ML17138A548
| ML17138A548 | |
| Person / Time | |
|---|---|
| Site: | Susquehanna  |
| Issue date: | 08/28/1975 |
| From: | Keil, Rupp PENNSYLVANIA POWER & LIGHT CO. |
| To: | |
| Shared Package | |
| ML17138A531 | List: |
| References | |
| V-822-RF13, NUDOCS 7903150374 | |
| Download: ML17138A548 (88) | |
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PHILIPPSBURG NUCLEAR PONER PLANT - FIRST EXTENSION HOT TEST
~
SPECIFICATION FOR THE TESTS OF THE RELIEF VALVES AND THE ENERGENCY AND SUPPRESSIO{'l CHAI"SER COOLING SYSTEI"iS as translated from,.G. E.R. M AU 4
KERNKRAFPPIERK PHILIPPSBll HErssTEsv SPEZrFrKAZrON D, TESTS D
NoT.- ufo KoIsD,-KA~vER-Ku WOT>CE THE ATTACHED FILES ARE OFFICIAl RECORDS OF THE DIVISION OF DOCUMENT CONTROL.
THEY HAVE BEEN CHARGED TO YOU FOR A LIMITEDTIME PERIOD AND MUST BE RETURNED TO THE RECORDS FACILITY BRANCH 016.
PLEASE DO NOT SEND DOCUMENTS CHARGED OUT THROUGH THE MAIL. REMOVALOF ANY PAGE{S) FROM DOCUMENT FOR REPRODUCTION MUST BE REFERRED TO FllE PERSONNEL.
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PROPRIETARY INFORMATION This document has been made NON-PROPRIETARY by the deletion of that information which was classified as PROPRIETARY by KRAFTHERK UNION AG (KWU).
The PROPRIETARY information deletions are so noted throughout the report where indicated by a)
Use of the term KRAFTWERE UNION AG PROPRIETARY INFORMATION~
b)
Use of blocked out areas by cross hatch bands in the report text and figures/tables<
e.g'ii) iv)
...." with a mass flow density ofLWWlKg/m2s...";
KL%tmm
...." should be kept below ~W w~~ atm."
8/17/78
Kraftwerk Union V 822/RF 13 Offenbach, 28 August 1975 COMPANY CONFIDENTIAL Philippsburg nuclear power plant First extension Hot test Specification for the tests of the relief valves and the emergency and suppression chamber cooling systems Rev.
0 Rev.
1 Rev.
2 Rev.
3 28 August 1975 1 November 1975 15 May 1976 Prepared:
/s/
Prepared:
/s/
Prepared:
/s/
1 September 1976 Prepared:
/s/
(Rupp V 822/T)
(Keil RF 13)
(Keil RF 13)
(Keil RF 13)
Remark concernin Rev.
3 The entered changes have no influence on the scope and execution II of the tests.
The entered changes are identified by (3).
17-1
I I
I
)
I I
I
~> Vent, clearing pressures
- Tempratures at the main valve
- Positioning signals for the pilot valves
- Volume flows into the main-steam-line legs IV To determine the dynamic behavior of the pressure suppression system
- Pressure load on the inner walls of the suppression chamber
- Strains at selected points of the suppression chamber To determine the behvaior of the lining 17-13
I I
I I
I I
The coverage of the measurement channels of the recording instru-ments is such that the number of measurement signals to be con-nected is. selected in such a way that the number of measurement channels per test does not exceed 40.
In particular, it is necessary to specify the switching of <the strain gauges in due time before beginning the test.
Details concerning the different tests are given in the legend (4.1).
Other instructions for performing the tests have still to be clarified, but they will have little effect on the overall test program.
4.3.
Le end for test r
ram l) The valves are designated as follows (see Figure l):
ACRa21$
211 B@ Ra 11 S 221 CRAa 11S 211 D ~ Ra 41 S 221 E 4 Ra 41 S 211 F
a Ra 31 S 221 G & Ra 31 S 211 H'2 Ra 21 S 221
- 2) For normal manual opening, the pilot relief valve is actuated first and, after a delay of l second, the pilot safety valve is actuated.
