ML20077N056
| ML20077N056 | |
| Person / Time | |
|---|---|
| Site: | Limerick  |
| Issue date: | 08/10/1983 |
| From: | Davidson A PATEL ENGINEERS |
| To: | |
| Shared Package | |
| ML20077N044 | List: |
| References | |
| PEI-TR-83-29, PEI-TR-83-29-R-A, NUDOCS 8309120497 | |
| Download: ML20077N056 (150) | |
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U TECHNICAL REPORT PEI-TR-83-29 July 14. 1983 REVISION A, AUGUST 10, 1983 SEISMIC QUALIFICATION OF CLOW WAFER STOP VALVE ASSEMBLIES JOB NUMBER 82-2053-01(N),
-02(N), -03(N), -05(N), -07(N)
ITEM NUMBERS 1.3, 1.5, 1.7, 1.11, 1.13 24"-HBB-BF-AO-57-114, -123, -124 A 18"-HBB-BF-AO-57-104 6"-HBB-BF-AO-57-121, -131 6"-HBB-BF-MO-57-109, -162, -164 4"-HBB-BF-MO-57-161, -163 A
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. by N. Allen Davidson Prepared for Bechtel Power Corporation for Philadelphia Electric Limerick Plant In Accordance ,with Bechtel Specification 8031-P-144, Revision 1 Work Performed Under Clow Purchase Order No. 30-10469 Bechtel Purchase Order No. 8031-P-144-AC Patel Job Number 8220 for Clow Corporation, Engineered Products Division Westmont, Illinois I
8309120497 830901 PDR ADOCK 05000352 A ppg
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Report No. PEI-TR-83-29 Page'No. 1 REVISION A 9 ( REPORT NO.: PEI-TR-83-29
?P PREPARED BY: .
N. Allen Davidson, Structural Dynamist APPROVED BY: tw A/L Johnny F. genkins,# / Vice-President Q.A. REVIEW: A Murvi'n J. Kimbrell, Df' rector, Product Assurance ORIGINAL ISSUE: July 14, 1983 ( . REVISIONS REV. REV. REV. CHECKED Q.A. DESCRIPTION OF CHANGES NO. DATE BY BY BY AND PAGES REVISED A 8/10/83 NA M JFJ M MJ Cover Page - Deleted "-147". Page 1 - Revised Section 1.2.2. RPP h Page 2 - Changed "57114" to "57-114", Added NOTE to Page. Page 4 - Changed " Water" to "Wafef.' Page 5 - Added Paragraph "The static tests........ valve assemblies tested". Page 5.1 - Added Figure 1 and Paragraph "The centrifuge speed.......of Appendix A. Moved Section 4.3.2 from Page 5 to Page 5.1. Page 6 - Changed " Event" to
" Earthquake", and " Mark I' to " Mark II".
Page 7 - Revised Items 2 and 3. Page 8 - Revised Items 5,6, and 7. APP. A - NTS Test Rt.528-0951Rev.C, V Affected pp shown on op 11 of Aco.C PEI Form No. 611 - 7/1982 patel engineers huntsville, o!abcmo
Report No. PEI-TR-83-29 Page No. ii O V CERTIFICATION OF CONFORMANCE The subject valve assemblies manufactured by Clow Corporation and described in this report have undergone seismic analysis and have been subjected to seismic testing to evaluate compliance with the governing specifications. Testing was performed in accordance with IEEE 344-1975, " Recommended Practices for Seismic Qualification of Class IE Equipment for Nuclear Power Generating Stations", and IEEE 382-1980, "IEEE Standard for Qualification of Safety Related Valve Actuators".
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Report No. PEI-TR-83-29 Page No. iii v-ABSTRACT A sequence of seismic qualification analysis and testing was performed on the subject valve assemblies manufactured by Clow Corporation. The tests were performed in accordance with National Technical Services Test Proce-dure 528-0951 Revision A. Structural integrity of the assemblies and operability of the functional components were verified during and after the qualification testing. The seismic analysis was done by Patel Engineers, Huntsville, Alabama. The analysis confirms the integrity of the structure and compliance with applicable codes and specifications. O - I 1 1 l l l l l l l p) patel engineers huntsville, alabama
Report No. PEI-TR-83-29 Page No. iv r TABLE OF CONTENTS P,,3yyj, 1.0 INTRODUCTORY
SUMMARY
................................... I 1.1 Introduction...................................... 1 l 1.2 Summary of Result s and Conclus ions . . . . . . . . . . . . . . . . I 1.2.1 Analysis................................ I 1.2.2 Testing................................. 1
2.0 DESCRIPTION
OF EQUIPMENT............................... 2 3.0 DESIGN SPECIFICATIONS.................................. 3 i l 4.0 Q U AL IF IC AT ION AP PR0 ACH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 l 4.1 Genera 1..........................................". 4 l 4.2 Phase I - Analysis................................ 4 . 4.3 Phase II - Testing................................ 5 4.3.1 Static Testing.......................... () i 5 l , 4.3.2 Dynamic Testing......................... 5 4.3.2.1 OBE Tests..................... 6 4.3.2.2 SSE Tests..................... 6 5.0 EVALU AT ION OF TE S T DATA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
6.0 CONCLUSION
S............................................ 9 l APPENDIX A TEST REPORT l-r i s patel engineers i huntsville, olabama
k i Report No. PEI-TR-83-29 Page No. 1 REVISION A c
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,s 1.0 INTRODUCTORY SUKHARY 1.1 Introduction This report presents the results of seismic qualification of Clow wafer stop valves for use in Philadelphia Electric Company's Limerick Nuclear Station. The testing portion was performed at National Technical Services, Saugus, California, in accordance with NTS Test Procedure 528-0951 Revision A.
The objective of the entire qualification program was met in the following phases:
- 1) Analytical phase where PEI, executed all analysis associated ~ with the requirements and documented this in the following reports:
a) PEI-TR-83-13 b) PEI-TR-83-14 c) PEI-TR-83-15 d) PEI-TR-83-16
- 2) A test phase in which PEI provided engineering
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decisions for qualification procedures and NTS (s_,')s
- provided both static and dynamic testing services as reported in Appendix A.
1.2 Summary of Results and Conclusions 1.2.1 Analysis The seismic analysis reports under Section 1.1 reveal that the stress leiels of the subject valve assemblies as analyzed do not exceed ASME allowable stress values as described in Bechte l ^ l Specification 8031-P-144, Revision 1. 1.2.2 Testing A 1 The valve assemblies were inspected following successful I completion of the subject tests and showed no visible damage. Operator parts , that did sustain seismically induced damage, had design modifications made on site. The modified units successfully completed the qualification program with no visible damage. Needed design modifications and maintenance requirements are detailed in Section 5.0 of this report. Operability of the functional components was verified during and after testing. Full documentation of the tests can be fo'und in NTS Test Report Number 528-0951, Revision C.
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h Report No. PEI-TR-83-29 Page No. 2 REVISION A 'V
2.0 DESCRIPTION
OF EQUIPMENT Four sizes of Clow wafer stop valves assemblies are included under this seismic qualification program. They are: a) 4-inch motor operated valve assembly b) 6-inch motor operated valve assembly c) 6-inch air operated valve assembly d) 18-inch air operated valve assembly e) 24-inch air operated valve assembly The specific units tested ar'e the following:
- 1) Clow 24-inch tricentric lugged wafer valve, serial number 82-2053-07-(N)-01, tag number 24-HBB-BF-AO-57-114 A
- 2) Clow 6-inch tricentric lugged wafer valve, serial number 82-2053-03-(N)-01, tag number 6-HBB-EF-AO-57-121
- 3) Clow 6-inch tricentric lugged wafer valve, serial number 82-2053-02-(N)-01, tag number 6-HBB-BF-MO-fs 57109
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- 4) Bettis 24-inch air operated actuator, model number NT820-SR4-S, part numbe r 49124, serial number 82-9029-1, tag number A0-57-114
- 5) Bettis 6-inch air operated actuator, model number NT312-SR5, part number 41041, serial number
,82-9029-5, tag number A0-57-121
- 6) Limitorque 6-inch motor operated actuator, model number SMB-00-10, serial number 352-809, tag number MO-57-109 NOTE: The 4-inch motor operated and 18-inch air operated valve assemblies are qualified by similarity with other sizes tested, A due to the Valve Qualification Table, C-1 of Design Specification 8031-P-144, Revision 1.
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Report No. PEI-TR-83-29 Page No. 3 f~%
'b 3.0 DESIGN SPECIFICATIONS The following documents were used in the performance of the seismic qualification program:
o Bechtel Power Corporation Design Specification No. 8031-P-144 Revision 1, " Design Specification for Flanged Butterfly Valves for Nuclear Service for the Limerick Generating Station Units 1 and 2" o Bechtel Power Corporation Specification No. 8031-P-358, " Specification for Dynamic Qualifica-tion of Safety Related Actuators for the Limerick ) Generating Station Units 1 and 2" l o Bechtel Power Corporation Specification No. l 8031-G-ll, Revision 15, General Project Require- l ments for Valve Motor Operators for the Limerick ! Generating Station Units 1 and 21", May 7, 1979 l o Bechtel Power Corporation Specification No. l 8031-P-359, " Specification for Valve Air Operators , l for the Limerick Generating Station Units 1 and 1
. 2", November 25, 1981 o IEEE 382-1980, "IEEE Standard for Qualification of Safety Related Valve Actuators" o IEEE 323-1974, "IEEE Standard for Qualifying Class lE Equipment for Nuclear Power Generating i Stations"
\ - o IEEE 344-1975, "IEEE Recommended Practices for Seismic Qualification of Class lE Equipment for Nuclear Power Generating Stations" o USNRC Regulatory Guide 1.100, " Seismic Qualifica-tion of Electric Equipment for Nuclear Power Plants", March 1976 o USNRC Regulatory Guide 1.89, " Qualification of Class IE Equipment for Nuclear Poder Plants" o ASME Boiler and Pressure Vessel Code Section III, Subsection NC Class 2 Components and Subsection ND Class 3 Components i n s I v . patel engineers ! huntsville, clabamo
_ f; Report No. PEI-TR-83-29 Page No. 4 REVISION A O ( l 4.0 QUALIFICATION APPROACH 4.1 General Testing was performed in accordance with NTS Test Procedure 528-0951 Revision A. Complete descriptions of the test set-ups and test procedures are presented in the test report of Appendix A. The objective of the qualification program is to demonstrate that the subject valves and valve actuators meet the requirements set forth in the specifications and guidelines of Section 3.0. To accomplish this a combined test and analysis approach was taken. 4.2 Phase 1 - Analysis The analysis was performed as follows:
- 1) Develop mathematical models of each valve /actua-tor configuration
- 2) Calculate resonant frequencies
- 3) Evaluate resonant frequencies
. t O I
- V 4) Perform static analysis
- 5) Evaluate structural integrity The results of the analysis efforts are documented in Patel Technical Reports:
. 1) PEI-TR-83-13, " Seismic Qualification Analysis of ( Clow 24-Inch Wafer Stop Valve"
- 2) PEI-TR-83-14, " Seismic Qualification Analysis of l Clow 18-Inch Wafer Stop Valve"
- 3) PEI-TR-83-15, " Seismic Qualification Analysis of Clow 6-Inch Wafer Stop Valve"
- 4) PEI-TR-83-16, " Seismic Qualification Analysis of Clow 4-Inch Wafer Stop Valve" A All valve assemblies as analyzed in the above reports meet the requirements for seismic analysis as set forth in the Bechtel design requirement number 8031-P-144, Revision 1.
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Report No. PEI-IR-83-29 Page No. 5 REVISION A
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( i N/ _ . . 4.3 Phase II - Testing 4.3.1 Static Testing Static testing was performed on the following items:
- 1) 24-Inch Clow valve with Bettis air operated actuator i
- 2) 6-Inch Clow valve with Limitorque motor operated actuator operated
~
- 3) 6-Inch Clow valve with Bettis air actuator The above items (described in Section 2.0) were subjected to static loads to demonstrate the capability of withstanding the simultaneous application of worst case forces anticipated in the course of service life. .
The loads applied to the equipment to satisfy the static load
- qualification requirements were the following:
~~ 1) All normal loads, including weight of valve top i . works and dif ferential pressure across the disc of
-' 55 psid
- 2) Horizontal and vertical inertial loads, equivalent to 4.5g seismic acceleration in each axis The equipment was rigidly attached to a mounting plate atop a centrifuge in an orientation which created worst-case stresses resulting from the application of the specified loads. Since the test was done on a centrifuge, the applied load during seismic acceleration was applied continuously as body forces along the entire assembly.
