ML20234E924
| ML20234E924 | |
| Person / Time | |
|---|---|
| Site: | Vermont Yankee File:NorthStar Vermont Yankee icon.png |
| Issue date: | 01/04/1988 |
| From: | Capstick R VERMONT YANKEE NUCLEAR POWER CORP. |
| To: | Russell W NRC OFFICE OF INSPECTION & ENFORCEMENT (IE REGION I) |
| References | |
| FVY-1-88, NUDOCS 8801110248 | |
| Download: ML20234E924 (14) | |
Text
STARTUP TEST REPORT VERMONT YANKEE CYCLE 13
==
Introduction:==
1 Vermont Yankee Cycle 13 initial startup commenced on October 1, 1987 following a 7 1/2 week outage for annual refueling, maintenance related activities and fuel sipping.
The core loading for Cycle 13 consisted of:
8 P8x8R P8DPB289 Reinserts from Cycle 10 104 P8x8R P8DPB289 Reinserts from Cycle 11.
120 P8x8R P8DPB289 Reinserts from Cycle 12 136 P8x8R BP8DRB299 non irradiated assemblies An as loaded Cycle 13 core map is included as Figure I. Details of the Cycle 13 core loading are contained in the Yankee Atomic Electric Company document YAEC-1600, " Vermont Yankee Cycle 13 Core Performance Analysis, May, 1987".
An in-sequence critical was performed satisfactorily on Aug. 27,1987.
The shutdown margin was verified to be satisfactory based on the data' collected i
from the in-sequence critical. Startup commenced October 1,1987 and steady j
state full power conditions were reached October 20,1987.
Control rod coupling verification was performed satisfactorily for all 89 control rods on Aug. 26 and 27, 1987. Control rod scram testing was per-3 formed satisfactorily prior to reaching 30% power per Tech. Specs. for all 89 control rods on Sept. 24 and Oct. 3,1987.
The final as loaded core loading was verified correct by vermont Yankee and Yankee Atomic Electric personnel on Aug. 25,1987.
Core Verification:
The final core loading was verified correct on Aug. 25,1987. Three separate criteria were checked:
- 1. Proper bundle orientation was verified by checking channel fastenor orientation and assuring that fastener orientation agreed with that shown in Figure II.
2.
Proper bundle seating was verified by following Vermont Yankee Procedure VYOP 1411.
- 3. Proper core loading was verified by checking the serial number of each bundle through the use of a video camera. This verification was recorded on video tape and was later independently reviewed and reverified to agree with the licensed core loading of Figure I.
11 2
BB e
5t
- \\
Process Computer Data Checks:
j Process computer data shuffling checks were completed Sept. 27,1987.
1 These checks included various manual and computer checks of the new data constants. A check for consistency of the data was also performed by Yankee
)
Atomic Electric Company and found to be satisfactory.
)
In-Sequence Critical:
Sequence 13-A-2 was used to perform the in-sequence critical test.
1 On Aug. 27, 1987 control rods were withdrawn in-sequence until criticality was attained. Criticality was achieved on the 5th rod in group 2 (34-23) at notch position 12. The moderator temperature was 86.8 F.
The actual critical rod pattern and the YAEC prediction agreed within
)
+/- 1% 6K/K. Figure III shows the actual, predicted and the +/- 1% 6K/K critical rod patterns.
Shutdown Margin Testing The shutdown margin calculation was performed using data collected during the in-sequence critical and information provided in the Core Management Report. The required shutdown margin to be demonstrated was 0.32 %AK/K. The actual shutdown margin was shown to be 1.253% A K/K.
Rod Scram Testing:
All 89 control rods were scram tested satisfactorily on Sept. 24 and Oct.3,1987. All insertion times were within the limits defined in the Vermont Yankee Technical Specifications. Results of the testing are presented in Table IA.
In accordance with Technical Specifications Section 4.3.C.2, scram time information available for scrams occurring since the transmittal of the previous startup test report is also included in Table IB. All insertion times were within the limits defined in the Vermont Yankee Technical Specifications.