In this test series, that should be done in such a way that the opening of the main valve is hardly affected by it.
- 3) The opening here should be accomplished only via the safety pilot, valve.
Therefore, the automatic system described above should be out of operation for this test series.
17 "14
I I
I I
I I
I
- 4) There is a rise of the liquid level in the RPV by 15 cm and the temperature of the reactor water falls by 5'C,on the average; smaller pressure drop in RPV.
- 5) Injection into RPV may last at most 1 minute.
Delivery flow rate ca.
1000 t/h at ca.
- 404C, si,nce suppression chanher water is being heated up in the meantime.
This results in a liquid I
level rise of 0.70 m and a reactor water temperature drop of 110 C on the average.
The reactor pressure will also droop slightly.
- 6) An attempt should be made to perform this test via the functiorel group control in order to maintain the broadest possible inspection.
The details as to which criteria have to be simu-lated and which switching actions have to be shunted are yet to be stipulated.
Starting from the nominal liquid level of 14.1 m, we roughly estimated a test duration of 90 s and a
'Iliquid level rise of 0.47 m (only due to coolant injection, without foaming up). It should be weighed whether the test should be begun with a reduced liquid level.
A temperature of 40'C was assumed for the injected water.
- 7) If possible, this test also should be performed via the functional group control.
This is yet to be examined in detail.
I For an injection of ca.
1200 t/h (40'C) through the core spray rings, the result is a pressure drop of 2.2 bar and a liq};id level rise of 0.80 m during a test duration of 1 minute.
17-15
I I
I I
I I
Reactor liquid level before beginning of test:
13.1 m.
. 8) It must again be clarified whether the test is run by functional I
group control or manually.
The readar fluid is cooled down to 60'C in advance.
5, Instrumentation The appended Figures 1-14 and the lists of measurement points include measurement transmitters which are recorded, by means of the special instrumentation.
Operating measurement points are Figure 3:
Figure 4:
Figure 5~
Figure 6:
Figure 7:
Figure 8:
Figure 9:
quencher F
meridian 108' 145o s
228o II 2444 II 260o II 284'lso included.
Figure 1s Survey diagram Figure 2:
Instrumentation of relief system F
DA ~ pressure trans-ducer DMS ~ strain gauge Wd;WA ~ displacement and accelerati~
transducers Figure 10'etail, of instrumentation of T-joint Figure 11:
L-joint Figure 12: Instrumentation of bottom mount Figure 13:
lining Figure 14:
Summary Pressure transducers in suppression chamber 17-16
In the lists of measurement
- points, subdivided according to the instrumentation diagrams, all measurement transmitters are listed individually and the location of their mounting is indicated.
Together with the Figures, the mounting point is thereby specified exactly in all cases.
In, the lists, the measurement transmitters of the operating and special instrumentation are identifed as follows:
(BM) + operating measurement (SM)
+ special instrumentation All temperatures are recorded throughout the entire test period with Polycomb recorders.
The analog data collected by the special instrumentation are recorded by fast recorders and also on magnetic tape.
To be able to follow the blowdown processes acoustically, an underwater microphone is installed with a loudspeaker on the control panel.
During the tests, the steady-state data are recorded with the process control computer and the transient data with fast recorders and magnetic tape.
In particular, the following quantities are determined<
In the blowdown tests:
- Excitation impulse (also on special instrumentation)
- Positioning signals for pilot valves and main valve
- Lift of relief valves (also on special instrumentation)
- Reactor pressure (sometimes also with special instrumentation)
- Liquid level in RPV 17-17
~
~
Test of RCIC system ATM}
- Excitation impulse of.TM system
- TM pump pressure
- TM flow rate
- Liquid level in RPU
- Reactor, pressure
- Reactor coolant temperature
- Temperature of injected water
- Pump speed Test of coolant injection system gTJ}
- Excitation of TJ system
- Flow rate of TJ system
- TJ pump pressure
- TJ turbine speed
- RPV liquid level
- Reactor pressure
- Reactor water temperature
- Temperature of injected ~ster Blowdown with holding-open system
" Excitation impulse (also on special instrumentation)
- Positioning signals for pilot valves and main valve
>> Possible liftof relief valves (also on special instrumentation)
- Reactor pressure 17-18
~
~
I I
I
" RPV liquid level
'" Reactor water temperature
<< Amount of water injected in to RPV
>> Temperature of injected water
- Pressure of RHR leg and core spray system
- Final position setting of the torque valves of the holding-open system Recirculation in coolant loop RPV - relief valve - suppression chamber - RPV
- Positioning signals for pilot valves and main valve
- Liftof relief valves (also with special instrumentation)
- RPV liquid level
- Reactor pressure
- Reactor water temperature
- Amount injected into RPV
- Temperature of injected water
- Final position setting of torque valves of the holding-open system 6.