All ancillary electromechanical devices necessary for equipment function were energized and monitored for change of state during the application of the inertial loads. The static tests were performed separately on each valve assembly listed under Items 1 through 3 above. The 6-inch valve assemblies were tested on a 25 foot radius centrifuge. The 24-inch valve assembly was tested on a 50 foot centrifuge. The valve assemblies were mounted as shown in the photographs of Figures 10 through 12 of Appendix A. Figure 1 gives a general orientation for the valve assemblies tested. O v patel engineers huntsville, clabamo I
Report No. PEI-TR-83-29 Page No. 5.1 REVISION A J O . OPERATOR
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s l l l ~ GIMBLE l NENTRIFUGEARM l O V ' FIGURE 1 GENERAL ORIENTATION OF VALVE ASSEMBLIES STATICALLY TESTED
- The centrifuge speed of revolution for each unit statically I
tested is contained in the test report of Appendix A. 4.3.2 Dynamic Testing Dynamic testing was performed on the following items:
- 1) 24-Inch Bettis air operated actuator l
- 2) 6-Inch Bettis air operated actuator l
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e Report No. PEI-TR-83-29 Page No. 6 REVISION A I U The above equipment (described in Section 2.0) was subjected to dynamic testing to demonstrate its capability of withstanding the acceleration of seismic events anticipated in the course of service life. The subject items were rigidly attached to the vibration table in their normal in-service mounting configuration. Electrical and pneumatic connections were provided to allow operation and monitoring of the equipment. The operators were cycled during each vibration exposure, as required. 4.3.2.1 OBE Tests The Operating Basis Earthquake (OBE) RIM Test was performed to A simulate the seismic vibration aging of five OBE earthquakes. The actuators were subjected to two sinusoidal sweeps at the required 3g (+10%, -0%) leve ls , in each of the three major orthogonal axes. Each sweep was conducted from 2 Hz to 100 Hz to 2 Hz at a rate equal to or less than one octave per minute. One sweep, in each axis, was performed with each actuator in the open position and one in the closed position. 4.3.2.2, SSE Tests The Safe Shutdown Earthquake (SSE) a'nd Mark II RIM Test were A performed to provide verification of the capability of the actuators to perform their sa fe ty-re lated functions when subjected. to the maximum dynamic vibration for which they were designed. The actuators were subjected to single freq uency sine beat tests at 4. 5g ( +10%, -0%) levels in each of the three major orthogonal axes. The sine beat tests were conducted at one-third octave in,tervals over the frequency range of 2 Hz to 100 Hz. The excitation at each frequency was in the form of a continuous series of sine beats of 15 sinusoidal cycles per beat for a minimum duration of 15 seconds. The successive beats were phased such that superposition of response motion was additive. The actuators were cycled from closed to open to closed at each of the test frequencies during testing. s
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Report No. PEI-TR-83-29 Page No. 7 REVISION A i '% J t l 5.0 EVALUATION OF TEST DATA i Appendix A contains the details from execution of the test proce-dures listed in NTS Test Procedure 528-0951. The tests demon- ,i strated the ability of the test articles to retain their struc-( tural integrity and functional capability during and after the specified tests. I Although there are Notices of Deviation contained in Appendix A, the majority of anomalies noted (concerning the Bettis air operated actuators) were due to equipment mishandling with the exception of the following items which constitute required design modifications or required maintenance items af ter an OBE. It should also be noted that when Bettis operator failures due to mishandling occurred, the subject operators pe rformed their safety-related functions and went to a closed position.
- 1) The copper supply line from the filter assembly on the 6-inch Bettis air operated actuator should be made as short as pos s ible . This will be accomplished by rotating the filter as s embly section such that the air supply outlet will be pointing in the direction of the air cylinder. -
d Design Requirement
- 2) A support band must be added to the air cylinder
! of the 6-inch, 18-inch, and 24-inch Bettis air operated actuators. This will be used to wrap A around the flex-conduit solenoid le ads and air ! cylinder to prevent the flex-conduit from gaining maximum motion which might be detrimental to the solenoid. - Design Requirement
- 3) Bolts securing the "L" brackets on the junction box of the 6-inch, 18-inch , and 24-inch Bet tis air operated actuators should be checked to insure the proper length bolt was used in order that the A bolts may be short enough to allow for a bolt preload. - Design Requirement
- 4) The brass nipples leading from the solenoid valve to the air cylinder on the 6-inch Bettis air operated actuators, must be replaced with a stainless steel nipple measuring no more than 1 1/2 inch of exposed length; the wall thickness of the nipple should be 1/8 inch minimum. - Design Requirement n
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4 ( . __ . Report No. PEI-TR-83-29 Page No. 8 REVISION A O
'U
- 5) The spring can tie rod bolts on the 6-in ch ,
18-inch, and 24-inch Bettis air operated actuators A must be retorqued to specified torque levels during normal maintenance or shutdown periods. - i Maintenance Requirement
- 6) Inspect the gasket material between the housing and air cylinder of 24-inch , 18-inch , and 6-inch Bettis air operated actuators during maintenance A or shutdown periods . This gasket material extruded during the test program, but appeared to have no effect on performance of the operator. -
Maintenance Requirement
- 7) The solenoid coil housing on the subject Bettis air operated actuators should be checked for signs 4
of cracking. This cracking was noted during A testing, but appeared to have no effect on the performance of the operator. - Maintenance Requirement 3 Cs - I l O potel engineers huntsville, clobomo
i Report No. PEI-TR-83-29 Page No. 9 N 4 J
6.0 CONCLUSION
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The pos t- tes t inspection and evaluation of analysis and test data lead to the following conclusions:
- 1) The valve assemblies as analyzed do not exceed the ASME allowable stress limits as set forth in l
Bechtel Specification 8031-P-144, Revision 1.
- 2) The equipment subjected to the series of seismic qualification testing maintained structural integrity and performed its specified safety-related functions during and after the applicable tests.
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4 I 1 l APPENDIX A TEST REPORT O - J Patel engineers huntsville. clabomo
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.s I .s Test Report Number 528-0951, Revision C
- i . Seismic Qualification Testing of a
Butterfly Valves and Actuators May 26, 1983 Revision A: June 27, 1983 Revision B: July 7,1983 Revision C: August 5, 1983 l l PREPARED FOR: PATEL ENTERPRISES, INC. P.O. Box 3531 3400 Blue Springs Road NW Huntsville, Alabama 35810 PREPARED BY: NATIONAL TECHNICAL SYSTEMS . Testing Division ! 20988 West Golden Triangle Road Saugus, California 91350 0 .
~~~~~
Ns Report 528-0951, Rev. C N Sonal sy. i 8 t
, rb REVISION C
SUMMARY
7 August 5, 1983 l l Page(s) Affected Paragraph (s) Affected i vii Table of Contents 6 5.1.2.1, 5.1.2.2 8 5.2.1
, 9 5.3.2.3 10 5.3.3.2.1, 5.3.3.3 -
11 5.3.3.3, 5.3.4.2 25 Table II
' 28 Figure 1 l 29 Figure 2 l
30, 32 Figure 3, Figure 5 i B-3 Appendix B B-4 Appendix B l Exhibit II Added
, Exhibit III Added
't 65 N00 9, Rev. A Due to revisions, some page page numbers were changed. These revisions reviewed and approved by:
/ . Date: E !
TECHNICAL WRIIER, Glenn D. Meltzer ' l Oh NUCLEAR PROGRAMS MANAGER, Alain Frocnaux
,4469tssio4 Date: f[f [83 I
sW #* Q , t
/ ) te: Gij f / 70 d QUALITY AS3URANCE MANGER, Robert A Ely ' At F ,
i l N) i J e 11 E369 mr - ~ ' - ' - - - - - +
i Report 528-0951, Rev. B pg Systems i s
'3
. , REVISION B
SUMMARY
July 7, 1983
'4 Page(s) Affected Paragraph (s) Affected v, vi Table of Contents 4 3.2 5, 6 5.1.2.1 7 5.1.2.2, 5.1.2.3 9 5.3.2.1 -
24 Table II 28 Figure 1 i 29 Figure 2 30 Figure 3 31 Figure 4
; 34 Photograph 2 38 Photograph 6 57 N0D D-2, Rev. A (Supersedes previous N0D D-2)
I. Due to revisions some page numbers were changed. A) The'se revisions reviewed and approved by: t - I l t TECHNICAL WRITER, Glenn D. Meltzer Date: M
# /
i df) Mt # .Da,,t e : 1 l i ., 7 RM d NUCLEAR [ROGRAMSMANAGER,MarkA.SggF" ] h[7 990 FESS /cg !' 5 8 Okg (b l M ~,- Csw' b( ll lv NO. 2' -
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N Report 528-0951, Rev. A sym J f V REVISI9N A
SUMMARY
i June 27, 1983 i Page(s) Affected Paragraph (s) Affected ) l iv, y Talle of Contents '
)
1 1.1 2 1.2 \ 3, 4 2.2, 3.2 - 6, 7 5.1.2.2 7 5.1.2.3 8 5.1.2.4 9 5.3.2.3 10, 11 5.3.3.2.1, 5.3.3.3 11 5.3.4.1, 5.3.4.2 12 through 15 Table I 16 through 25 Table II 26 Table II-A 27 - Table III 28 Figure 1 30 Figure 3 , 31 Figure 4 32 ' Figure 5 t 35 Photograph 3 50, 51 C0P 4 52, 52A, 52B C0P 5 53, 54 C0P 6, C0P 7 68 N0D-12 A-11 Appendix A B-1 through B-5 Appendix B Exhibit-I Added Due to revisions some page numbers were changed. These revisions reviewed and approved by: NI - Date: Mb TECHNICAL' WRITER, Glenn D. Me Uzer nGUCLEAR _ W PROGRAMS
& $- Date: EONM2- lO3 MANAGER, Mark A. Smith ~
MdilM!0%f o9 Q Sg (
/ '
QUALITY ASSURANCE MANAGER, R 1E wo. c oa u 2 5Date: s# h./k3 trt A. j
. ., s
$369
- 1. um Reoort 528-0951
$iN 2 '. APPROVALS
- 1
.3 Written By: / ' TECHNICAL WRITER, Glenn 9. Meltzer Date: bM IN 8 Approved By: T QA k M blh NUCLEAR ?ROGRAMS MANAGER, Mark A. Smith Date: (, M 19 83
-fflSSIOy,
{ . k of Approved By: /h , p 1 No. qum2 D e c9 /fCd o- **'- ^-"*"" "*""
> "-p's"s'l$$y 4
l1 0 4P O . V E369
4 Report 528-0951, Rev. B
- Nellonel Tectmical
{ Systems . 3 TABLE OF CONTENTS
, a, Section Title Page a
. 1.0 PURP0SE................................................. 1 1.1 Test Articles..................................... 1 i 1.2 Com po ne nt Ma t ri x . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 i
l
2.0 REFERENCES
.............................................. 3 3.0 S U MMA R Y . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - i 3.1 Introduction...................................... 3 l 3.2 Co n cl u s i o n . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 1 4.0 TEST CONDITIONS AND TEST E0VIPMENT...................... 4 i ! 4.1 Te s t Co nd i t i o n s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 is 4.2 Test Equipment.................................... 4 5.0 TEST PROCEDURE AND TEST RESULTS......................... 5 5.1 Performance Testing............................... 5 5.2 Vi b ra t i o n Ag i n g . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 5.3 Seismic Testing................................... 9 TASLES
\- I Pre and Post Pe rfo rma nce Test Summa ry. . . . . . . . . . . . . . . . . . . 12 II Seismic Testing Performance Summary (During Testing)
Dynamics Test........................................... 16 IIA Test Sequence........................................... 26 III- Resonance Survey Results................................ 27
, FIGURES 1 6-inch Air 0perated Actuator (Before Modification)...... 28 2 6-inch Air Operated Actuator (After Modification)....... 29 3 24-i n ch Ai r Actu a to r . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30
4 Required Input Motion................................... 31 5 Static Load Test Fixture ............................... 32 PHOTOGRAPHS 1 Se at Le a k a g e Te s t . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 2 Resonance Survey and Dynamics Test Setup (Y Axis)
- , 24-Inch Ai r Ope rated Actua to r. . . . . . . . . . . . . . . . . . . . . . . . . 34 l 3 Resonance Survey and Dynamics Test Setup (Y Axis) 6-In ch Ai r Ope rated Actua to r. . . . . . . . . . . . . . . . . . . . . . . . . . 35 l 4 Dynamics Retest 24-i nch Actuator (Y-Z Axes ) . . . . . . . . . . . . . 36 5 Copper Line Damage - Dynamics Test (6-inch Actuator).... 37 6 Reconfi gurati on for 6-i nch Actuator. . . . . . . . . . . . . . . . . . . . . 38 7 Damage Noted - Dynamics Test (6-inch Actuator) . . . . . . . . . . 39 8 Reconfiguration (1/2-inch Steel Pipe on Inlet to Accum-40 l
' l's)
\-- 9 ul a to r) 6-i nch Actua to r. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Reconfiguration Stainless Steel Nipple (6-inch Actuator) 41 10 St a ti c Te s t Se tu p 6-i nch Val ve . . . . . . . . . . . . . . . . . . . . . . . . . . 42 vi _ ,_. _ _. - _ __ ._ _ _ E . _
4
,,,,, Report 528-0951, Rev. C Technicai
; sy.i E
i T' i
' s_(')
i TABLE 0F CONTENTS (Continued) , i Section Title Page 11 St ati c Te s t Setu p 24-i n ch Val ve . . . . . . . . . . . . . . . . . . . . . . . . . 43
. 12 Stati c Test Setup 24-i nch Va1 ve . . . . . . . . . . . . . . . . . . . . . . . . . 44 13 Dynamics Retest. Y Axis 24-inch Air Operated Actuator.. 45 CHANGES OF PROCEDURE 1 Baseline Functional..................................... 46 -
2 Vibration Aging......................................... 47 3 Dynamic Test............................................ 48 1 4 Sei smi c Oual i ficati on Testi ng . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 - 5 Test Report............................................. 52 6 Static Test............................................. 53 l, 7 Static Test............................................. 54 NOTICES OF DEVIATION 1 Dy n am i c Te s t i n g . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55 2 Seismic Testing......................................... 57 3 Po st-Dyn ami c Fun cti on al . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58 4 Baseline Functional..................................... 59 5 Dy n am i c Te s t . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... . 60 s_ d Dynamic Testing......................................... 62 7 Dynamic Test............................................ 63 8 Dynamic Test............................................ 64 9 Baseline Functional..................................... 65 10 Dynamic Testing......................................... 66 11 Dy n a m i c Te s t i n g . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
. 12 Basel i ne Functional (Stati c ) . . . . . . . . . . . . . . . . . . . . . . . . . . . 68 APPENDICES A E q u i p me n t Li s t . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A-1
- ' B Stati c Test Perfo rmance 0ata . . . . . . . . . . . . . . . . . . . . . . . . . . . . R-1 C Resonance Survey and Dynamics Test 24-inch Air.. . .. . . .. .
