Text

Reactor Bldg Liner Plate Anchorage Tests for AR Nuclear 1, App A.Prepared for Bechtel Corp for Transmittal to Util
	ML19326D073
Person / Time
Site:	Arkansas Nuclear
Issue date:	03/03/1969
From:	Foreman E; AFFILIATION NOT ASSIGNED
To:	;
Shared Package
ML19326D072	List: ML19326D071; ML19326D073; ML19326D074; ML19326D075;
References
	6600-C-35-AC, NUDOCS 8006030631
	Download: ML19326D073 (23)
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APPENDIX A PREPARED BY ANAMET LABORATORIES, ,INC. j 2827 SEVENTH STREET I BERKELEY 10, CALIFORNIA 1

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LABORATORY C20T!71CATE i Anamet Laboratocies, Inc. 33.Im 3827 SEVENTH STREET . 3FRMELEY 10. CALJFORNIA. . THommwAu.15778 mow TrursaArums APPWRO AS$4ANCM April 11, 1969 " " ""*

LABORATORY NUMBER: 469.146 P.O. No. 6600-C-35-AC Job No. 6600 SAMPLE: Testing of the Reactor Building Liner Plate Anchorage Test Specimens DATE SUBMITTED: March 3, 1969 REPORT TO: Bechtel Corporation 301 Mission Street San Francisco, California Attn: Mr. Ted Johnson aEPQRT 7- The following report is a summary of the test preparation and Y data on eight (8) liner plate anchor specimens prepared and tested by our laboratory for Bechtel Corporation on Purchase Order 660-C-35-AC. .

The eight (8) test specimens, identified I through VIII, were prepared in accordance with the purchase order. All eight (8) were compression specimens. Seven (7) were tested on 4/4/69 (16 days after casting) and one (1) specimen, No. V, is to be tested on 9/15/69. The tests on 4/4/69 were witnessed by Ted Johnson of Bechtel Corporation. These tests were performed in l a 120,000 lb. Tinius Olson Hydraulic Testing Machine. A summary of the test specimens, test data, welded sample type, j weld and angle leg directions is given in the attached data.

The test plates used to make the specimens were hot rolled A 36 material 1/4" thick. The material is certified by vaseph T. Ryerson & Sons Inc. to meet the chemical and mechanical requirements of ASTM A 36 material. Tensile tests were per-

s. formed by our laboratory on the plate material - two (2) in I

LASONATORY CERTFICATE Anamet Laboratories, Inc. Lab. No: 469.146

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the longitudinal direction and two (2) in the transverse di-rection. This test data is attached.

The angles were fillet welded onto the plates by Advanced Heli l Welders in accordance with AWS D 1.0-63. The welding rod used l was E6010 celluloce electrode. The weld and angle positions l is included in the appendix.

On March 19, 1969 the eight (8) liner plates were cast in con-crete blocks. At the same time, eight (8) concrete test cylinders were als'o prepared. The cement was Portland Cement, Type II, per ASTM C 150 and only one brand, Calaveras, was !

used. The aggregates used conformed to ASTM C-33 and were manufactured from calcite limestone by Kaiser Sand and Gravel.

The fine and coarse aggregates were graded in accordance with the purchase order as follows:

Type of Gradation i Sieve Size Percentage Passing -

U.S. Std. Fine Aggregate Coarse Aggregate Sq. Mesh (Sand) 3/4 in. 1 1/2 in.

2 inch 100 1 1/2 inch 90-100 1 inch 100 20- 55 3/4 inch 90-100 0- 15 3/8 inch 100 20- 55 0- 5

4 95-100 0- 10

8 80-100 0- 5

16 50- 85

30 25- 60

50 10- 30

100 2- 10 The admixtures used were "Darex" per ASTM C-260 and Type A Pozzolith #8 from Master Builders Company.