Test conditions to be res cted
- When heating up the reactor pressure vessel before the tests, it must be made certain by means of sufficient venting that no more air is contained in the RPV or in the relief lines during the first blowdown test.
A reliable method of venting is to be arranged.
17-19
- Zn all blowdown tests, including those with the holding-open
- system, the nominal water level of 16.54 m in the suppression chamber is to be respected.
Before beginning the test series, the liquid level indication in the suppression chamber should be checked by remeasurement.
- The liquid level in the RPV should be. at the nominal value of 14.1 m at the beginning of all blowdown tests.
Exceptions are listed in the program.
- During water injection into 'the RPV and also during the blowdown tests with holding-open
- system, the internal axial-flow pumps should be running at minimum speed.
- During all other blowdown tests, the axial-flow pumps should be shut off and interlocked.
- For relief systems G and F, the pressure in the blowdown pipe must be checked before beginning a test,.
Deviations of more than 0.10 bar from atmospheric pressure must be avoided.
- When lowering the reactor pressure with the relief valves, pauses should be intercalated in order to respect the permissible cooldown rate of the RPV.
The following temperature gradients apply:
50'C/h between 285'nd 185'04C/h below 180oC 17-20
I l
I l
A voice link must be installed between the measurement rooms for the special instrumentation and the main control, panel.
7.
Documentation I
- Report KWU/R 311 " 3100, KKP I; Hydraulic holding open of the
.safety/relief valves in the event of loss of coolant
-.Specification KKP 1/RA 49/& ~ 202 KKP 1 - Design and control of the safety/relief valves, March 1975
- Specification KKP/XZ/00/SD/001, Rev.
3 KKP containment instrumentation, July 1975.
- KKB - Specification for the blowdown tests in the non-nuclear hot test, Rev.'I, 4 October 1974.
Attachments!
Instrumentation diagrams 1-14 Lists of measurement points 0 21
l
Figure 3t KKP I Blowdown tests in the hot test Instrumentation of quencher F
(RA 31 S 221)
Revision 3 of 1 Septertber 1976 View tow rd fittin
'L: KKPI-Abb!osever suche beim HeiA!est instrumenticrung der Diise F (Rk 31 5221)
All strain gauges on tteo quencher arms displaced. rotation ally to the left byQ$ mm from.
middle of weld on the top of the two quencher arms Revision 3
vom 1.9.76 Antlers ttey:nFmnniick Atte DrCS cd beidenO sen-'rmen evMh, nm nn SP>>eJL-.cbt-mitte ovf der oberse'.te bLder oisen-orme lines drebend verse'~
Dv.S-23 /
Dt~ S - 25/ 25 DMS-24 gy
/I
-19'MS-2D y
~
%MS-21/22
//
Top and bottom or.
quencher arr..s in the vertical plane MeC ve~cnCEr.rx r w tn Cp sm"ewcnrwne
)7-22
Duse A V/A'-16 ADA-1C
+ 12,78m DA-16 WA-17 DA-15 DMS e6 DMs e7~
~-V+-1e D.~s-ee Des-e9
,Figure 4:
KKP 1 Instrumentation of the suppression chamber Meridian 108o Revision 3 of 1 September 1976 Bild 4:
KKP 1 lnstrumentierunq der Kondensotions-Kcmmer Meridion: 106
'e V i S i On 3 vora
- 1. 9. 76 17-23
l l
GhlS-9r V/A-)9 Dh<S -95 Figure ss KKP 1 Instrumentation of the suppression chamber Meridian: 145o
'\\
Revision:.