Operated Actuator....................................... C-1 D Resonance Survey and Dynamics Test on 6-inch Air........ 0perated Actuator....................................... D-1 L EXHIBIT ' I Seat Leakage Test Procedure II Static Test Parameters III SSE Test Acceleration Levels - [ t vii E369
u, , Reoort 528-0951. Rev. A Testinical syse 7-.
' A
.lU r 1.0 PURPOSE
. The purpose of this report is to 'present the test procedure used and the test results obtained during a test program. The objective of the test program was to verify that the Valves and Actuators, defined in Paragraph 1.1, were capable of performing their safety-related function during and subsequent to seismic qualification testing.
1.1 TEST ARTICLES A component matrix is provided in Paragraph 1.2. The test article assemblies are listed below according to each seismic test exposure: Dynamic Test One 24-inch air-operated Actuator (item 1) One 6-inch air-operated Actuator (item 2) Static Test
~
One 6-inch Valve with an air operated Actuator (items 5 and 2) Oise 6-inch Valve with a motor operated Actuator (items 6 and 3) ( . One 24-inch Valve with an air operated Actuator (items 4 and 1) The Actuators were equipped with ancillary devices to verify func-tional performance. All ancillary devices were installed by the customer or in accordance with customer request. O d . Eas, __ __ _ _ _ , _ _ , . _ . ~ _ _ _ _ -
Report 528-0951, Rev. A gangg, syn r 1.2 COMPONENT MATRIX 9 Model Number / Part Serial Tag Item Quantity Part Description Description Number Number Number _ 1 1 Bettis, 24-inch Air NT820-SR4-S 49124 82-9029-1 A0-57-114
- Operated Actuator '
f 2 1 Bettis, 6-inch Air NT312-SR5 41041 82-9029-5 A0-57-121 ! Operated Actuator Limitorque 3 1 6-inch Motor SMB-00-10 --- 352-809 M0-57-109 Operated Actuator H2BC 4 1 24-inch Valve Tricentric --- 82-2053- 24-HBB-BF-Lugged 07-N-01 A0-57-114-Wafer - ( . 5 1 6-inch Valve Tricentric --- 82-2053- 6-HBB-BF-Lugged 03-N-01 A0-57-121 Wafer 6 1 6-inch Valve Tricentric --- 82-2053- 6-HBB-BF-1 - Lugged 02-N-01 M0-57-109 Wafer 1 1 l i l0 E369
Report 528-0951, Rev. A yg
- sy.s.m.
e-JO - I
2.0 REFERENCES
g 2.1 National Technical Systems Nuclear Test Procedure 528-0951, Revision A, dated 4 January 1983 (modified by Changes of Procedure 1 through
; 7, included herein).
2.2 Clow Corporation Pneumatic Seat Bubble Test, EPS 30-49-832, Revi- l sion A, dated 18 February 1983 (includd herein). I
' 2.3 Patel Enterprises Purchase Order Number PEI-8220
- 3.0
SUMMARY
3.1 INTRODUCTION
9 Three Valves and Three Actuators, described in Paragraph 1.1, have been subjected to seismic Testing as described in this report. A summar" of the acceptance criteria and results for the pre and post perfor..iance baseline tests is presented in Table I. A summary of the acceptance criteria and results during the seismic tests is pre-sented in Table II. The test sequence is presented in Table II-A. (3 g
3.2 CONCLUSION
The results of the performance tests indicate that the Valves and Actuators satisfactorily completed the requirements of reference 2.1. During the post-test performance verification on the 24-inch air operated Actuator, an apparent failure was noted. A careful analysis of the test setup revealed an insufficient air supply to the Actuator causing the Actuator to stop during its operation cycli ng. When sufficient air flow was supplied to the Actuator, the Actuator operated satisfactorily. Out-of-tolerance Actuator operating times were noted for the 6-inch Valve with motor operated Actuator and 24-inch Valve with Air Operated Actuator. The Actuator travel times were monitored for information only and do not neces-sarily indicate equipment failure. During seismic testing, design
' modifications were implemented on the 6 and 24-inch air operated Actuators, as detailed below. No modifications were required for l the Valve assembles. All results for the Valve assemblies conformed to the specification requirements.
24-Inch Air Operated Actuator A. The original bolts securing the ~"L" bracket (holding the l Junction box) to the actuator body must be removed and replaced with commerci al grade (minimum) bolts 1/2-inch shorter in length. q B. The gasket between the housing and the air cylinder shall l be inspected and replaced, as required. E369
Report 528-0951, Rev. B s-sE p. ',! O j C. A band shall be installed around the air cylinder to
, support the flexible conduit. .. D. The spring can tie rods shall be inspected and retorqued, if required, as routine maintentance.
E. The solenoid coil housings shall be inspected and main-tained as required. 6-Inch Air Operated Actuator f A. The copper line between the cylinder and the ASCO Valve shall be removed and replaced by copper tubing of a short-er length. This re-configuration shall be accomplished by:
- 1. Rotating the filter / regulator 180' and installing a direct copper line between the filter / regulator
, and the solenoid operated pilot Valve, reference Photograph 6.
B. .The brass pipe connecting the air cylindcr and ASCO Valve l must be replaced by a stainless steel pipe shorter in length and heavier gauge than the copper pipe. The nipple exposed length not to exceed 1-1/2 inch. The gauge shall be 1/8-inch. O , C. A band shall be installed around the air cylinder to support the flexible conduit. D. The spring can tie rods shall be inspected and retorqued, if required, as routine maintentance. E. The solenoid coil housings shall be inspected and main-tained as required. A 4.0 TEST CONDITI0t.3 AND TEST EQUIPMENT 4.1 TEST CONDITIONS Unless otherwise specified herein, all tests were performed at room ambient conditions defined as a temperature of 73 tl8'F (23 t10'C), a relative humidity of 50 130 percent, and a barometric pressure of ~28.5 +2.0, -3.0 inches of mercury absolute (725 +50,
-75 mm of mercury absolute).
4.2 TEST EQUIPMENT The test equipment presented in Appendix A was calibrated, as re-quired, in accordance with MIL-STD-45662 Notice 1 and is traceable to the Natit'r0 Bureau of Standards (NBS). The NBS traceability records are qa ntained on file in the NTS Quality Assurance Office. O
'5: u.
. Report 528-0951 Rev. 8 ! .L
- f. IO i
j 5.0 TEST PROCEDURE AND TEST RESULTS .
- f. 5.1 PERFORMANCE TESTING I Reference 2.1, Paragraph 7.1 Dates Performed: :
- Pre-Dynamics Baseline (24-inch Air Operated Actuator) 15 March 1983
- - Post-Dynamics Baseline (24-inch Air Operated Actuator) 1 April 1983 through 4 April 1983 Pre-Dynamics Baseline (6-inch Air Operated Actuator) 13 April 1983 Post-Dynamics Baseline (6-inch Air Operated Actuator) 20 April 1983
! Pre-Static Baseline (6-inch Motor Operated Valve) 27 April 1983
- , Post-Static Baseline (6-inch Motor Operated Valve) 29 April 1983 Fre-Static Baseline (6-inch Ai r Operated Valve) 28 April 1983 Post-Static Baseline (6-inch Air Operated Valve) 29 April 1983
- - Pre-Dynamics Retest Baseline (24-inch Air Operated Actuator) 4 May 1983 O, Post-Dynamics Retest 5 May 1983 Baseline (24-inch Air Operated Actuator) [
i Pre-Static Baseline (24-inc.h Air Operated Valve) 6 May 1983 through 7 May 1983 Post-Static Baseline (24-inch Air Operated Valve) 7 May 1983 5.1.1 Baseline Examination , l - !
.Each Valve and Actuator was visually examined on arrival at NTS, l
prior to functional testing and at the conclusion of the test pro- ! gram. Any adverse or out-of-tolerance connditions were documented and reported to Patel Enterprises. All adverse or out of tolerance conditions are summarized in Tables I and II. 5.1.2 Baseline Performance Tests 5.1.2.1 Air-Operated Actuators j The Air-Operated Actuators were monitored in accordance with the 1 i following criteria: A. With a load fixture installed simulating seating torque
- i and with minimum air pressure applied *,.the Actuator was required to operate to either end of rotation within a 5-second period. The open-to-close or close-to-open air O' Actuator travel times were determined by visual inspection of the rotating cam and utilization of a stop watch.
Ei,
I8 Report 528-0951, Rev. C i N Ja
^! When the rotating cam movement started, the watch was started. When the rotating cam movement stopped, the watch was stopped. The solenoid pilot Valve was operated at 80 ;4 percent and 100 percent of line voltage, reference Change of Procedure 1. During the Post Dynamics Baseline on the 24-inch Air Operated Actuator, an inadequate air compressor .4'~
pressure supply resulted in the apparent failure of the Air Actuator, reference Notices of Deviation D-2 and D-3. , Careful investigation of the test setup revealed that the l l air compressor used to operate th 24-inch Air Operated Actuator was unable to supply sufficient volumetric flow to - meet the requirements of the 24-inch Operator. The test ! i setup was modified to meet the volumetric flow require-
- 8 ments of the 24-inch operator and operability was verifio before and after the partial dynamics retest, reference l Page 12.
- i. B. The leakage rate at the rod seal at maximum pressure was not required, reference Change of Procedure 1.
C. Confirmation and recording of above parameters and limit switch continuity at extremes of travel: .L ,
. Levels Six-inch Actuator 24-inch Actuator Minimum Air 85psig 80 psig pressure Maximum Air 100 psig 100,psig
- j. pressure Torque criteria 495 ft-lbs 7,958 ft-lbs (seating valve) 5.1.2.2 Motor-0perated Valve The Valve was monitored in accordance with the following criteria:
A. A maximum opening or closing time of five seconds with a differential air pressure of 55 psig. All operations were , achieved with 80 percent of rated voltage (80% x 460 V), L 368, 3 phase, 60 Hz. The times for opening and closing l were recorded and are presented in Appendix B and Table I. B. The Seat Leakage Test was conducted in accordance with Clow Corporation Acceptance Test Procedure EPS 30-49-832, Re-The Seat Leakage Test O vision A presented in Exhibit I. consisted of a visual inspection of the seating surfaces. The seating surfaces were coated with leak-tec solution 336'
I. Report 520-0951, Rev. B . .O of leakage.
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Leakage was not observed. Leakage measure-i ment testing was then performed to determine the valve
- f. leak rate. The Leakage Measurement Test was performed using 'a blind flange fitted with a copper tube, on the downstream side of the valve, to collect air leaked. The copper tube was submerged in water to a depth of 1/4 inch to 1/8 inch. The upstream side of the valve disc was pres-surized to 55 psig. The detailed test procedure is pre-sented in Exhibit I. The test results are presented in i Appendix B, Pages B-6 and B-7. No leakage was noted.
l C. Electrical data was recorded during the operational test (described in subparagraph A), as follows:
- s
- 1. Test voltage
- 2. The motor running current drawn during test opera-
'I tion of the Valve, in both opening and closing directions, for all Valves
- 3. The motor current drawn at the time of opening of the torque switches at Valves recommended setting l 4 Recording of settings and performance verification of torque switches and position switches 5.1.2.3 Air-Operated Valves These -Valves were monitored in accordance with the following cri-
- teria
(' A. A maximum Valve closing or opening time of five seconds ! with a differential air pressure of 55 psig. All opera-tions were achieved with minimum supply pressure.* The times for opening and closing were recorded as well as any failure mode, reference Table I. The open-to-close or close-to-open air Actuator travel times were determined l by visual inspection of the rotating cam and utilization of a stop watch. When the rotating cam movement started, the watch was started. When the rotating cam movement stopped, the watch was stopped. i B. The Seat Leakage Test was conducted in accordance with Clow ! Corporation Acceptance Test Procedure EPS 30-49-832, Re-vision A presented in Exhibit I. The Seat Leakage Test , consisted of a visual inspection of the seating surfaces ! with the Valve in the closed position. The seating sur-I faces were coated with leak-tec solution on the downstream . side of the disc with a pressure of 55 psig applied to l the upstream side of the disc. The downstream side of
- the disc was visually checked for evidence of leakage.