The following concrete mix was made:

l LABORATORY CERTFICATE Anamet Laboratories, Inc. ,

Lab. No: 469.146 l

l r sv syswrw ernaar . eiusury io.muroam Cement '588f Calaveras Cement Type II Sand 1217f (8' moisture allowance) 3/4" Calcite Limestone 944# Kaiser's Calcite 1 1/2" Calcite Limestone 974f Kaiser's Calcite Water 30 Gallons Pozzolith #8 If-3 oz.

Darex 3 3/4 oz.

Concrete slump 2 1/4 ,

Air entrainment 1 1/2%

Eight (8) test specimens containirig liner plate anchorage specimens were filled and vibrated to the satisfaction of the representatives of the Bechtel Corporation present.

~The exposed concrete surface was coated with Grace Con-struction Company's Clean Seal #12 after the initial set of the concrete and covered with burlap.

, Twenty-four (24) hours af ter completing the concrete pour, all test specimens were stripped from the forms and coated all sides with Clean Seal #12.

A seven (7) day compression test was performed on two (2) of the test cylinders. The cylinders were capped and load de-flection measurements were made at 500 psi, no load, 500 psi, 1,000 psi. 2,000 psi, 3,000 psi and 4,000 psi. Two (2) cylinders were again tested after sixt:en (16) days. Of the remaining four (4) cylinders, two (2) are to be tested after twenty-eight (28) days and two (2) after one hundred and eighty (180) days. The load-deflection data from the' testec -i linders is given in the attached data.

The compression tests on the liner plate test blocks were per-

! formed with load deflection measurements being made at 5,000 lbs., 10,000 lbs., 15,000 lbs., 20,000 lbs. and in 10,000 lbs. ;

increments to test completion. Additional measurements were l

. also made at specified loads ,or deflections after yielding oc-curred.

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w,ensisa de J ee ----o4.-4*--,e--iw 3 e-ew - we,,- ,w, -ws L.A50RATORY CERTIFICATE 3 /unanact laboratories, Inc. Lab. No: 469.146 saar uvem erneur . naxaay io.cuuouw The deflection readings were made on eight (8) dial indi-cators. The upper three (3) dials were designated 1, 2 and 3 from the front to the back of the machine. The lower dials were designated 4, 5, 6, 7 and 8 again from the front to the back of the machine (see Drawing C199 for the actual lo-cations). The upper dials 1, 2 and 3 were used to preset the compressive load on the concrete test block in addition to measuring any deflection during the test. 1 1/16" thick asbestos padding was placed beneath and on top of )

the concrete blockr between them and the clamping fixtures. l The loading surfaces were not capped for this series of tests. l They were ground, however, to remove any loose concrete or ridges.

Photographs were taken of Specimen II showing the overall set-up, a close-up of the specimen at 40,000, at yield, and at )

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ultimate. -Photographs were also taken of SpecimenTEE, close-up, at 40,000 lbs. and at yield.

Respectfully submitted, ANAMET LABORATORIES, INC.

By M b b%

Edward A. Foreman Laboratory Supervisor l

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'~'Anamet Laboratories, Inc. Lab. No- 469.146 near esveme ernaar . maamm.sv amm.wona TE*;SILE TESTS 1/4" thick A36 Plate Test per ASTM A 370 Tensile Tests were performed on this plate in both the longitudinal and transverse directions. The test results are as follows:

Di re cti on Longitudinal (1) Longitudinal (2) Recuirements ASTM A 36 Dimensions of Specimen: 0.256 x 0.49E In. 0.256 x 0.498 Inc.

Area: 0.127 Sq. In. 0.127 Sq. In.

Tensile Strength: 68100 Psi 65400 Psi 58/80000 Psi Yield Strength 9 0.2% Offset: 42500 Psi 46100 Psi 36000 Psi Min Elongation in 2" Gage: 31% 32% 23% Min.