3 of 1 September 1976 Bi ld 5 'KP 1
lnstrumentierung dcr l<ondcnsations-Kornrn "r
Meridian: 145 Rev is i on:3 vom 1 9 76 17-24
+16 5/i Duse G
SVA-20 DA-18
. /
+ 12,700 DA-2 DA-1 WA-21 D MS-90
+ 10,45 DMS.91~ 9 VlA-2?
DMS 92 DVi5.93 Figure 6:
KKP 1 Instrumentation of the suppression chamber Meridian:
228'evision:3 of 1 September 1976 Bild 6:
l<l<P 1
Instrumentierurq der l<ondensotions-l<ommer Meridian 228 o Revision: 3 vom 1 9.76 17-25
+16 Sc
+ 1450 DA-6 DA-3
~
)5"-'A-5 DA 4
1045 Figure 7:
KKP 1 Instrumentation of the suppression chamber Meridian:
2444 Revision5 3 of 1 September 19I6 Bild 7
KKP l lnstrumentieruno der l<ondensa t i ons-Ka mr@ er Meridian: 244 o ReViSiOn: 3 VOm >.9.76 17-26
DW DMiS-60/70 eini /ii OA-12 L
DA 7
+) 5.0<
DMS-6 DAS'iviS-65 Ot'5 -6r Quencher F
DUse F
WA-23 IVA-15 i
DMi5-6 3,
~ + 11,92
> DMS62 V/A-)i Dt~iS-60 DMS-61 DA-10
- 1) Strain gauges doubly glued, wired, only
connected once DA-8 DMS.52.
10 ~5 DMS-53~i'<XDiiS.50 DMS-57 D MS-51 DMS 56 DtdS SS DMS-59 DA-9 C
- 1) DMS doppett Kteben, verdrahten,nur 1-fach anschlie Aen Bitd 8:
KKP 1
instrument'icrung dcr Figure 8:
Kgp 1
'-"r.
KOndenSCtiOnS-KCrnmer Instrumentation of the
'Vleridjpn '60 o suppression chamber Meridian: 260'evision:
3 vom1.9.76 Revision:
3 of 1 September 1976 17-27
Ouse E
Quencher E
4 strain gauges, each displaced by 90'A-t3 IMS 85 rxOMS jeweils urn 90o ver se tz t tutze ouf 205 Support at 285'teS 64 2'70 CHSS2
'80 DMS s3 Bild 9.'<KP 1
1nstrumen tierung der Kondcnsotions-Kcmmcr Meridign: 284 Revision: 1.976 Figure 9
KKP 1 Instrumentation of the suppression cham e
meridian:
2844 Revision:
1 September 1976 17-28
KRAFTWERK UNION AG PROPRIETARY INFOKIATION 17-29
-KRAFTWERK UNION AG PROPRIETARY INFORMATION 17-30
Figure 12:
Instrumentation in the region of the bottom mount in the su'ppress'ion chamber Revision 3 of 1 September 1976 DMS-78 DMS 79 J
pp DMS-7i,/
i DMS-75 I
'.DMS-eO DMS-Bl Strain gaug 73 glued longi udina ly
+ 9690 rn jest)
)
~ 3)
$ }j3 IIiti DMS-73~
m) t 't le re tP gaged'~~
Kegelr ippe kleig<
Middle conical ribf at Y( A - 11/12 cu!
253'VA
- 17 oui 103'V A
21 oui Ansicht von un'.cn egcn Ri ppe View from below toward fin WA-12 Xy
~J Dlts - 72 longs geklebt V(A-11 (t
~l il Meridian 250 Bild 12:
lnstrurnen t icrung des Bereiches Bodenha t t er un'n der l(ond-l<o mm er Strain gauge 72 glued longitudinally RevISIOn 3 v. 1.9.7p 17-31
l
Figure 13:
KKP 1 Instrumentation of the suppression chamber lining Revision.