I Leakage was not observed. Leakage measurement testing was then performed to determine the valve leak rate. The 3 Leakage Measurement Test was performed using a blind flange J fitted with a copper tube, on the downstream side of the l E369
_ m Report 528-0951, Rev. C j sN ,
O ' Leakage Measurement Test was performed using a blind flange fitted with a copper tube, on the downstream side of the valve, to collect air leaked. The copper tube was sub-
- ' merged in water to a depth of 1/4 inch to 1/8 inch. The upstream side of the valve disc was pressurized to 55 psig. The detailed test procedure is presented in Exhibit I. The test results are presented in Appendix B, Pages B-8 and B-11. No leakage was noted on the Valves. How-ever, leakage was noted through a small dowel hole and clamp ring bolt on the 6-inch Valve, Serial Number 82-2053-03-N-01, reference Pages B-8 and B-9. Leakage mea- -
surement testing was performed on all Valves whether or not visual leakage was evident. t C. Recording of setting and performance verification of the position switches i Levels Six-inch Actuator 24-inch Actuator
- Minimum Air 80 psig 80 psig pressure
, . Maximum Air- 100 psig 100 psig pressure Torque criteria 495 ft-lbs 7,958 ft-lbs
. (seating valve) 5.1.2.4 Test Results' l
All test results are sumarized in Table I. Motor current draw for the 6-inch motor operated Valve was recorded before, during and ! after the Static Load Test, reference Appendix B, Pages B-1 through l B-5. The operational state of the Valve (open or closed) is shown on the recordfngs. The data is expressed in current draw (amps) versus time (seconds). 5.2 VIBRATION AGING l 5.2.1 Vibration Aging was omitted in acordance with customer request, l reference Change of Procedure 2. The fatigue cycles from vibration aging are insignificant compared to the number of fatigue cycles and high acceleration levels induced during the SSE test exposure. A V E369
Report 628-0951, Rev. C O 5.3 SEISMIC TESTING . 5.3.1 Objective The objective of seismic vibration exposure was to determine the natural resonant frequencies of the Specimens and to verify the is ability of the Specimens to perform their safety-related functions when subjected to a specific sequence of earthquake simulations. 5.3.2 Resonance Survey 5.3.2.1 Orientation and Mounting .
- The 24-inch and 6-inch Air Operated Actuators were individually installed in .a test fixture and rigidly mounted to a vibration exciter. The axes definition and accelerometer locations are shown i; in Figures 2 and 3. Representative photographs of the test setups are shown in Photographs 2 and 3.
5.3.2.2 Survey In accordance with Change of Procedure 2, each Actuator was subject-ed to a resonance search in each of the three major orthogonal axes, 4 as defined in Figures 1 and 2. A resonance was defined as having a Q of 2. The resonance search was conducted at the following levels: Frequency (Hz) Level i t 2 - 12 . 0.1 inch d.a. 12 - 100; 0.75 g peak Sweep rate: 1 octave per minute. 5.3.2.3 Test Results All resonances noted are presented in Table III. An acceleration versus frequency (X-Y) plot was recorded during testing for the
, input acceleration, and is provided in Appendices C and D. No resonant frequencies were noted below 7.8 Hz for the 24-inch Air Operated Actuator. No resonant frequencies were noted below 18 Hz for the 6-inch Air Operated Actuator. A high acceleration amplifi-cation signal (27.2 g) was noted at 31 Hz in the X axis for the accelerometer located on the spring can support fixture (Accelero- '
meter Number 4). This amplification was determined to have re-
- 8 sulted from rattling and impacting of the spring on the spring can.
I This amplification does not represent a global resonance of the test specimen. Transmissibility data for the Actuators was re-
. corded with a light beam oscillograph. All oscillograph records are on file'at NTS and are available upon request.
-g-32"
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. Report ud-0951, Rev. C T
- O 5. 3. 3, Dynamic Test 5.3.3.1 The 24-inch and 6-inch Air Operated Actuators were subjected to Re-quired Input Motion (RIM) testing. The RIM test was conducted uniaxially in each axis. The acceleration levels were maintained in
! accordance with the requirements and limitations of the vibration exciter. The Resonanca Survey and Dynamics test were completed in one axis before proceeding to the .next axis, reference Change of Procedure 3. The dynamics test was completed in each of the three
! major orthogonal axes as defined in Figures 'I and 2. The orienta-tion and mounting configurations are described in Paragraph 5.3.2.1. . Provisions were included in the test setup to operate the Actuators during the test. The Actuators were supplied with 80 psig air pressure dpring the test, reference Change of Procedure 4. A l partial dynamics retest was performed on the 24-inch Air .0perated Actuator due to unmet test levels during the initial SSE test. The accelerometer locations for the retest are shown in Figure 3. The Dynamics retest was performed on a seismic simulator. The test setup is shown in Photograph 4. 5.3.3.2 Operating Basis Earthquake 5.3.3.2.1 The Operating Basis Earthquake (OBE) RIM Test was performed to sim-ulate the seismic vibration aging of five OBE earthquakes. The Actuators were subjected to two sinusoidal sweeps at 2/3 RIM levels (4.5 g), as shown in Figure 4 Test data is presented in Appendices C and D. Due to inherent capabilities of the test machine, NTS was unable to meet the OBE test level at low frequencies. Additional SSE testing was ' conducted in excess of the OBE test levels, refer-ence Figure 4 for the SSE and OBE test levels. Each OBE sweep was conducted from 2 Hz to 100 Hz to 2 Hz at a sweep rate of one octave per minute., The vibration levels were as follows: Frequency (Hz) Level 2 - 12 1.0 inch d.a. 12 - 100 3 g peak 5.3.3.2.2 One sweep, in each axis, was performed with each Actuator in the open position and one sweep was performed with each Actuator in the closed position. 5.3.3.3 Safe Shutdown Earthquake i The' Safe Shutdown Earthquake (SSE) and Mark II RIM test was performed to provide verification of the capability of the Actuators to per-fonn their safety-related function when subjected to the maximum
, dynamic vibr.ation for which they were designed. The Actuators were p subjected to single frequency sine beat tests at the RIM levels, d shown in Figure 4, plus a 10 percent margin, in each of the three major orthogonal axes. The sine beat tests were conducted at E369
Report 528-0951, Rev. C sN one-third octave intervals over the frequency range of 2 Hz to 100 Hz. The excitation at each frequency was in the form of a contin-uous series of sine beats of 15 sinusoidal cycles per beat for a minimum duration of 15 seconds per frequency. The successive beats were phased such that any superposition of response motion was additive. Additional sine beat tests were performed at all reso-nances recorded during the resonance survey where there was greater than 2 Hz difference between the prescribed 1/3-octave frequence sine beat tests and the resonance frequency. The Actuators were cycled under loads closed-to-open and open-t_o-closed, at each fre-quency during testing. A matrix showing acceleration test values - recorded during SSE testing is presented in Exhibit III. 5.3.3.4 Upon completion of testing, the Actuator: were subjected to per-formance testing as described in Paragraph 5.1.2.3. The Actuators were then visually examined for any signs of physical damage. The
- pre and post dynamic performance test results are summarized in Table I. During dynamic testing several anomalies were noted, these anomalies are summarized in Table II.
5.3.4 Static Test I 5.3.4.1 Orientation and Mounting Valves, with attached Actuators (as defined in Paragraph 1.1), were mounted in the test setup so that the Valves .would be subjected to the highest stresses in the pressure boundaries of the Valves. This test was performed on a centrifuge in one direction only, reference Change of Procedure 7. Representative photographs of the test set-ups are shown in Photographs 10, 11, and 12. The inertial loads
- 1. were applied as an equal body load throughout the structure of the l Valve and Actuator Assembly. To simulate normal operating loads, a 55 psig di f ferential pressure was applied and simultaneously
! applied with a horizontal and a vertical inertial load that was equivalent to a seismic acceleration of 4.5 g in each of the three i major orthogonal axes, reference Changes of Procedure 5 and 6. l The Gimbal Angles are shown in Figure 5. The Valves were activated using the minimum air pressure (refer to Paragraph 5.1.2.1 for level s) . l 5.3.4.2 The rotational speed of the centrifuge was increased as required, l to obtain the required acceleration level . The speed of rotation and the length of the centrifuge arm for each Assembly tested are - presented in Exhibit II. The duration of testing for each Valve
- ' was two minutes. During static load testing, each Valve was cycled from the closed to the open position and from the open to the
- closed position. Two full cyc'les were performed. Operating times
" for each Valve are presented in Table II. E369
4 Report 528-0951, Rev. A
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pg sy e-
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4
*- ' TABLE I PRE AND POST PERFORMANCE TEST
SUMMARY
Report Paragraph Reference Requirement Pre Post Pre and Post Dynamics Baseline (24-inch Air Operated Actuator) 5.1.2.1 Verify operation 7958 C-0 0-C C-0 0-C (A) ft-lb load. Air / Inlet (sec) (sec) (sec) (sec) i Pressure 80 psig. Maxi-mum Operating Time Close 96 Vac 96 Vac to Open (C-0) or Open to Close (0-C), 5 seconds. 4.5 1.5 5.9 1.9 Operate at 96 Vac (80% (reference N00 line voltage) and 120 Vac
- D-2 and D-3).
(100% line voltage). l 120 Vac 120 Vac 4.8 1.4 -- -- 96 Vac 96 Vac Retest (see note A) re- 4.6 1.1 4.7 1.1 quirements same as above.
. 120 Vac 120 Vac l 4.7 1.2 4.6 1.1 (B) Omitted, Reference C0P 1 l
! (C) Confirm above Parameters Veri fied , no Verified, no l and limit switch contin- anomalies noted anomalies noted uity.
- NOTES:
A. A partial dynamics retest was conducted on May 4, 1983 to perform reso-nant frequency dwells at certain frequencies that were omitted during the initial Dynamics Test and to repeat sine beat tests at certain O frequencies where the required acceleration level was not achieved. Pre and Post Baseline Tests were repeated as insufficient volumetric flow was supplied during the initial baseline resulting in erroneous The data. E369
Report 528-0951. Rev. A 3 TABLE I (Continued) , PRE AND POST PERFORMANCE TEST
SUMMARY
Report Paragraph Reference Requirement Pre l Post Pre and Post Dynamics Baseline (6-inch Air Operated Actuator) 5.1.2.1 Verify operation 495 ft-lb C-0 0-C C-0 0-C (A) load. Air / Inlet Pressure (sec) l (sec) (sec) (sec) 80 psig. Maximum Opera-ting time Close to Open 96 Vac 96 Vac (C-0) or Open to Close
, (0-C), 5 seconds. Operate 1.2 1.5 1.2 1.6 at 96 Vac (80% line volt-Age) and 120 Vac (100%
line voltage). 120 Vac 120 Vac 1.2 1.5 1.2 1.4 O' . (B) Ommited, Reference C0P 1 (C) Confirm above parameters Veri fied, ex.- Verified, ex-and limit switch contin- cept all opera- cept all opera-ui ty. - tions performed tions performed with a 318 ft- with a 318 ft-lb load instead lb load instead of the 495 ft- of the 495 ft-lb load, Refer- lb load, Refer-ence N00 D-4 ence N00 D-4 O E 369
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m Report 528-0951, Rev. A sN . 6
- . TABLE I (Continued)
PRE AND POST PERFORMANCE TEST
SUMMARY
Report Paragraph I. Reference Requirement Pre Post l. Pre and Post Static Baseline (6-inch Motor Operated Valve) l 5.1.2.2 Verify operation 55 psig C-0 0-C C-0 0-C (A) differential pressure 368 (sec) (sec) (sec) (sec) t10 Vac, 3 phase, 60 Hz (80% rated voltage) Max- 5.2 4.8 5.5 5.5 l imum Operating time Close (ref. NOD D-9) (ref. NOD D-9) to Opn (B) Seat Leakage Test No leakage noted No leakage noted l
^
[ * (C) Record data during opera- , tion in (A): -
- 1. Test Voltage 372 Vac 372 Vac
- 2. Motor running current Reference Reference drawn during operation Appendix B Appendix B
- 3. Motor current drawn at 4.6 amps 6.1 amps l
time of opening of torque switches at torque seated valves recommended settings.
