do l a ><,/ ~ l 28 9 1 se lx' g f* ~ ^ 4 y ,/ 97 Ss. l \\ ,\\gl

  1. P

<a8 Nls 3n I / 1 ,h \\ t ,/ 8 ? /p CL-1 e",/ gp V Fig. A U - Pressurizer spray line

1 %E# / N,j.,/ .h k sgqq A l N '4 h D w N$ h ' x., xj 15o gtsc-4 t N ( W bh - lf ib305 's. ' N hp fV k** Q-p- 8 4 x y:,4 ' g j,, ' +. ' mN 7 \\ s a-T A-o--4 n x + is Sj_ _ L; Vsqb l, \\5 2so QPORV t o q ~ (sa e c t> N nsw 3 ~ Nk{0\\ i'g N ,4, 4 3 4h i, i / ask i 4' l 1 N'65:3 9 f ~Y' .20 - [ d e , to k O '/ \\ - /49'/ ~ /g ,/ / ? j sl N i -k/Ig% .3, I ~ J-2 h L'N_ .r% ti N> A 'n a4 xp ot---- m 3 s s t t a, N<x 's = o o . b*4 ). sso y,Q. { PORV 4g -9q N x -Nd n (x o 0 ~ O M51V R % 23o 43 l N - r Ak ' si ~ %q p?g. o g 3 pf v d5 x y' MSL-0 '% ) Fig B2 - Main steam line n1 ~ uy a

b s-a a ~ \\ J, ^, i I .f< a \\ 9 g? u\\ h ~ t e a Ng"y NN. E / ~ y oN N SG-3 4 n / ~ ~ 58 ~ y o/ N 1 2so x s \\ tyoRV f .E% t W 4 a 't \\ w\\ 1 N N-zm . q Q ~w = \\ t ts t-3 N \\ % fi v ~ m \\ 66 i W O, e h \\ b / h j'; 4* l we 7 p Mst-0 / / ,7 fig. B3 ' Main s' team tine n3 1 ' h

~ MSL-2 MSL-1 \\ MSL-3 \\ ' h. 's 4':P k, t i N 'b-N f -i ~ k .i g t-iSDL i @99 -/ ,/ .j / g0 \\ / 4', - \\+ j b '/ PHL -g ,ysd ~ qJ3 _Sipp valve / M [' Pressure control g, 7 i valve \\p \\ I e e O \\ q 'N v g s1 4 \\ SDL i T i Fig. B4 - Main steam line header i s

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