3 of 1 September 1976 at DlAS-96 ouf 106 t:".)
P QS-97 cu f 2 28 of'n>
PMS-9B ouf 26DO l.")
DMS - 99 au'09 fui
~
DMS-100 auf 228'ui Dt>S -101 cut 260 (u.
Bi ld 13:
Kl
4: KKP t tnstrumentierung d" r .Kondcnsotions-Kammer mit Drucl<oufnehmcr Revision: 3 vom 1 9.76 Figure 14: KKP 1 Instrumentation of the suppression chamber ~ith prcssure transducers Revision 3 of 1 September'976 17-33 t KWU-RF-13 Revision No.: 3 KKP hot test Blcwdown tests on relief system Dates 9/1/76 No. Measurement Location of measurement ooint transmitter Remarks Measurement group classification Relief s stem A (RA 21 S 211) on Meridian 108 1 ml 2 W 1 3.W2 4 W 3 hP across flow.limiter YD21 P 101 Liftof relief valve Positioning signal for pilot relief valve Positioning signal for pilot safety valve dynamic BM III SM III SM III SM III (3) 5 P t 1 6 T-l 7 T-2 Control pressure for relief valve Temperature after pilot relief valve Temperature after pilot safety valve dynamic SM III Log before and SM III after each test SM III Relief s stem B (RAll S 221) on meridian 84' m2 9 W 4 10 W5 llWW6 12 P -2 st 13 T -3 14 T -4 v BM III SM III dynamic SM III SM III dynamic SM III Log before and SM III after each test SM III hP across flow limiter YD11 P 101 Liftof relief valve Positioning signal for pilot RV Positioning signal for pilot SV Control pressure for RV Temperature after pilot RV Temperature after pilot SV (3) NOTES> BM ~ operating measurement SM ~ special measurement U ~ measurement direction circumferential V ~ vertical M ~ meridian I KWU-RF-13 Revision NO. s 3 KKP hot test Blowdown tests on relief system Date: 9/1/76 No. Measurement Location of measurement point transmitter Remarks Measurement group classification Relief s stem C (RA11 S 211 on meridian 36 15 A2 16 W -7 17 W -8 18 W -9 V 19 P t 3 20 T -5 21 T -6 V hP across flow limiter YDll F 101 Liftof relief valve dynamic Positioning signal for pilot RV Positioning signal for pilot SV Control pressure for RV dynamic Temperature after pilot RV )Log before Temperature after pilot SV )after each BM III SM III SH III SH III SM III and SM III test SM III (3) Relief 22 m3 23 W -10 24 W -ll 25 W -12 V 26 P -4 st 27 T 7 28 T-8 NOTES$ s stem D (RA 41 S 221) on meridian 324 hP across flow limiter YD41 F 101 Liftof relief valve dynamic Positioning signal. for pilot RV Positioning signal for pilot SV Control pressure for RV dynamic Temperature after pilot RV /Log before Temperature after pilot SV )after each BH III SM III SM III SH III SM III and SM III test SH III (3) R ~~w(as~ KWU-RF-13 Revision No.: 3 KKP hot test Blowdown tests on relief system Date: 9/1/76 No. Measurement Location of measurement point transmitter Remarks Measurement group classification Relief s stem E (RA41 S ll) on meridian 284 29 m3 30 W -13 v 31 W -14 v 32 W -15 v 33 P -5 st 34 P -1 35 T -9 v 36 T -10 v Iift of relief valve Positioning signal for pilot RV Positioning signal for pilot SV Control pressure for RV Pressure before orifice Temperature after pilot RV Temperature after pilot, SV dynamic dynamic dynamic Log before after each hP across flow limiter YD41 F 101 BM III SH III SH III SM III SN IIX SN III and SH III test SH III (3) Relief s 37 m4 38 W -16 v 39 W -17 V 40 W -18 v 41 P t6 st 42 Pd-2 43 Pd 3 44 Pd-4 4 5 Pd-5 stem F (RA31 S 221) on meridian 260 hP across flow limiter YD 31 F 101 Liftof relief valve dynamic Positioning signal for pilot RV Positioning signal for pilot SV Control pressure for RV dynamic Pressure before orifice dynamic Pressure before orifice = static Pressure after orifice dynamic Pressure in blowdown pipe + 17.54 dynamic BN III SM III SM III SH III SH III SM III SM IIX SH III SM III (3) NOTES: KWU-RF-13 Revision No.: 3 KKP hot test Blowdown tests on relief system Date: 9/1/76 No. Measurement Location of measurement point transmitter Remarks Measurement group classification 46 P -1 f 47 Wd-1 48 Wd-2 Vent clearing pressure before quencher inlet + 12.47 Gap measurement between cladding tube and blowdown pipe Gap measurement between cladding tube and blowdown pipe dynamic Relative dis-placement in x-direction Relative dis-placement in y-direction SN III SH III SM III (3) 49 Wd 3 50 DMS 1 51 OMS 2 52 DMS 3 53 DHS 4 54 DHS 5 55 DNS 6 56 DMS 7 57 DMS 8 58 DMS 9 59 DMS 10 Vertical dimension of blowdown pipe relative to bottom mount At blowdown pipe + 17.54 m N N + 17.54 m N + 17.54 m N N + 17.54 m At cladding tube 1 x d below strut application point (d ~ diameter of cladding tube N Bending in y-direction SH II SM IZ SM II SN II SH II SN II SH II SH II Vertical strain SH II Vertical strain SH II Relative dis-SH III placement in z-direction (U) 60 DMS 11 61 DMS 12 62 DHS 13. 63 DMS 14 At blowdown pipe as far as possible above the quencher ball 389 mm above weld to the quencher ball Bending in y-direction N Bending in x-direction N SH ZI SM II SM II SH II (3) (U) KwU-RF-13 KKP hot test Revision No. s 3 Blowdown tests on relief system Date: 9/1/76 No. Measurement Location of measurement point transmitter Remarks Measurement group classification 64 DHS 15 65 DHS 16 66 DMS 17 67 DMS 18 68 DMS 19 69 DHS 20 70 DMS 21 71 DMS 22 72 DMS 23 73 DMS 24 74 DMS 25 75 DMS 26 Quencher arm - 1 Quencher Quencher Quencher Quencher arm 1 arm - 1 arm - 1 arm 2 Quencher arm - 2 Quencher arm - 2 Quencher arm - 2 At blowdown pipe 389 mm above SN to the quencher ball } At blowdown pipe 375 mm above SN to the quencher ball Vertical strain SM II Vertical strain SM II Internal pressure and SM II thermal expansion SM ZZ (3) (in circumferential direction) are determined Bending in x-direction SH II SM II y-direction SM II SM II x-direction SM II SM IZ y-direction SM IZ SH II (V) (V) (0) (U) (U) (V) Relief s 76 m4 77 w -19 v 78 w -20 V 79 w -21 v 80 P -7 st 81 P -2 f dynamic stem G (RA31 S 211) on 2284 hP across flow limiter YD 31 P 101 Lift of relief valve dynamic Positioning signal for pilot RV Positioning signal for pilot SV Control pressure RV dynamic Clearing pressure before quencher inlet BM I'II SH ZII SM III SM IZZ SM III SH III (3) KWU-RF-13 Revision No ~. 