- 4. Perfomance verifica- No anomalies No anomalies tion of torque switch- noted, Refer- noted, Refer-es and position ence Appendix B ence Appendix B switches 1
- E369
e m Report 528-0951, Rev. A sN . .. O TABLE I (Continued)
. PRE AND POST PERFORMANCE TEST
SUMMARY
Report Paragraph Reference Requirement Pre Post Pre and Post Static Baseline (6-inch Air Operated Valve) i 5.1.2.3 Verify Operation. 55 psig C-0 0-C C-0 0-C (A) differential pressure. (sec) (sec) (sec) (sec) Air / Inlet pressure 80 psig Maximum Operating time 1.7 1.5 2.5 2.5 Close to Open (C-0) or Open to Close (0-C), 5 seconds l l (B) Seat Leakage Test 27 bubbles in 4 25 bubbles in 4 1 minutes (1.01 minutes (1.0 cc/ min) cc/ min) C . (C) Performance verification of Veri fied Veri fied , torque switches and posi-switches Pre and Post Statics Baseline (24-inch ir Operated Valve) 5.1.2.3 Verify Operation. 55 psig C-0 0-C C-0 0-C (A) differential pressure. (sec) (sec) (sec) (sec) Air / Inlet pressure 80 psig Maximum Operating time 5.2* 1.2 5.2* 1.1 Close to Open (C-0) or
- Refer-
- Refer-Open to Close (0-C), 5 ence ence seconds N0D N00 D-12 0-12 (B) Seat Leakage Test No Leakage Noted No Leakage Noted (C) Parformance verification of Veri fied Veri fied torque switches and posi-tion switches O .
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'_ NeGene Report 528-0951, Rev. A 7
s ,.e TABLE II SEISMIC TESTING PERFORMANCE
SUMMARY
(DURING DYNAMICS TEST) Report Paragraph Reference Requirement Performance Description 24-inch Air Operated Actuator 5.3.2.2 Resonance Survey
- 1. Identify resonant frequen- 1. All resonant frequencies are cies between 2 Hz and listed in Table III.
100 Hz
- 2. If resonances are noted, resonant dwells shall be 2. Resonant dwells were per-
. performed as described for formed at the following SSE sine beat tests, frequencies:
reference C0P 1. 17*, 22*, 31* 7.8, 24.5 41*, 44*, 60* 26.5, 38*, 72*, 80* 47*, 78, 87*
.Z_ :
I - 11, 12, 19* 27, 28*, 37*, 55*, 75*, 99
- See Note A
- NOTES:
A. A partial dynamics retest was conducted on May 4,1983 to perform reso-nant frequency dwells at certain frequencies that were omitted during the initial Dynamics Test and to repeat sine beat tests at certain frequencies where the required acceleration level was not achieved. Those frequencies marked with an asterisk (*) were performed during the partial dynamics retest. E u,
Report 528-0951, Rev. A A ,
, O r- TABLE II (Continued) , ,. SEISMIC TESTING PERFORMANCE
SUMMARY
(DURING DYNAMICS TEST)
't Report Paragraph Reference Requirement Performance Description 24-inch Air Operated Actuator 5.3.3.2 OBE -
- 1. During one frequency sweep 1. Verified, no anomalies the actuator shall be in noted. Two sweeps per-the open position and dur- formed from 2 Hz to 100 ing one frequency sweep, Hz to 2 Hz; 1 octave / min.
the actuator shall be in the closed position. 2. The test was ~ performed at ! the nominal requirement.
- 2. The OBE RIM levels shall The 10 percent margin was
()
. be the nominal requirement not included, reference plus 10 percent. N00 D-6.
i, t I O 33s,
( U m Report 528-0951, Rev. A sN iA TABLE II (Continued)
,U SEISMIC TESTING PERFORMANCE
SUMMARY
(DURING DYNAMICS TEST) Report Paragraph Reference Requirement Performance Description 24-inch Air Operated Actuator 5.3.3.3 SSE
- 1. Perform sine beat testing 1. The following sine beat at 1/3 octave intervals frequencies (Hz) were used from 2 Hz to 100 Hz, at in each axis, as defined 5.0 g peak,15 seconds per in Figure 1: 100, 85.3, I beat (minimum),15 oscil- 64.0, 53.3, 42.6, 32.0, lations per beat, 50 26.6, 21.3, 16.0, 13.2, milliseconds between behts 10.6, 8.0, 6.6, 5.3, 4.0, (depending on the frequen- 3.32, 2.66, 2.0 (see note cy), reference COPS 3 & 4. B,below) 8
/m b *
- 2. The Actuator shall be cycled close to open and
- 2. No anomalies were noted in the X and Z axes, open to close once per frequency.
5.3.3.5 Post Examination Except for the items describ-ed in N0D D-1, no other evi-
- dence of adverse effects was noted. Continuity of position switches was verified during testing by indicator lights.
No anomalies were noted. l NOTES: 1 B. On . completion of SSE testing in the Y axis, the junction box mounting had loosened and the gasket between the air cylinder and Actuator housing had dislodged, reference Notice of Deviation D-1. The junction box was re-secured using commercial grade bolts,1/2 inch shorter in length than the i original bolts. The original bolts were too long and bottomed out before tightening the junction box mounting to the Actuator housing entirely. This change will be addressed as a design requirement. The tie rods loosened - D due to loading and unloading of the tie rods, resulting from their inherent
\ natural. frequencies. The tie rod bolts were re-torqued to approximately 130 foot-pounds, reference N00 D-1. This operation shall be addressed as a maintenance requirement.
$369
', Report 528-0951, Rev. A sN ib V) TABLE II (Continued)
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SEISMIC TESTING PERFORMANCE
SUMMARY
., (DURING DYNAMIC TEST) Report Paragraph Reference Requirement Performance Description 24-inch Air Operated Actuator (Retest) 5.3.3.3 SSE
- 1. Perform sine beat testing The following sine beat test at 1/3 octave intervals frequencies were repeated due from 2 Hz to 100 Hz, at to insufficient acceleration 5.0 g peak,15 seconds per levels:
beat (minimum),15 oscil-lations per beat, 50 Y Axis Z Axis j milliseconds between beats (depending on the frequen- 10.6, 16.0, 16, 21.3, cy), reference COPS 3 & 4. 53.3, 64 85.3 The following dwell frequen-cies, omitted during the intial phase of dynamics testing, were perforned: X Axis Z Axis 17, 22, 31, 19, 28, 37, 41 (C), 44, 55, 75 60, 72, 80 Y Axis 28 (D), 47, 78.5 NOTES: C. On completion of the 41 Hz run in the X Axis during the SSE retest, the gasket between the air cylinder and Actuator broke in several places and dislodged from its seating, reference N0D D-10. The customer was notified and the customer instructed NTS to continue the test. No Actuator mal-function was noted. f) D. During the axis change from the Z to the Y axis, the copper tube connecting V the regulator filter assembly to the solenoid valve was inadvertently dam-aged. Before running the sine beat tests in the Y-axis, an air leak was E369
m Reoort 528-0951. Rev. A Teeweses sm
.O' noted in the copper tube fitting to the Solenoid Valve. In accordance with customer request, the test was continued. After sine beat testing at 10.6 .
- . Hz,16 Hz and 38 hz, in the X-axis, the copper tube sheared off at the Solenoid Valve fitting, reference N0011 and Photograph 13. The test was l interrupted and the copper tube and fitting were replaced, in accordance
.. with customer request. The sine beat tests in the Y-axis were repeated. l No anomalies were noted during the Y-axis retest. i
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l l I l l l l i i 1 I l lO E369
a Report 528-0951, Rev. A meeuw 7
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- TABLE II (Continued)
' SEISMIC TESTING PERFORMANCE
SUMMARY
(DURING DYNAMIC TEST) Report Paragraph Reference Requirement Performance Description 24-inch Air Operated Actuator (Rotest)
- 2. The Actuator shall be 2. No anomalies were noted cycled close to open and in the X and Z axes, open to close once per After the copper tubing frequency. was replaced (see Note C) in the Y axis, no anom-alies were noted.
l 5.3.3.5 Post Examination No adverse effects were noted. ' Continuity of position switches was verified by indicator Os -
~
lights during the test. No anomalies were noted. I O S w.
Report 528-0951. Rev. A TABLEII(Continued)
.' SEISMIC TESTING PERFORMhNCE
SUMMARY
(DURING DYNAMIC TEST) i Report Paragraph Reference Requirement Performance Description 6-inch Air Operated Actuator 5.3.3.2 Resonance Survey
,, 1. Identify resonant frequen- 1. All resonances are cies between 2 Hz and presented in Table III 100 Hz
- 2. If resonarces are notad, 2. Resonant frequency dwells '
resonant deweels shall be were performed at the performed as described for following frequencies:
'i SSE sine beat tests,
. . reference C0P 1. Y Axis X Axis
- 24, 74, 88 20, 14 Z Axis
. 18, 74, 87, 95 OBE 5.3.3.2 1. During one frequency sweep Verified, no anomalies noted.
the actuator shall be in Two sweeps performed from the open position and 2 Hz to 100 Hz to 2 Hz; i during one frequency 1 octave / min. l sweep, the actuator shall be in the closed position.
- 2. The OBE RIM levels shall 2. The test was performed at be the nominal requirement the nominal requirement.
plus 10 percent. The 10 percent margin was not included, reference N00 6. (See Note E, next l page).
- Further analysis of data indicated that no resonances existed at these frequenci es. The dwells were conducted for conservatism at the time of test.
E369
R2 port 528-0951, Rev. A sN 4 4 NOTES: [ r E'. During the first OBE frequency sweep in the Y-axis, the copper airline be-tween the cylinder and the ASCO valve broke inside of the fitting, refer-ence N00 0-5 and Photograph 5. The Actuator copper airline was replaced by a shorter line directly connecting the filter / regulator with the solenoid operated pilot valve, reference Photograph 6. The OBE frequency sweep was re-started. During the initial OBE retest in the Y-axis, the copper pipe i connecting the air cylinder to the ASCO Valve sheared off at the interface to the air cylinder, reference N00 D-7. A steel pipe was installed as shown l in Photograph 6. At the completion of the first OBE frequency sweep, the steel pipe sheared off at the same location as the copper tube, reference N0D 8 and Photograph 8. A commercial grade stainless steel pipe was in-stalled as shown in Photograph 9. The stainless steel nipple length shall not exceed 1-1/2-inch. The gauge shall be 1/8-inch. The OBE RIM level test was repeated in the Y-axis, no anomalies were noted. The stainless steel pipe shall be addressed as a design requirement. The test sequence was Y axis, X axis and Z axis, as defined in Figure 2. No anomalies were noted in the X or Z axes. oO
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l l l l 0 E369
, - . . = .
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. Report 528-0951, Rev. B sN
- . 0 -
TABl.E II (Continued)
;, SEISMIC TESTING PERFORMANCE
SUMMARY
(DURING DYNAMIC TEST) Report Paragraph Reference Requirement Performance Description 5.3.3.3 SSE
. 1. Perfonn sine beat testing 1. The following sine beat at 1/3 octave intervals frequencies (Hz) were used from 2 Hz to 100 Hz, at in each axis, as defined 5.0 g peak,15 seconds per in Figure 2: 100, 85.3, l beat (minimum),15 oscil- 64.0, 53.3, 42.6, 32.0, lations per beat, 50 26.6, 21.3, 16.0, 13.2,
, milliseconds to 1210 10.6, 8.0, 6.6', 5.3, 4.0, millisecoiids between beats 3.32, 2.66, 2.0 (depending on the fre- !, quency), reference COP's 3 and 4. . , . 2. Additional resonant fre- 2. Resonant frequency dwells: quency dwells
,: Y Axis X Axis
- 24, 74, 88 20, 14
. Z Axis l
18, 74, 87, 95
- 3. The Actuator shall be 3. No anomalies were noted.
cycled close to open and open to close once per frequency. 5.3.3.1 Post Examination No evidence of physical damage was noted. Continuity of posi-tion switches was verified by indicator lights during the test. No anomalies were noted.
- Further anlaysis of data indicated that no resonances existed at these f requenci es . These dwells were conducted for conservatism at the time of test.