Direction Transverse (1) Transverse (2) Reouirements ASTM A 36 Dimensions of Specimen: 0.256 x 0.498 In. 0.256 x 0.498 In.

Area: 0.127 Sq. In. 0.127 Sq. In.

Tensile Strength: 64600 Psi 64600 Psi 58/80000 Psi Yield Strength 9 0.2% Offset: -

42900 Psi 36000 Psi Min Yield Point 46900 Psi -

36000 Psi Min Elongation in 2" Gage: 35% .5% 23% Min.

L.ASORATORY CERTIMCATE

^ A,namet Laboratories, Inc. Lab. No: 469.146 sea, asyswrn ernsse . ennusta ie.uuronnu LINER PLATE ANCHORAGE TESTS Test Test No. Date Weld Angle Type I 16 days 4-12 down Up II II 16 days 4-12 up Up II III 16 days 4-12 down Down II IV 16 days 4-12 up Down II V 130 days 6-12 down Up II VI 16 days 6-12 up Up II VII 16 days 6-12 down Down II

( VIII 16 days 6-12 up Down II NOTE: A restraining block was used on all samples.

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LASORATOMY CERTIFICATE E' Anamet Labore:ories, :nc.

Lab. No: 469.146 asar savam maar . sanna.,r io.caumn:ca CONCRETE CYLINDER TESTS 7 Day Test Date Cast: 3/19/69 Date Tested: 3/26/69 Deflection (inches)

Load No. 1 No. 2 0 Psi 0.000 0.000 500 Psi 0.033 0.0025

( 500 Psi 0 Psi . 0.000 0.004 0.000 0.004 1000 Psi- 0.0055 0.0055

.2000 Psi 0.009 0.010 3000 Psi 0.014 0.0165 4000 Psi - -

Cylinder No. 1 deflected 0.028 inches 9 3979 Psi Cylinder No. 2 deflected 0.030 inches 9 3939 Psi l

Ultimate Compressive Strength 113080 lbs. 1105000 lbs.

Ultimate Compressive Strength 3979 Psi 3909 Psi

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LABORATORY CTJmMCATE

' Anamet I cboratories, Inc. Lab. No: 469.146 sea, e,svanne en.wr . ms- io.curowa CONCRETE CYLINDER TESTS 16 Day Test Date Cast: 3/19/69 Date Tested: 4/4/69 Deflection (incnes)

Load No. 1 No. 2 0 Psi 0.000 0.000 500 Psi 0.003 0.0034

, O Psi 0.000 0.000

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500 Psi 0.0015 0.0015 1000 Psi 0.004 0.004 2000 Psi 0.009 0.009 3000 Psi 0.014 0.013 4000 Psi 0.022 0.021 Ultimate Compressive Strength - 140000 lbs. 145000 lbs.

Ultimate Compressive Strength 4952 Psi 5129 Psi S

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(L Up 4-12 Down)

Load Deflection TT5s) (inches)

Dial 1 2 3 4 5 6 7 8 0 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 5,000 0.0005 0.000 0.000 0.0015 0.009 0.005 0.0065 0.0045 10,000 0.0005 0.0005 0.0005 0.002 0.012 0.007 0.009 0.0053 15,000 0.0005 0.0005 0.0005 0.0025 0.016 0.010 0.011 0.0057 20,000 0.010 0.0005 0.0005 0.003 0.021 0.012 0.013 0.0058

( 30,000 0.010 0.0005 0.0005 0.035 0.029 0.018 0.018 0.0061 40,000 0.010 0.010 0.000 0.0035 0.038 0.027 0.026 0.0064 50,000 0.0005 0.000 0.000 0.002 0.052 0.038 0.037 0.0058 54,000 ,

slight cracking observed 59,200 +0.001 +0 0015+0 002 . . 0.002 0.131 0.100 0.090 -0.005 Weld Failed 9 Approximately 0.300" (No. 6 Dial) and Approximately 42,000 lbs.