3 KKP hot test Blowdown tests on relief system Date: 9/1/76 No. Measurement Location of measurement. point transmitter Remarks Measurement group classification Relief s stem H (RA21 S 221 at 132'2 ml 83 W -22 84 W -23 v 85 W -24 V 86 P -8 st hP across flow limiter YD 21 F 101 Liftof relief valve dynamic Positioning signal for pilot RV dynamic Positioning signal for pilot SV dynamic Control pressure for RV dynamic DM III SM III SM III SM III SM III KWU-RF-13 Revision No.: 3 KKP hot test Blowdown tests on relief system Date: 9/1/76 No. Heasurement Location of measurement point transmitter Remarks Measurement gro ~ classification 87 DHS-50 88 DHS-51 89 DMS-52 90 DMS-53 91 DHS-54 92 DMS-55 93 DMS-56 94 DMS-57 95 DMS-58 96 DHS-59 97 DMS-60 98 DHS-61 99 DMS-62 100 DHS-63 At spherical shell, outside + 10.45 / 260D At spherical shell, outside + 10.45 / 260
- ) At spherical shell, inside
+ 10.45 / 260 <<) At spherical shell, inside + 10.45 / 260O At, spherical shell in region of T-joint / 260', outside At spherical shell in region of T-joint / 260', outside At spherical shell in region of T-joint / 260', inside At spherical shell in region of T-joint / 260', inside In region of T-joint, inside / 260'n region of T-joint, inside / 2604 Runout of the weld of the connection to the conical bottom / 260 At inner cylinder, inside / 260 ) At inner cylinder, inside / 260'j SM I;IY SM I SM I IY SM I SN I SM I SM I SH I SH I SM I SN I SN I SM I (3) SM I (U) (H) (H) (U) (N) (v) (H) (U) (M) (U) (H) (U) (H) NOTES:
- ) Measurement point redundant
k KWU-RF-13 KKP hot test Revision No.c 3 Blmrdmm tests on relief system Date: 9/1/76 NO. Measurement Location of measurement Remarks Measurement group point transmitter classification 101 DMS-64 102 DMS-65 103 DMS-66 104 DMS-67 105 DMS 68 106 DHS-69 "107 DMS-70 108 DHS-71 109 DMS-72 110 DMS-73 <<) At inner cylinder, inside, +12.78 / 260<<
- ) At inner cylinder, inside,
+12 78 / 260O <<) At inner cylinder, outside/ + 12.78 / 260o <<) At inner cylinder, outside, +12.78 / 260o
- ) Strut 1, system P to the inner cylinder, top /
260') Strut 1, system F to the inner cylinder, bottom / 260') Strut 2, system F to the inner cylinder, top / 260') Strut 2, system F to the inner cylinder, bottom / 260'n reinforcement rib under conical bottom / 260<< On reinfrocement rib under conical bottom / 2604 SH I SM I SM I SM I Strut forces SH II Strut forces SH II Strut forces SM II Strut forces SH II SH II SH II (U) (H) (U) (M) 111 DMS-74 112 DHS-75 113 DNS-76 114 DMS-77 115 DMS-78 L16 DNS-79 '17 DMS-80 118 DMS-81 Bottom mount (torsion guard) / 260 Torsion SH ll
- )
Measurement point redundant KWU-RF-13 Revision No.: 3 KKP hot test Blovdmm tests on relief system Date: 9/1/76 No. Measurement Location of measurement point transmitter Remarks .Heasurement group classification 119 DHS-82 120 DMS-83 121 DMS-84 122 DMS-85 123 DMS-86 124 DHS-87 125 DMS-88 126 DMS-89 127 DMS-90 128 DMS-91 129 DMS-92 130 DMS-93 131 DHS-94 132 DHS-95 133 DHS-96 134 DMS-97 135 DHS-98 NOTES:
- )
e) Support 2&5' 8.9 m 4) + 4} IS ~I 1) s w At spherical shell, inside, 108~/+10~45 At spherical shell, inside, 108~/+10 '5 At spherical shell, outsidei 10&~/+10.45 At spherical shell, outside, 108~/+1.0 '5 At spherical shell, inside/ 228~/+10.45 At spherical shell, inside, 228'/+10.45 At spherical shell, outside, 228 /+10.45 At spherical shell, outside, 228 /+10.45 At spherical shell, inside, 1450/+10.45 At spherical shell, outside, 145~/+10 45 Lining 1084 +10.451 Lining 228'10.451 Lining 260'10.451 Measurement point redundant (3) SM