E369 __._.._-._-.__.__.n.____
Report b28-fl951, Rev. C
$seme i
O TABLE II (Continued) SEISMIC TESTING PERFORMANCE
SUMMARY
(DURING DYNAMIC TEST) i Report Paragraph Reference Requirement Performance Description
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STATICS 4 6-inch Valve with Air Operated Actuator 5.3.4.2 1. The Valve shall be sub- Cycle 1 Cycle 2
., jected to two full cycles.
, One cycle is from the C-0 0-C C-0 0-C closed to the open to the (sec) (sec) (sec) (sec) closed position (C-0-C),
80 psig, 55 psid, refer- 2.S 2.5 2.5 2.6 ence C0P 6 and 7. 6-inch Valve with Motor Operated Actuator 5.3.4.2 1. Same as above, (Two full
- cycles C-0-C)* 6.0 6.0 6.0 6.0 l l 24-inch Valve with Air Operated Actuator
,i 5.3.4.2 1. Same as above (Two full cycles C-0-C). 5.0 1.0 5.2 1.1
- Motor current draw during each valve cycle is presented in Appendix B, l Pages B-3 and B-4. Limit switch operation was verified with the use of l indicator lights. No anomalies were noted.
1 ,f f E369
Neuensi Reoort 5?8-0951. Rev. A Teenmeel Systems
. O TA8LE !!-A TEST SEQUENCE 1
6-Notices of Changes of , Date Date Deviation Procedure l-Started Completed Test Test Article (N00) (COP) : l 3/15/83 3/15/83 Baseline 24" Air Operated 1 Actuator l 3/11/83 4/1/83 Dynamics 24" Air Operated 0-1,0-6 3 i Actuator 4/1/83 4/4/83 Post Dynamics 24" Air Operated D-2,0-3 (retest) Baseline Actuator 4/13/83 4/13/83 Baseline 6" Air Operated D-4 Actuator l 4/13/83 4/19/83 Dynamics 6" Air Operated D-6,0-7,0-8 3,4 ! Actuator ; 4/20/83 4/20/83 Post Dynamics 6" Air Operated D-4,0 5 - Baseline Actuator ; 4/27/83 4/27/83 Static 6" Valve, Air ! Baseline Operated Actuator' t I 4/28/83 4/28/83 Static 6" Valve, Motor Baseline Operated Actuator j 4/28/83 4/28/83 Static Load 6" Valve Air 6,7 I Operated Actuator l 4/29/83 4/29/83 Static Load 6" Valve, Motor D-9 l Operated Actuator 4/29/83 4/29/83 Post !tatic 6" Valve, Air
- Baseline Operated Actuator 4/29/83 4/29/83 Post Static 6" Valve, Motor D-9 Baseline Operated Actuator 5/4/83 5/4/83 Baseline 24" Air Operated D-10,0-11 (Retest) Actuator l
5/4/83 5/5/83 Dynamics 24" Air Operated l (Retest) Actuator 5/5/83 5/5/83 Post Dynamics 24" Air Operated Baseline Actuator (Retest) 5/6/83 5/7/83 Static 24" Valve. Air Baseline Operated Actuator-5/7/83 5/7/83 Static Load 24" Valve, Air D-12' Operated Actuator 5/7/83 5/7/83 Post Static 24" Valve, Air Baseline Ooerated 8ctuator' d l . 33,
,,,,, Report 528-0951, Rev. A T nm.m sr.w=. .O TABLE III RESONANCE SURVEY RESULTS l
Resonant Input Frequency Response Accelerometer Acceleration (Hz) Axis of Vibration Levels (g peak) l 24-inch Air Operated Actuator l Z Axis ,
#2 #3 #4 0.1 inch d.a. 11 1.0 1.0 4.0 0.75 g peak 12 1.6 1.13 5.7 0.75 g peak 19 1.6 1.13 6.5 0.75 g peak 27 1.0 2.18 4.5 0.75 g peak 28 1.7 2.0 7.5 0.75 g peak 37 1.0 4.1 10.4 0.75 g peak 55, 1.0 1.4 3.33 0.75 g peak 75 1.0 0.66 2.8 0.75 g peak 99 1.1 0.44 2.8 X Axis #2 #3 #4 0.75 g peak 17 1.71 2.23 5.9 l
0.75 g peak 22 1.28 5.37 3.14 l ' 0.75 g peak 31 1.6 2.40 27.2 O.75 g peak 41 1.42 1.14 11.5 0.75 g peak 44 1.32 0.73 8.8 0.75 g peak 60 1.0 0.80 3.0 _0./5 g peak 72 1.28 0.93 4.6 0.75 g peak 80 1.2 1.2 6.0 Y Axis #2 #3 #4 0.1 inch d.a. I.8 0.6 1.4 2.4 0.75 g peak 24;5 0.95 0.95 12.9 0.75 g peak 26.5 0.66 1.4 3.0 l 0.75 g peak 38.0 0.88 1.88 2.22 0.75 g peak 47.0 1.54 1.54 12.0 0.75 g peak 78.5 1.42 1.42 4.8 0./5 g peak 87.0 I 1.70 1./0 5.6 6-inch Air Operated Actuator I Z Axis #2 #3 #4 #5 0.75 g peak 18 1.26 0.86 5.71 4.43 0.75 g peak 74 3.25 10.0 5.25 7.0 l 0./5 g peak 87 1.17 0.66 4.83 3.33 1 0.75 g peak 95 1.25 2.25 5.75 4.0 l X Axis #2 #3 #4 #5 l 0.75 g peak 87 1.5 2.75 1.0 1.5 Y Axis #2 #3 .#4 #5 s 0.75 g peak 24 0.91 1.08 10.16 6.58 0./5 g peak 74 1.0 0.86 1.86 2.86 0.75 g peak 88 1.30 0.85 2.07 2.15 4
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, to the mounting point of the test specimen $
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3 E l
Reoort 528-0951, Rev. C Y O' i e_ N I N' T
^
l b l Accelerometer #5 was k located adjacent to I the mounting point of the test specimen and was used to con-trol input vibration 5 OU N _ Spring Can
# :l A response accelerometer was placed on the spring i can to measure accelera-tion levels at the fixture support.
i Actuator
, 0:=} @,/ NOTE:
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' Actuators ANALYSIS BAND N/A EVENT OBE D SSE 3 .
- Capabilities of test machine NOTE: Actual SSE Test levels I included 10% margin.
FIGURE 4 Required Input Motion
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12 > NM l TEST SPECIFICATION A)Td OYb S23-b9N I REV M PA R A. NO. 7.3.4 TEST TITLE bih $ C. bunlibCd_Nem Tesdin c, l J CHANGE REQUESTED NP- SeI&th C- \ de% -E leve l 5 S ba l l mee.t or e x c.e.e cl % e. n n yw i no- I re a n l,- % #m L leve is nfus A n ere ow4 n,etro,n. Th.o ' rn o reouicewen+ C.r r I O 0 V foc th e_ SS E +s+ Rim will b e a_ n, i n n, a m of is SecnnAs o e. c hau + +cn Th e- a c-ho 4ncs m hn i I b e equipp J l U .J () Il to in a comoriale_ acea ssori es: du r-i n c, Je s-i-1n c, . Th e. 18 i , J J nc -k a4ncs s hn l \ 6 e 's o an 1:e <4 uM I, %n as;o ai r acessure . Ir I 3 i REASON bhanceS re E kC, debe b6n O[ M S b OroudWR J e m acc ordctnca toil-1, Me reo u i emp r +s of IEEE 3?? - 0 193O(Re b we# UTS le b 40 Jn k r - s h kims - aRoched) J C O P. INITIATED BY F - [ OF (Company) N CUSTOMER NOTIFICATION MADE TO dhnnu -- d e n k ihS HOW FN P J DATE AND TIME Fe brua ru 16.19K3 BY maek A Sm ,VI, J ! APPROVAL CUSTOMER REPRESENTATIVE b LN - (- b- "~~'C NTS ENGINEER lO/l k - # NTS QC M l } DCAS NOTIFIED: Yes O N/AM 49 DATE M-/d ~8 b Q393
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s , _ - - N Nationsi Scientific 26525 Gcicen Valley Road v Technical Services Saugus. California 91350-2680 systems Group Tel: 805 251 6622 February 16, 1983 Patel Engineers _ t 3400 Blue Springs Road, N.W. ! Huntsville, Alabama 35810 Attention: Johnny Jenkins
Subject:
Seismic Testing for Bechtel Limerick (Bechtel P.O. 8031-P-144-
. AC), NTS QTP 528-0951.
Dear Mr. Jenkins:
Per our conversation of February 15, 1983, I am responding to Bechtels com-ments as an addendum to NTS QTP 528-0951: Item 4a) .The NTS final-test ' report shall list the valves by Bechtel tag number in order to document that-the valves tested are same as those sup-plied to the Limerick project. Item 4b) The NTS final report shall be prepared in accordance with sec-tion 6.2 of specification 8031-P-358. The final report shall include the " Dynamic Qualification Report Cross Reference Form" per Figure 1 of 8031-P-358. . Item 4c) The acceleratiion tolerance of 10 percent applies to vibration aging only and no longer applies s.ince this req)1rement has been dropped.
- Seismic (RIM) test levels must meet or exceed the nominal requirement 1evels plus ten percent margin. The time requirement for the SSE RIM Test will be a minimum of 15 seconds as indicated in Paragraph 7.3.4.3 of NTS QTP 528-0951.
Item 4d) No additional comments. Test will be performed at 80 psig. - Item 4e) Not applicable since vibration' aging has been dropped. O
1 r-q -
.t O Page 2 i
February 16, 1983 I E i Item 4f) NTS shall place response accelerometers on the test device at points most likely to demonstrate resonance and on the fixture adjacent to the mounting of the equipment. Resonances shall be identified as a Q 2 2.0, defined as the ratio of the device dynamic response to the input " acceleration. The input response is measured at the fixture accelerometer to minimize the effects of system / fixture natural resonances. Item 49) To simulate normal operating loads, a 55 psig differential pres-sure shall be applied simultaneously with both a horizontally-applied and a vertically-applied inertial load that shall be equivalent to a seismic - acceleration of 4.5 g in each of the three major orthogonal axes. Item 4h) The actuators, with' appropriate accessories attached, shall be . subjected to Required Input Motion (RIM) testing. Item 41) NTS concurs with the Clow, Patel, and Bechtel agreement that this requirement constitutes additional ~ scope of work which is not en- ~ veloped by the present contract. I hope that this addendum satisifies the Bechtel comments that you submitted. Please phone me if 'you should have any additional questions or comments. Sincerely, W )an k / . % +b Mark A. Smith Nuclear Programs Manager MAS:ss 1 O
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CHANGE OF PROCEDURE - CUSTOMER C1 h b OfiMS MJO NO. <-Nb~ODl Inoice and.Ae 'Operak.d PART NAME Acbm M hd do lues { .O. NO. PET- A220 PART NO. LL l'TEMS $'05 e o p no_ y
- d. Ibb3 SERIAL NO. DATE
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TEST SPECIFICATION M .528-0951 REv A PARA.NO. T. O TEST TITLE 'Id. S %E.pFk CHANGE REQUESTED %e W$ fino l M re Oork 9 hn 1l MA ndTu %e., 1 J vnives bu Bech4e.l Tao du m her, m cc mn I co m c4 J J be n,-e oace_A i a n eeneda nce un&k Paraa ra ck G.2 O c kn l'l r i a i o-r behel SnecWienkc i n Bos I - P- 358 The fino I roonc+ s hn it ine lo de & " D o na m'i t CD ua l;Rea Mc n i J Reaoct Cmss L Geeneo Foc m" n o c. Fio o re I cf 90 1 - P - vR - R e f. o. SzA w 52 s (.-<a pb) @Mb c. REASON W *. O nCu m'w h rh n%htYuh% de An; Alr n 6$ ExiSbo nn J Arrs non1C?ce k n 4s-/- n ncedu re n u m her 52R-695i)
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s. oyuw.6 mcarAun cu[ -i-35g e FIGOBE 2l i DY"aMIC QUAZ.ZFluyggs agy0RT CROS5 AITEREleCE FO8et . I f- Page me. (s1 213E in se m i ERA \ t
- 1. Report me.EAO'OiGI .
A , gg n wie fir 3 gg , i 69+4e-[fy ulve.s '
- 2. aquipment/ system faaetional name ak4 Ac4va+= 3 Tefle .rg,.I
- 3. Pershame Order us. PCE
- T2Zo , 3 ,, _ - 3 )
- a. Certifiestions signed by an authorised company officer, that .. .-
the equipment meets the eynamic requirementa. L6/"' l S. seisnie gealification specification used . pr5 r8' 52 8-o 1Tl, lt**^ 3 spectrum oneve mood (Figsze so.): 4 3I 6. I
- 7. Origia of dimensions, loads and metesial propertise (esgs.,
3 eposs. , codes, etc. as applicablel uvs rp 62*-ogrl jd e* *
,\
S. Equipment is asock item } u 4wM Os.
- i, as
.s.