All scram time information was evaluated to ensure that proper drive performance is being maintained. No degradation of drive performance is noticeable.
Thermal Hydraulic Limits and Power Distribution:
Core Maximum Fraction of Critical Power (CMFCP), Core Maximum Fraction of Limiting Power Density (CMFLPD), Maximum Average Planar Linear Heat Generation Rate ratio to its limit (MAPRAT) and the ratio of CMFLPD to the Fraction of Rated Power (CMFLPD/FRP) were all checked daily during the startup using the process computer. All checks of core thermal limits were within the limits specified in Technical Specifications.
i The results of the Backup Core Limits Evaluation (BUCLE) program were compared to results of the process computer for the same core conditions.
The results were identical as can be seen in Table II.
The process computer power distribution was updated twenty (20) times using the TIP system during the ascent to full power. The results of these updates are presented in Table III.
The LPRMs were calibrated once in conjunction with TIP set 1085. The initial checkout of LPRM high and low trip alarm setpoints was done at 0%
power on Sept. 21,1987. The TIPS and the LPRMs were both functionally tested and found to operate satisfactorily.
The process computer power distribution update was performed on Oct.21,1987. TIP 1103 was used as a basis for comparison with an offline calculation performed using the Yankee Atomic Electric Company nodal code SIMULATE. For the power distribution of Oct. 21,1987 the SIMULATE core average axial power distribution was compared to that calculated by the plant process computer; comparisons are shown in Table IV. A comparison was also performed between SIMULATE and the process computer peak radial power; comparisons are shown in Table V.
TIP Reproducibility and TIP Symmetry:
TIP system reproducibility was checked in conjunction with the power distribution update performed on Oct. 7,1987. All three TIP system traces were reproducible to within 4.3%.
The A-2 sequence used as the initial control rod sequence varied slightly from an eignth core symmetric pattern with octant symmetric rod locations at notch 46 and 48. Due to this lack of eighth core symmetry, calculation of a total TIP certainty was performed using synthetic traces from a SIMULATE case at the same conditions as calibration 1103, but with the control rod at core location 22-35 set to position 48. These synthetic traces were pointwise adjusted by SIMULATE using the ratio of the actual TIP 1103 traces to the synthetic SIMULATE TIP 1103 traces. By using the pointwise adjustment ratics it is possible to estimate what the actual TIP traces would be for a symmetric rod pattern.
The resulting total TIP uncertainty for this case was 1.52 percent.
The results of the TIP uncertainty test as shown in Table VI are well below the 8.7% acceptance criteria.
Figure 1 Cycle 13 Cora Map VERMONT YANKEE
~
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01 03 05 07 09 11 13 15 17 19 21 23 25 27 29 31 33 35 37 39 41 43 g LPRM LOCATION (COWtON LOCATION FOR ALL TYP MACHINES) 43 Q LPRM LOCATION (LETTElt INDICATES 39 TIP MACHINE)
$ IRM LOCATION 31 A sam NOR 27 23 19 15 11 7
3 2 6 10 14 18 22 26 30 14 u 4,
FIGURE II CORE CELL LOADING. CONFIGURA TION r
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CRITICAL ION C W ARISCN BEGINNING OF CYCLE 13 43 k8 39 kb h8 h8 3$
h8 31 kS k$
27 49 48 48 48 48 23 19
/0 15 k8 h8 11 k8 07 3b k8 k8 k8 l
03
-12 MA Predicted Critical Pattern 02 06 10 1c 18 22 26 30 34 38 42 02 06 10 14 18 22 26 30 34 38 42 43 48 h8 48 48 39 48 48 k8 48 35 h8 k2 kb