Deflection 9 Failure - 5/16"

, Preset on Tie Down Bar - 0.006"

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LABORATORY CEMTFICA72 Anamet I c*ooratories,

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,69.146 LI?:ER PLATE ANCHOR 5;.00X Specimen No: II Date Tested: 4/4/69 Type (L Up II 12 Comp)ression Up -

Load Oeflection TTEs) (inches)

. Dial 1 2 3 4 5 6 7 8 0 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 5,000 ' O.0005 0.0005 0.0005 0.006 0.012 0.010 0.007 0.0042 10,000 0.0005 0.0005 0.0005 0.005 0.014 0.012 0.009 0.0046 15,000 0.0005 0.0005 0.0005 0.008 0.017 0.015 0.011 0.0046 20,000 0.0005 0.0005 0.0005 0.008 0.019 0.017 0.013 0.0046 b 30,000 0.0005 0.0005 0.0005 0.0085 0.025 0.024 0.018 0.0046 40,000 0.000 0.000 0.000 0.0075 0.039 0.034 0.026 0.0046 50,000 -0.015 -0.001 -0.0005 0.0035 0.071 0.058 0.048 0.0022

, 53,200 yield - small cracks 53,400 - - - -

0.200 0.162 0.155 - l 45,000 - - - -

0.300 0.245 0.235 -

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Deflection 9 Failure - 5/8" Preset on Tie Down Bar - 0.006" W

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LI.'ER PLATE Ah*CHOR BLOCX Specimen No: III Date Tested: 4/4/69 Type II - Compression (L Down 4-12 Down)

Load Deflection I'Ios) (inches)

Dial 1 2 3 4 5 6 7 8 0 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 5,000 0.000 0.000 0.000 0.005 0.013 0.013 0.013 0.0095 10,000 -0.0005 0 000 0.000 0.0055 0.016 0.016 0.016 0.011 15,000 -0.001 -0. 005 0.000 0.006 0.018 0.019 0.0195 0.012 20,000 -0.001 -0.0005-0.0005 0.0065 0.020 0.022 0.022 0.0125 k

30,000 -0.001 -0.0005-0.0005 0.008 0.025 0.027 0.029 0.013 40,000 -0.0015-0.0005 0.000 0.00P 0.031 0.034 0.036 0.0133 4

50.000 -0.0015-0.0005 0.000 0.0095'O.038 0.042 0.0465 0.132 60,000* +0.0005+0.0015+0.002 0.010 0.052 0.058 0.077 0.007 70,000 +0.003 +0.004 +0.004 0.0105 0.082 0.086 0.128 0.0033 ;

74,000 yield 1

70,000 - - - -

0.110 -

0.200 -

Deflection 9 Failure - (0.250) 1/4" l Preset on Tie Down Bar - 0.006"

Cracking started.

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Specimen No: IV Date Tested: 4/4/69 Type II - Compression (L Down 4-12 Up)

Load Deflection TTTs) (inches)

Dial 1 2 3 4 5 6 7 8 0 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 5,000 0.000 -0.0005 0.000 0.0025 0.005 0.007 0.007 0.0015 10,000 0.000 -0.0005-0.0005 0.0025 0.007 0.011 0.011 0.0015 15,000 0.000 -0.0005-0.0005 O.003 0.010 0.014 0.013 0.0015 20,000 0.000 -0.001 -0.001 0.003 0.012 0.017 0.017 0.0015

( 30,000 0.000 -0.0005-0.001 0.0035 0.017 0.023 0.023 0.0015 40,000 0.000 0.0005-0.0008 0.0035 0.024 0.030 0.029 0.0015 50,000 0.000 -0.0005-0.0005 0.0035 0.033 0.039 0.037 0.0015 60,000 +0.0005+0.0005+0.0005 0.0035 0.048 0.054 0.051 0.0015 6E,300 ,

cr4cks observed 70,000 .+0.0025+0.0025+0.003 0.0035 0.080 0.090 0.085 0.0015 71,600 yield 60,000 weld failure Deflection 9 Failure - 1/8" Preset on Tie Down Bar - 0.006" e