I (3) SM I (3) SM I (3} SM I SM IV SM IV SM IV SM IV SH IV SM IV SH IV SH IV SM TV SH V SH V SH V (V) (V) (V) (V) (U) (H) (U) (H) (U) (H) (U) (H) (U) (U) (H) (M) (M) RWu-RF-13 KKP hot test Blowdown teste on relief system Revision No. s 3 Date: 9/1/76 No. Measurement Location of measurement point transmitter Remarks Measurement group classification 136 WA-ll 137 WA-12 138 WA-13 139 WA-14 140 WA-15 141 WA-16 142 WA-17 .143 WA-18 144 WA-19 145 WA-20 146 WA-21 147 WA-22 148 WA-23 Belch bottom mount Spherical shell, outside/ +10 45 / 260~ Bearing shoe. inner cylinder as low as possible Inner cylinder, 1084 +12.78 Below conical bottom, 108'uter shell, 108'10.45 Outer shell, 145', +10.45 Inner cylinder, 228', +12.78 Below conical bottom, 228'uter .shell, 228', +10.45 Inner cylinder, 260', +12.78 Relative motion SM IlgIV of th<<onical SM II IU bottom relative to concrete Motion of spherical shell SM I>IV Relative motion,SH I horizontalvertical SM IV SM IV SH IV SH IV SM IV. SM IV SH IV SM IV (3) 149 WA-40 150 WA-41 151 WA-42 Pole - pressure suppression
- system, x direction Pole pressure suppression
- system, y direction Pole
- pressure suppression
l K ~ ~l ~ ~ ~ ~ ~ ~ ~ KWU-RP-13 Revision No.c 3 KKP hot test Blowdcnrn tests on relief system= Date-9/1/76 No. Heasurement Location of measurement point transmitter Remarks Measurement group classification 152 DA-1 153 DA-2 154 DA-3 155 DA-4 156 DA-5 157 DA-6 158 DA-7 159 DA-8 160 DA-9 161 DA-10 162 DA-ll 163 DA-12 164,DA-13 Conical bottom, meridian 228'uter shell, meridian 2284 + 10.45 Outer shell 2440 +15.05 Outer shell-244 +10.45 Conical bottom 2444 Inner cylinder 244 +14.50 Outer shell 2600 +15.04 Outer shall 250i +10.45'uter shell 2604 Conical bottom 2600 Inner cylinder 260 i+11. 9 Inner cylinder 260 +14.50 Conical bottom 2840 Reference mea-surement for DHS 82-85 SM I IV SH I IV SM I SM I SH I SM I SM I SM ZgIV SM I SM I ~II~III/IV SM I SH IgIV (3) (3) (3) 165 DA-14 166 DA-15 167 DA-16 168 DA-17 169 DA-18 Inner cylinder Outer shell Conical bottom Outer shell Inner cylinder 108 /12.78 108 /10/45 108'45 /+10.45 2280/+12.78 SM IV SM IV SM IV SM IV SM IV S ~ ~ ~ KWU-RF-13 Revision No. c 3 KKP hot test Blcnrdown tests on relief system Date: 9/1/76 No. Measurement Location of measurement point transmitter Remarks Measurement group classification 170 T-24 171 T-2 172 T-22 173 T-29 174 T-1 175 T-21 176 T-28 177 T-26 178 T-27 179 T-25 180 T-3 181 T-23 182 PRDB Temp. lance 68 + 68 + 68 + 68 + 188 + 188 + 188 + 188 + 308 + 308 + 14.0 ll.3 15 ~ 8 14 ' 14 0 11.3
- 15. 8 14.0 308 + 14 '
308 + 11.3 Reactor pressure From operating instrumentation 1000 m BM BM BM BM 183 Ei Excitation impulse and internal reference signal and synchronizing signal (10 Nz) coupled S l l Rl KWV-RF-13 Revision No.t 3 'KKP hot test Blnrdcwn tests on relief system Date: 9/1/76 No. Heasurement Location of measurement point transmitter Remarks Heasurement group classification 184 Pd-6 185 DHS-99 186 -100 187 -101 Pressure before orifice at quencher G 'at 2284 Lining, outside, 108 /+10.45 228o/+10.45 2604/+10 '5 static SH III SH V SH V SH V (3) (U) (3) (0) (3) (V) (3) '1 I ki ~ 5 KRAFTWERK UNION AG PROPRIETARY INFORMATION APPENDIX.. 17-47 17-50 I