__h h k8 31 27 42 48 48 48 42 48 23 48 48 48 12.
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1 1
I A
TABLE IA CONTROL ROD SCRAM TESTING RESULTS VERMONT YANKEE BEGINNING OF CYCLE 13 1
i
- Scram #132' September 25,1987 j
i
- Mean Time;for % Insertion 4.51%
25.34%
46.18%
87 84%
Measured time-(sec)-
0.339 0.879 1.431 2.591 Tech. Spec.1 Limit (sec) 0.358 0.912 1.468 2.686 Maximum 87.84% insertion time (sec) 2.879
=
Tech. Spec. limit.for slowest 87.84% insertion time (sec) = 7.000
- Slowest 2x2 Array for % Insertion 4.51%
25.'_34%
46.18%
87.84%
Measured time (sec) 0.362 0.929
'1.519 2.710 Tech. Spec. Limit ~(sec) 0.379 0.967 1.556 2.848 Includes scram times collected during single lod scram testing for all control-rod' drives except 06-35. The time for 06-35 was obtained during full scram #133.
1 l
l 1
1_______________________________________n____________________.
____________._._____________________._____m___u._2._a
TABLE IB CONTROL ROD SCRAM TESTING RESULTS VERMONT YANKEE CYCLE 12-Scram #129 (Full Scram)
October 4,1986 Mean Time for % Insertion 4.51%
25.34%
46.18%
87.84%
Measured time (sec) 0.317 0.829 1.391 2.563 Tech. Spec. Limit (sec) 0.358 0.912 1.468 2.686 2.872 Maximum 87.84% insertion time (sec)
=
Tech. Spec. limit for clowest 87.84% insertion time (sec) = 7.000 Slowest 2x2 Array for % Insertion 4.51%
25.34%
46.18%
87.84%
Measured time (sec) 0.326 0.856 1.454 2.688 Toch. Spec. Limit (sec) 0.379 0.967 1.556 2.848 Scram #130 (Single rod scrams at power)
May 9,1987 Mean Time for % Insertion 4.51%
25.34%
46.18%
87.84%
Measured time (sec) 0.309 0.822 1.383 2.563 Tech. Spec. Limit (sec) 0.358 0.912 1.468 2.686 Maximum 87.84% insertion time (soc) 2.944
=
Tech. Spec. limit for slowest 87.84% insertion time (sec) = 7.000 Slowest 2x2 Array for % Insertion 4.51%
25.34%
46.18%
87.84%
l Measured time (sec) 0.322 0.862 1.454 2.688 Tech. Spec. Limit (sec) 0.379 0.967 1.556 2.848 Scram #131 (Full Scram)
August 7, 1987 Mean Time for % Insertion 4.51%
25.34%
46.18%
87.84%
l Measured time (sec) 0.279 0.782 1.296 2.399 Tech. Spec. Limit (sec) 0.358 0.912 1.468 2.686 Maximum 87.84% insertion time (sec) 3.012
=
Tech. Spec. limit for slowest 87.84% insertion time (sec) = 7.000 Slowest 2x2 Array for % Insertion 4.51%
25.34%
46.18%
87.84%
Measured time (sec) 0.308 0.833 1.370 2.530 Tech. Spec. Limit (sec) 0.379 0.967 1.556 2.848 j
l
TABLE II Comparison of BUCLE and' Process Computer Thermal Limits Calculation Parameter BUCLE Process Computer CMFCP*
0.352 0.352 Location 25-26 25-26 CMFLPD*
0.269 0.269 Location 25-26-20 25-26-20 MAPRAT*
0.252 0.252 Location 25-26-20 25-26-20
- Tech. Spec. Limit - 1.000 1
l
TABLE III Power Distribution Measurements - Cycle 13 Start-Up October 1,1987 _ October 21,1987 l
Date Power %
Core Flow %
CMFLPD*
CMFCP*
MAPRAT*
1987 10/4 17.92
'48.21 0.269 0.352 0.252 10/5 23.45 31.88 0.259