;...h eAM ..am s
3> s __ j
- 9. Equipment is gus11fied by aanlysis , testing y, '
er comoimation
- 10. schematic sketch of the oneplete amit. 27 /2e,4o l
- 11. Description of method of operation and conssel of equipment. 5'~ i
- 12. Criteria for behavior enring a seismic event including -
3 _ ., operating and seiscic land cossimation. I
- 13. codes, etandards and specifications and the eatent of their compliance when qualifying equipment. T.F rzc- cifi, fee #" 13 1s. Effects of equipment annanting assumed La analysis er used duriaq testiaq as compared to actual asunting. Tu Seevice f" 'I et,u om o usu"C O lJ[4 15. Qualification by Analysie V/A
- a. Description of the analytical apprese (such as mathematical model, rigid = fleaible system, etagle er unitidegree of freedom system, eta.) . #[A
- b. Damping factere moed in the analysis. 9/A
- c. Justification for use of damping facters other than those permitted by seismic goalification requirements. W /h
- d. Deseriptism and voirification of competer programs need. _
AJ /A sammary table showing competed 03E and sat stresses and deflections for operating, seismic and combined conditions for equipeens ecungonents and anchorage . onoponents, compared with allowahle stresses and N[A deflections.
- f. Reactions at egelpment supports. '. u/A
- g. meterial designation (As;M, etc.) for egeipment componente considered in analysis. #4
- 14. Qualification by Testing /
- a. Description of the testing approach (such as biasial tee tiaq , sismiated plant operation, teasing frequency range, frequency intarvel, type and frequency of wave form Laputs, etc.) S, -
9
-52A-R"Y" O
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.- o SPScifid icn 8031-P-358 e
Page No.Iss
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Summary taal, of equipment reement frequencies as e b. determined egeramentally by saanntag includarig sne b, / 21 input acesierations, sad ampLificatasm factors.
- o. netnod of monitoring and ionations of smalters during 2S 1130i
' testang of equapeemt. IL 1 N *'s J /
- k. Functioning of equipsent during and after sosting.
Test response spectra (Tps) shown to equai or eseeed l0
' c. required reepanse spectsa (Ass:.
d[. Justification Lf other tasa $1 damping factors Ng are used for RAS and TRS. T8 *
- g. Name and location of testing facility.
9 /A I[' combined qualification methods jsstification. , e 6 e f G e e
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DCAS NOTIFIED: Yes O N/Ak DATE g393
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CO P. NO. TEST. SPECIFICATION A/Ts OTP MA-095/ Rev 4 PARA.NO. 7.31 TEST TITLE Mad [C- YdSb CHANGE REOUESTED Th e- va lue Inneradnr a sun, hlies c ho 11 be shabic 4es 'ed
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1 hN \ i r i n b) NOTICE OF DEVIATION ! 1 CUSTOM ER O b. bnMr n ci S&9 MJO NO. 519 ~~ d 3 I I PART NAME be di5 AI r- Mcbabr(2- P.O. NO. EN-622O PART NO. M l 24 NOD NO. D-I /s Paor i o f 2. /\ O SERIAL NO. b2~SO '! DATE M C' f'c k 3I , l9 b 3 TEST SPECIFICATION MTS C7FP 52.8 -09 5 I REv. A PARA.NO. 73MM TEST TITLE D u n d_ m IC. Yes b vm ORIGINATOR b r~f1 C 6 lA )be J J REQUIREMENT: 'Ib E- QC d -[OFS 9bd / / he U.I W Q [/u eyd N [ nec/ [c( _ J cig4errocal,cn.
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_ iOMER NOTIFICATION: Made to: an //f!fth1 How: d!ddOL
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' ART NO. M l 24 NOD NO. O- 3 SERI AL NO. b -9O M -I DATE Aort ! 4 19 M
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3 SERIAL NO. b2"'9b29~b DATE MDrt I t1 . 19F;3 TEST SPECIFICATION 52S'b9bI REV. PARA.NO. 7 3. 4 4 TEST TITLE b%am C TI*A b ORIGINATOR MA ek M beIb ' d REQUIREMENT: OAME 45 N/ __ EVIATION: Od M e 43 I- _ OISPOsITION: %e- CInnnDS r'* Or M E H b r A n E M rn YiL% W d'TCG*!irhR Q l J
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/ (NTS QC) (Customer Representatrvel CUSTOMER NOTIFICATION: Jgg Jp [ Q O )to: How:
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USTOMER NOTIFICATION: ace to-Y hllG en DOV h How: Y0f 0$'
)
Date & Time: M Or-I l i l4_1999 By: bdFk M M' DCAS Notified: Yes O N/Ag (2 4 k '- Mi 1 oare / "'S **'5""*""' E n5
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, CUSTOMER a h PDFki' S MJO NO. 5M"b9bI i
PART NAME bebS Mr MCb or h P.O. N O. EU ~ erb PART NO. 4I04l NOD NO. O- 7 _ SERIAL NO. U"90d' b DATE M,Dr[ / /4, N$3 TEST SPECIFICATION AJ75 G7F 5.28- 605/ REv. A PARA.NO. 7 S.4 TEST TITLE Ou r,a rw !c /ese ORiOINATOR m<, ck A 19n.,;w, J REQUIREMENT: NR OC- O Slio // bE- S h b ld C b M M /Yo h osv [C U J
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,- REOUIREMENT: e OC bin Y Rbd ll be Sl' b Ie C bf N Y N o *ma inn lr-kst%c, A>,u slav.s n-P oh u<iro I ek$n,n ca-_ er- dl+u,cco+un r v J /
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y SERI AL NO. 8 Q ~Cc TJ ~ 0 2 -^2 -o r '3D ~Poo - DATE 6'* 2 P ~ & 3 i V b S S Y'$ W TEST SPECIFICATION A'73 <~29-09c/ WA ._. REV. A PAR A. NO. Ir /,2, / N TEST TITLE AdII-owd A'e/e vec'M < ORIGIN ATOR f emM7 7-#+'/2 4 AL-REQUIREMENT: JA LM r M i^/L t)C t*PGM,N A Mn tm u es 7/ m 2 WAo L 15 5 pien <,ro&Dr DEVIATION: M A*S Y M7/C O A !2 '=un'L 7/ r^/G i- Unt-- vr= nh'av^ '6 FA'h
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Date & Time: /u M V- 'i. 9 - ? 2 By: C C n a N r v - # r > /2 u I dfk M !fI DCAS Notified: Yes O N/A[ OATE
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[ NOTICE OF DEVIATION CUSTOM ER ATb b NN2 M MJO NO. 50 2 -@ C PART NAME NS SIR b@AD A b J'/ P.O. NO. PART NO. N 9 / M N NOD NO. ~/b SERIAL NO. b k OS ~~! DATE 8 !Y T3 TEST SPECIFICATION HTS O.rP 6.7 F-OW/ REv. A PARA.NO.2 S- bI TEST TITLE Yd AM IE DRTiM b ORIGIN ATOR tc M AMD MrO 4M REQUIREMENT: Ef b'E w WC 7 A S I4R"$D 14 GEo 06 s . P. 9, ). 3 .9. 3 8 i,0 r hr- @ s !4 o cT "O niMU aLS, Fa.o rn 24a To toola t TeSos A <s T- DOE LL's _ _ DEVIATION: 0t CornM6 TIC M O F 1/l # ;L eSiee REAT'- X-AX#_s i T was NON $43hT %W GED SIR OY liOT E (L 4 ACTu C1 Toft L) A S TSv0Gn a u. T~ od VIEC $ DISPOSITION: O(A9 Y<9 M d dAS A C SQ t. OE SAAke.t 4 NEOLdTeh D & T/*)Gd RT R EVIEW: #3 ~b APPROVAL-(NTS oci (customer aeoresentative, CUSTOMER NOTIFICATION: ['] to: AbMC 2AOIDhD How: OfR2 ah i10 TEhD
%.)
Cate & Time: 5/v/s3 Ic.c o u a s sy.% ums ut DCAS Notified: Yes O N/A 2 OATE , NTS Dept. Supervisor g 395
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M~ DATE NA .- TEST SPECIFICATION - . C. bN -'03 bI REV. A PARA.NO. 9.b .3 TEST TITLE Y 4MLEIEAN M ORIGIN ATO O N4 2b ~$<94 b REQUIREMENT: E2bdM AS T M MO I4 M No dG"' T h. 2 5.0 3 ,. cSitO R 3 GATE @ $8 OC'7' ju7Eitt/4LL Yrto m .2 na -rb t oo. _4_. 4- VAS ON A W TOELCS . h - DEVIATION: I I SIC . f M T2) 375NE c:5 r >r 8 Ear % A 7:.s.s Co PPen CuS E e4 __ A IG CYLa d'E>ee. EksQ o C f-- e co a e ak . DISPOSITION: Ou e T- WAs QQA W o @ 7eRLgw TE.m c. +-W % T h ETA E
& NEPeAT- V AXs% S w rle%% O vr. ~~Sshr.A e s "T'u~ "RE wAS Game 66b cDtAQ_ rs 0 C A X. l$ C M A C 6. I. Ce mOLCTid oC X+4 AX e 4 l~u'% F '2)h A oT /,4 A V 74.tooTD Y aX.t R % 7- % R E t~/ g L;roLB C .
R EVIEW: M-Od APPROVAL: (Customer Representative) (NTS QC) CUSTOMER NOTIFICATION: e to: S E Ad 8DSO M How: UEE & [so7eaceD Date & Time: IbN3 I IIO N 4 By: 2tMC Dial DCAS Notified: Yes O N/A2 DATE NEQ mA NM Ceot. Suprvisor g
,g7,
hbY NOTICE OF DEVI ATION g
- USTOM ER - ,Mlf M MJO NO. ~O N PART NAME I 8JfM M IMfd bf P.O. NO. bEI E22 O
,.A R WTtib-SR4-Sf j N/2 NOD NO. b) ~ b
;ERI AL NO. D ~ k80 Y~/ DATE $ l TEST STECIFICATIONYT [MI"OTII REV. PAR A. NO. 7. /. 2 8 -
EST TITLE l CAllMd JM/ O ORIGINATOR ' US ' IEQUIREMENT: # t/d/L/# M h/Ifa Bf <*/A,f f pu Mg e7/gj[ T d tf/%ded
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)lSPOSITION: f Ina (1)d.T /*S7)bn/Jed W P12X&gf* jr7ktsekt
./ /
A r HEVIEW: 9 APPROVAL-
# (Customer Reoresentativel
[/ (NTS QC)
.USTOMER NOTIFICATION: < b: dM M/ # How: Y al Oa & Time: O /7 /33 Bv: Add / 6Md )CAS Natified: Yss O N/Ak ,_// 9hd ,, , _
. _ . _ _ . _ . _ . . _ _ _ _ _ . . _ . _ _ _ . . . _ _ _ _ . _ . = _ . _ .