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Lord Deflection (los) (incnes)

Dial i 2 3 4 5 6 7 8 0 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 5,000 0.000 -0.0005 0.000 0.001 0.004 0.004 0.005 0.0042 10,000 0.000 -0.001 -0.001 0.001 0.006 0.007 0.010 0.0062 15,000 0.000 -0.001 -0.0015 0.001 0.009 0 . 0 ~. 0 0.014 0.0094 20,000 0.000 -0.0015-0.0025 0.0008 0.012 0.014 0.019 0.0114 30,000 0.000 -0.002 -0.0035 0.0005 0.016 0.024 0.031 0.0136 40,000* +0.005 -0.005 -0.0015 0.001 0.028 0.041 0.050 0.014 50,000 +0.001 $0.005 0.000 0.002 0.046 0.058 0.068 0.0184 53,600 yield 50,000 +0.003 +0.003 +0.0025 0.004 0.135 0.149 0.162 0.0204 51,000 +0.004 +0.0045+0.0035 0.008 0.180 0.200 0.220 -

53,000 - - - -

0.275 0.300 0.350 -

48,000 - - - -

0.385 0.400 - -

l Preset on Tie Down Bar - 0.006"

Cracking observed.

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Specimen No: VII Date Tested: 4/4/69 Type II - Compression (L Down 6-12 Down)

Load Deflection (lbs) (inches)

Dial 1 2 3 4 5 6 7 8 0 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

- 5,000 0.000 0.000 0.0005 0.0035 0.007 0.008 0.007 0.0053 10,000 0.000 -0.0005-0.001 0.0035 0.009 0.011 0.011 0.0072 15,000 0.000 -0.001 -0.001 0.003 0.012 0.015 0.015 0.0096 20,000 0.000 -0.001 -0.002 0.0028 0.014 0.018 0.019 0.0115 g 30,000 0.000 -0.0015-0.0025 0.0025 0.019 0.024 0.026 0.0136 k

40,000 0.000 -0.0015-0.0025 0.0025 0.025 0.029 0.032 0.0163 50,000 +0.0005-0.0015-0.0025 0.0025 0.030 0.036 0.039 0.0177 60,000 +0.0005-0.001 -0.002 0.003 0.038 0.044 0.047 0.0175 70,000 +0.002 +0.001 0.000 0.0055 0.050 0.058 0.060 0.0138 74600* +0.0035+0.002 +0.001 0.008 0.058 0.065 0.065 0.012 The test was discontinued due to the plate bending Preset on Tie Down Bar - 0.006"

Cracking observed.

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Loaa Deflection (ios) (incnes)

Dial 1 2 3 4 5 6 7 8 0 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 5,000 0.000 0.000 0.000 0.0035 0.007 0.006 0.010 0.003 10,000 0.001 0.0005 0.0005 0.0055 0.011 0.009 0.016 0.0037 15,000 0.0015 0.001 0.0005 0.0055 0.016 0.012 0.022 0.0039 20,000 0.0015 0.001 0.0005 0.0055 0.021 0.016 0.029 0.0039 f.

\ 30,000 0.002 0.0015 0.0005 0.006 0.028 0.021 0.043 0.0034 40,000 0.002 0.0015 0.0005 0.005 0.036 0.028 0.080 0.0037 46,000 slight cracking 50,000 0.002 0.001 0.0005 0.006 0.044 0.035 0.084 0.005 60,000 0.0005 0.000 -0.001 0.006 0.057 0.048 0.125 0.0053 67,000 yield -0.002 -0.0025-0.003 0.002 0.076 0.064 -

-0.001 The test was discontinued due to the plate bending Preset on Tie Down Bar - 0.006" I

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