'0.411 0.248 10/5 23.49 31.75 0.259 0.408 0.247 10/6 34.34 32.75 0.361 0.554 0.360 10/7 54.51 48.00 0.579 0.675 0.560 10/7 59.37 46.83 0.608 0.761~
0.614 10/7 59.06 46.73 0.557 0.749 0.559 10/7 63.53 46.65 0.578 0.855 0.579 10/8
'78.83 66.58-0.710 0.864 0.713 10/9 87.13 84.40 0.767 0.852 0.773 10/9 45.57 34.35 0.461 0.805 0'.463 10/9 48.78 30.56 0.526 0.906 0.519 10/10 65.35 41.81 0.679 0.999 0.681 10/10 71.13 47.15 0.721 0.995 0.724 10/13 98.53 97.46 0.901 0.917 0.902 10/14 97.75 97.31 0.898 0.907 0.898 10/16 97.40 99.33 0.895
-0.898 0.896
(
10/17 49.19 36.10 0.505 0.781 0.511 10/17 69.96 60.44 0.643 0.809 0.651 10/21 99.91 99.08 0.871 0.918 0.882 I
- Tech. Spec. Limit = 1.000 I
i 1
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Q.--_--_._____-.___._____._.-__--_____.__-.-_-___....-.___._----_._-_-_---_-______1-_
a
---.._____J
b Table IV Comparison of Direct-From-Traces and-SIMULATE Core Average Axial Distributions PROCESS SIMULATE NODE COMPUTER PARTB 24
.3978
.2729 23
.5710
.4582 22
.7089
.6185 21
.7994
.7507 20
.8937
.8563 19
.9797
.9382 18 1.0123
.9994 17 1.0249 1.0413 16 1.0760 1.0638 15 1.0645 1.0625 14 1.0404 1.0724 13 1.0833 1.0938 12 1.1253 1.1237 11 1.1350 1.1598 10 1.1647 1.2002 9
1.2304 1.2407 8
1.2587 1.2748 7
1.2302 1.2892 6
1.2714 1.3103 5
1.2832 1.3212 4
1.2222 1.2879 3
1.0868 1.1733 2
.8479
.9560 1
.4925
.4351
l TABLE V' Comparison of 10 Highest Relative Radial Powers
- Location' SIMULATE Plant
_____ 28 1.365 1.380 25-26 1.440 1.498-25-28 1.370 1.293-25-30 1.294 1.376'
~27-24 1.366 1.391 27-26 l'.370 1.299-29-26 1.294' l'.382 29-30 1.209 1.299 33-26 1.244 1.292 35-24 1.272 1.315 l
l l
TABLE VI Total TIP Uncertainty Case Rod Pattern Power (%)
Core Flow (%)
Uncertainty (%)
SYM 1103 18 34 99.91 99.08 1.52 42 18
VI2RMONT YANKEE NUCLEAR POWER CORPORATION RD 5 Box 169, Ferry Road. Brattleboro, VT 05301
,,,L y,g.
ENGINEERING OFFICE f
y January 4, 1988 1671 WORCESTER ROAD -
FR AMINGHAM, MASS ACHUSETTS 01701 pyy y_gg TELEPHONE 617-872-6100 l
United States Nuclear Regulatory Commission Region I 631 Park Avenue King of Prussia, PA 19406 Attention:
Mr. William T. Russell Regional Administrator
References:
(a) License No. DPR-28 (Docket No. 50-271)
(b) Vermont Yankee Technical Specification, Section 6.7.A.1
Subject:
Cycle 13 Start-Up Test Report
Dear Sir:
Enclosed please find the Cycle 13 Start-Up Test Report for Vermont Yankee which is submitted to you in accordance with the requirements of Reference (b).
We trust that you will find this information satisfactory; however, should you desire additional information, please contact us.
Very truly yours, VERMONT YANKEE NUCLEAR POWER CORPORATION Robert W. Ca stick Licensing Engineer RWC/16.265 Enclosure cc:
U.S. Nuclear Regulatory Commission Document Control Desk Washington, DC 20555 NRC Resident Inspector di
__