ML23317A170
ML23317A170 | |
Person / Time | |
---|---|
Site: | Seabrook |
Issue date: | 11/03/2023 |
From: | NextEra Energy Seabrook |
To: | Office of Nuclear Reactor Regulation |
Shared Package | |
ML23317A044 | List:
|
References | |
L-2023-152 | |
Download: ML23317A170 (1) | |
Text
SB 1 & 2 Amendment 52 FSAR December 1983
APPENDIX C
LOAD CELL CALIBRATION AND ORIGINAL DATA
3G-29 SB 1 & 2 Amendment 52 FSAR December 1983
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N SB 1 & 2 Amendment 52 FSAR December 1983
CONTAINMENT LINER ANCHOR LOAD TEST FABRICATION OF SPECIMENS SEABROOK PROJECT
Date: April 7, 1981
Prepared by:lt~l~
B. Galunic
3G-52 SB 1 & 2 Amendment 52 FSAR December 1983
Containment Liner Anchor Load Test Fabrication of Specimens Seabrook Project
- 1. INTRODUCTION
The containment structure at the Seabrook Nuclear Project is a right
vertical cylinder having an inside radius of 140 feet and wall thickness
of 4'-6", and it has a hemispherical dome which is 3'-6" thick. At the base
is a 10 foot thick mat. It is designed to resist the pressure from the most
severe break in a reactor coolant pipe. In order to meet the leak tightness
requirements of the vessel, a steel liner plate is installed over the inside
surface of the concrete. The liner is generally 3/8 inch thick in the cyl-
indrical portion and is thickened to 3/4 inches in the penetration areas near
the base. The liner in the dome has a uniform thickness of 1/2 inch and it
is 1/4 inch thick on top of the mat. It is anchored to the concrete shell by
embedded structural tees and studs welded to the liner plate. Headed studs
are only used on the 3/4 inch plates in the penetration area. The tees are
used in all other regions.
The purpose of these tests is to define a load-deflection curve for the
anchors which can be used in the analysis of the liner/anchor system. The
liner strains and anchor displacements must meet the requirements of the ASME
Section III Division 2 Code.
- 2. MATERIALS
2.1 Tees
The tees are made from SA36 steel. They were rolled in Japan and accord-
ingly have metric dimensions. The tee WT 100x100 corresponds very closely
3G-53 SB 1 & 2 Amendment 52 FSAR December 1983
with the American W~ 4x7.5 (3.94 in. VS 4.0 in. flange Width).
2.2 Studs The stud material conforms to ASTM Specification A-108 Grade 1018. The
yield stress is approximately 50 ksi and the ultimate strength is approximately
60 ksi.
2.3 Liner Plate The liner plate is made from SA 516 Grade 60 steel (Specification 9763.
006 15-1). The plate was cut so that the tensile load on the plate during
the test is applied in the direction of rolling. The plate thickness used for
all tests, including the studs, was 3/8 inch. In the containment structure
the studs are welded to a 3/4 inch plate. It is expected that the thinner
plate used in the test will permit larger rotations of the anchor in the
vicinity of the plate causing larger stresses in the concrete and thereby
conservative results.
2.4 Concrete All concrete was mixed in accordance with PSNH Specification 9763.006
~9-7 and 9763-69-3. The design strength vas 4000 psi. The concrete mix is
the same as used in the containment structure. An air-entraining and retard-ing admixture was used. The concrete was Atlantic Type II and the coarse ag~
gregate conforms to ASTM C-67.
2.5 Reinforcement The concrete is reinforced with rebar that conforms to ASTM A615 Grade
60 Specifications.
3G-54 SB FSAR 1 & 2 Amendment 52 December 1983
- 3. DESIGN OF SPECIMENS
The dimensions of the specimens, the reinforcement and pertinent details
are shown in the drawing LT-1. The overall size of the specimens and the
length and taper of the liner were based on the dimensional limitations of the
testing equipment. The reinforcement served two purposes. It first provided
a confinement of the concrete and prevented cracking that could occur during
transportation and other handling. Also, additional rebar were placed on the
side of the tees away from the load application. The purpose of these bars
was to prevent overall cracking of the specimen when the test load is applied.
They are intended to eliminate failure modes that might occur due to the phy-
sica! limitations of the test specimen. Any cracking of the free vertical
surfaces would not be representative of what could occur in the actual struc-
ture which is continuous. The length of the tee specimens was held to 12 in-
ches, to minimize the effect of the free edge.
These problems are not expected to occur when studs are used because the
failure will be localized to a small area. The same overall dimensions were
used for simplicity of fabrication.
- 4. POURING PROCEDURE
The test block forms were fabricated at the Seabrook site. The liner
formed one side of the form as is the case in the containment structure. The
tees were oriented vertically during the pouring operation. Before the con-
crete was poured a thin coating of WD-40 was sprayed on the liner to eliminate
bond between the liner and concrete. Concre~e was mixed at the Site Batch
Plant and brought to the test area by trucks. The concrete was placed into
the forms by a pump truck to simulate actual field placement conditions.
3G-55 SB 1 & 2 December 1983 Amendment 52 FSAR
Each specimen was fabricated in three lifts. After each lift a vibrator
was used to consolidate the concrete and eliminate voids. Two different
trucks were used. Twelve cylinders were taken from each truck. In addition,
six cylinders were made for each specimen. These were stored on site in a
controlled environment curing room. Three were broken on the day of the test
of the specimen. At the end of the pour the top of the concrete surface was troweled to a smooth finish. A chemical curing compound was applied to
the exposed surface to seal in moisture and thereby replace water curing.
5* TRANSPORTATION
The specimens were transported to Knoxville, Tennessee on two flatbed
trucks 14 days after fabrication. Five day cylinder breaks indicated a strength
of 3550 psi.
3G-56 SB FSAR 1 & 2 Amendment 52 December 1983
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- 2'-q'4 SECTION &* f, ENGINEER DATE
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l 1'-~11 PIPE W/CAPPED ENOS FOill1fTIN4 ~ro r ( tfll) 'l' - 5~ I, t'*'!> J r I liN[R ANC~QB SECTION AA ~{Dill_ TEST SPECIMENS
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~0 5180 fiRST ISSUE 6u a:z DATE DESCRIPTION ENGR SUP [1\\jG I L i-I SB 1 & 2 Amendment 52 FSAR December 1983
Plate 1: Close-up of tee welded to liner plate
Plate 2: Reinforcing cage and tee
3G-59 SB 1 & 2 Amendment 52 FSAR December 1983
Plate 3: Finished specimens at end of pouring operation
3G-60 SEABROOK DESIGN OF STRUCTURES, COMPONENTS EQUIPMENT AND Revision 8 STATION SYSTEMS Appendix 3H UFSAR Deleted in Amendment 53 Page 3H-1
APPENDIX 3H (DELETED IN AMENDMENT 53)