a i.. li { m Teennsees Report 528-0951 l
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4 9 l t i G 4 I
- i. e -
- APPENDIX A
. EQUIPMENT LIST ,
h l 1 1 i, s
- 8 i
i i E f i- - . t 4 + .I
- I
} l 4 IO I e t 336, ; l . I ,
Report 528-0951 y
.- syn -
PRE AND POST BASELINE 24" AIR OPERATED ACTUATOR NTS Number E1345S Instrument Digital Multimeter-Counter Manufacturer Valhalla Scientific
.- Model Number 4440 Type LED Display Calibration Due 8-14-83 NTS Number G850S Instrument Drop Test Tower Manufacturer National Technical Systems s' Model Number None Calibratio'n Due 4-29-83
, NTS Number P588V Instrument Pressure Gauge Manufacturer Ashcroft Model Number 1082A Calibration Due 3-20-83 NTS Number P670V Instrument Pressure Gauge O Manufacturer Helicoid V ' Model Number - 4-1/2W-5000-50 Calibration Due 5-14-83 NTS Number P1062V Instrument Pressure Gauge Manufacturer U.S. Gauge Company Model Number 1818 Calibration Due 6-12-83 , VIBRRATION 24" AIR OPERATED ACTUA0R DYNAMICS NTS Number 0920S l Instrument Log Voltmeter / Converter Manufacturer Hewlett/Packard . Model Number 7562A Calibration Due N/A NTS Number D1001S Instrument DC Ampiifier Manufacturer Dymec, Inc. Model Number 2460A Calibration Due N/A A-1 E369
t i mmm.m Rennrt 528-0951 b-s$ to NTS Number D1024S Instrument X-Y Plotter Manufacturer Esterline Angus, Inc. Model Number 575 Calibration Due Prior to Use NTS Number D1132S Instrument Shaker Manufacturer MB Electronics Model Number C220 Calibration Due N/A NTS Number D1133S Instrument Amplifier Manufacturer Ling Elecronics
, Model Number PP120/150 Calibration Due N/A NTS Number D1320S Instrument -
Accelerometer
- r. Manufacturer PCB l Model Number 3088
, Calibration Due 9-22-83 NTS Number D1321S Instrument Accelerometer Manufacturer PCB Model Number 3088 Calibration Due 9-22-83 NTS Number D1327S Instrument - Accelermneter Manufacturer PCB Model Number 3088 Calibration Due 9-22-83 NTS Number D1328S Instrument Accelerometer Manufacturer PC8 . l Model Number 3088 Calibration Due 9-22-83 NTS Number D13635 Instrument Power Supply Manufacturer PCB Model Number 483M59 Calibration Due N/A i s> l A-2 1 E u,
Report 528-0951 i ymhaw ,
.- sym
. O NTS Number D1491S Instrument Sine Beat Computer Manufacturer Ohio Scientific Model Number Challenger 8 Calibration Due N/A 9
NTS Number D1492S Instrunent Disk Drive Manufacturer Ohio Scientific Model Number CO 2 Calibration Due N/A NTS Number 01493S Instrument Keyboard Manufacturer Ohio Scientific
, Model Number Unknown Calibration Due N/A NTS Number D14965 Instrument Accelerometer Manufacturer Entran Devices Model Number EGAXT-25 Calibration Due Prior to Use O
(,,/
- NTS Number D1536S Instrument Power Supply Manufacturer PCB Model Number 483 A Calibration Due Prior to Use NTS Number D1560S Instrument Sweep Oscillator Manufacturer -
Spectral Dynamics Corporation Model Number SD-104A-5 ,, Calibration Due 7-14-83 NTS Number D1561S Instrument Amplitude Servo / Monitor Manufacturer Spectral Dynamics Corporation Model Number SD-105-B Modified to C-1 Calibration Due 7-14-83 NTS Number E13155 Instrunent True RMS Voltmeter Manufacturer Ballantine for MB Electronics Model Number 320-076 Calibration Due 8-3-83 O
\s J A-3 E369
-. - - - .- n . , . . . -- . - - - , - - -
a-g ,,,, Report 528-0951 sN NTS Number E1544S
, Instrument Oscilloscope ,
Manufacturer Tektronix, Inc. Model Number 535 Calibration Due 3-20-83
- i. NTS Number E1554S Instrument Oscillograph, 18 Channel
. Manufacturer Honeywell, Inc.
Model Number 1858-T790G Calibration Due Prior to Use NTS Number G862S Instrument Video Monnitor Manufacturer Panasonic a- Model Number WV-411 4 Calibration Due N/A NTS Number G863S
' Video Monitor Instrument
.4 Manufacturer Panasonic Model Number WV-411 Calibration Due N/A SEISMIC PRE AND POST BASELINE 6" AIR OPERATED ACTUATOR NTS Number E1495S Instrument Variable Transformer Manufacturer Superior Electric Company Model Number 1168 Type . Single phase,120 volt Calibration Due Maintenance only NTS Number G835S Instrument Stop Watch Manufacturer Aristo Import Co., Inc. Model Number " Apollo" Calibration Due 8-10-83 - NTS Number P1286S Instrument Pressure Gauge Manufacturer Kunkle Model Number None Calibration Due 7-9-83 NTS Number P585V Instrument Flowmeter Manufacturer Fischer & Porter Co. I' Model Number Tube No. 8635 10/77 Type Tapered Tube Calibration Due 7-9-83 A-4 E369
N Report 528-0951
, atone
] sy.e I
l.0 ' NTS Number E1473S j.. Instrument Data Logger
, Manufacturer Fluke Model Number 8034A i Calibration Due 4-14-83 )
- VIBRATION 6" AIR OPERATED ACTUATOR DYNAMICS TEST .
NTS Number 01025S Instrument X-Y Plotter I Manufacturer Esterline Angus, Inc. Model Number 575 ) Calibration Due Prior to Use ; l 1 NTS Number D1240S Instrument Accelerometer ' Manufacturer PCB Model Number 308B Calibration Due 10-12-83 NTS Number D1320S Instrument Accelerometer Manufacturer PCB Os Model Number 3088 Calibration Due 9-22-83 NTS Number 01327S Instrument Accelerometer Manufacturer PCB . Model Number 308B Calibration Due , 9-22-83
- NTS Number D13285 l- Instrument Accelerometer l Manufacturer PCB Model Number 308B Calibration Due 9-22-83 NTS Number D1345S Instrument Accelerometer Manufacturer PCB
! Model Number 308B Calibration Due 10-12-83 NTS Number G832S Instrument Torque Wrench Manufacturer Snap-On Tools Corporation Model Number TE-12A - Calibration Due 9-9-83 A-5 E369
Report 528-0951 D ~
, .1s Number 0519V Instrument Sweep Oscillator Servo Manufacturer Spectral Dynamics Corp.
Model Number 104A-5 Calibration Due 7-14-83 NTS Number D1022V Instrument Amplitude Servo Control / Monitor Manufacturer Spectral Dynamics Corp. Model Number 1058 Calibration Due 7-12-83 NTS Number D1192V Instrument Signal Vibration Protector Manufacturer Spectral Dynamics Corp.
. Model Number 129A Calibration Due Prior to Use PRE AND POST STATIC LOADS TEST BASELINE NTS Number E1490S Instrument Digital Multimeter
/~'N Manufacturer Keithley Instruments, Inc.
(,-)
- Model Number 179-20A Calibration Due 5-26-83 NTS Number G835S Instrument Stop Watch Manufacturer Aristo Import Company, Inc.
Model Number Calibration Due
') Apollo 8-10-83
( . STATIC LOADS NTS Number 0838S Instrument Centrifuge Manufacturer CEL . Model Number None Type Diesel engiine driven Calibration Due N/A NTS Number D839S Instrument Centrifuge Control Console Manufacturer CEL Model Number None Calibration Due N/A O A-6 . E369
Report 528-0951
, ,Netone e sr ,
. O NTS Number D1453S Instrument Centrifuge Control Console Manufacturer NTS Model Number None
. Type Remote operational speed control
.- Calibration Due N/A NTS Number E1305S Instrument Electronic Counter-Timer Manufacturer Systron Donner Corporation Model Number 1032 Calibration Due 5-23-83 SEISMIC PRE AND POST DYNAMICS RETEST NTS Number E1495S Instrument Variable Transformer Manufacturer Superior Electric Company Model Number 116B Type Single Phase, 120 volt Calibration Due N/A
("'N NTS Number P551V
\s,)
- Instrument Pressure Gauge -
Manufacturer Ashcroft Model Number 1082A Calibration Due 7-4-83 NTS Number P585V Instrument Pressure Gauge Manufacturer Ashcroft Model Number None Calibration Due 7-12-83 NTS Number P670V Instrument Pressure Gauge Manufacturer Helicoid Model Number 4-1/2W-5000-50 - Calibration Due 5-14-83 I NTS Number P1062V Instrument Pressure Gauge Manufacturer U.S. Gauge Company Model Number 1818 Calibration Due 6-12-83 I O
. A-7 E369
u, Reoort 528-0951 sN r .
!.. VIBRATION DYNAMICS RETEST
.l
'~
NTS Number D1422S Instrument Accelerometer
- . . Manufacturer BBN Instruments Company Model Number 5088-01 j Type With top count connector Calibration Due 9-9-83 NTS Number D1426S Instrument Accelerometer Manufacturer BBN Instruments Company Model Number 5088-01 Type With top mount connector
, Calibration Due 9-9-83 NTS Number D1427S Instrument Accelerometer Manufacturer BBN Instruments Company i Model Number 508B-01 l Type With top mount connector Calibration Due 9-9-83 O)
( ,, NTS Number D1429S Instrument Accclerometer Manufacturer BBN Instruments Company Model Number 5088-01 Type With top mount connector 4 Calibration Due 9-9-83 NTS Number 01433S l Instrument - Accelerometer Manufacturer BBN Instruments Company Model Number 5088-01 Type With top mount connector Calibration Due 9-16-83 NTS Number D1438S . 1 Instrument Accelerometer Manufacturer BBN Instruments Company Model Number 5088-01 Type With top mount connector Calibration Due 10-5-83 NTS Number D14395 Instrument Accelerometer Manufacturer BBN Instruments Company Model Number 5088-01 Type With top mount connector O Calibration Due 10-5-83 A-8 E369
I Report 528-0951
! umm.m sN io 'V NTS Number D1542S , Instrument Accelarometer Manufacturer PCB Piezotronics, Inc.
Model Number 3088
}
Calibration Due 6-17-83 NTS Number D1543S I Instrument Accelerometer Manufacturer PCB Piezotronics, Inc. Model Number 3088 Calibration Due 6-17-83 't VIBRATION - 24" AIR OPERATED ACUTUATOR i - NTS Number D13555 Instrument Accelerometer / Power Supply Manufacturer PCB Model Number 483A07 Calibration Due Prior to Use NTS Number D14585
-g Instrument Servo Programmer y) . Manufacturer Unholtz-Dickie Corporation SPA-7 Model Number Calibration Due 5-30-83 NTS Number D1475S Instrument Sweep Oscillator Manufacturer Spectral Dynamics Corp.
Model Number SD104A-5 Calibration Due . 7-21-83 NTS Number D1479S Instrument Servo Controller Manufacturer Akashi Seisakusho, Ltd. Model Number SC-1 i Calibration Due Prior to Use NTS Number D1480S Instrument Servo Controller Manufacturer Akashi Seisakusho, Ltd. Model Number SC-1 Calibration Due Prior to Use ( NTS Number D1484S Instrument X-Y Plotter Manufacturer Esterline Angus, Inc. Model Number XYS75 fg ( ,) Calibration Due Prior to Use 1 A-9 l l 5369
N.e.nw Report 528-0951 sy n.
..~~
l i
, NTS Number D1489S Instrument Charge and Voltage Amplifier .
Manufacturer PCB Piezotronics, Inc. Model Number 464 M10 : Calibration Due 7-28-83 i NTS Number D1490S i Instrument Charge and Voltage Amplifier
, Manufacturer PCB Piezotronics, Inc.
Model Number 464 M10
] Calibration Due 7-28-83
', NTS Number 01491S Instrument Sine Beat Computer
. Manufacturer Ohio Scientific
,- Model Number Challenger 8 Calibration Due N/A NTS Number D1492S Int ament Disk Drive
- 2~
Manufacturer Ohio Scientific Model Number CO 2
,, Calibration Due N/A
\~~/ 'NTS Number D1493S Instrument Keyboard Manufacturer Ohio Scientific Model Number Unknown Calibration Due N/A NTS Number D1568S Instrument ~
Log Converter Manufacturer Hewlett-Packard Model Number 7562A
- i. Calibration Due 9-30-83 NTS Number E1383S Instrument Calibrator Manufacturer Trigtek Model Number 401A Type Battery operated Calibration Due 4-25-83 NTS Number E15165 Instrument Tape Recorder Manufacturer Sangamo Model Number Sabre VI Calibration Due Prior to Use 1
O 1 O A-10 E u,
_ Report 528-0951. Rev. A ! y W i i i
- .O NTS Number E1551S i Instrument Oscilloscope, Storage
.- Manufacturer -
Tektronix, Inc. Model Number 564 Calibration Due 8-22-83 NTS Number Nene (rented equipment) a : Ir.:,trument Volt /Anp Recorder . Manufacturer Esterline Angus ' Model Number A601C Calibration Due Prior to use 'I i 'l e
- o. .
I O A-11 E as,
- - - - _ . - - . . .- .. _ _ _ . - _ _ _ . .. . . . . . - - _ _ _ _ _ = _ _
Report 528-0951 I 1.. sN 4 !.O i ,e-i l j' e 1 APPENDIX B STATIC TEST PERFORMANCE DATA FOR
. 6-INCH MOTOR OPERATED. VALVE, 6-INCH AIR OPERATED VALVE
, AND 24-INCH AIR OPERATED VALVE
- 1. Pre Test Baselines
- 2. Performance During Test
- 3. Post Test Baselines i
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~ . Report 528-0951, R::v. A Y
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.- m National Scientife Testing Owision Technical Servces ..O Systems Grouc 20988 West Goicen inangte Acao Canyon Ccyntry. California 91351 Tel: sos 259 8184 ,. TEST RECORD Shell Test (Fill in all blanks or indicate NR) Seat Test & '9 Q.E.-STPst\C. HYDROSTATIC PNEUMATIC k i
OTHER Job No. $3-(T-tS I Job Name Pr16_L. Assembly Dwg. No./Rev. Description (size, type) Mark No of Valve v a. - 2.o s3-o 2.-p - o i V a u o e_ Serial Number of Item Tested %$~2-80% L.\ rn t 0 9Ed?.9rto rt_ Test Procedure No: S?_S -0951 Rev. b Date \- M -I 3
/
Calibration of Pressure Gage S/N 9-\276 5 Data Calibrated Before Test M-33 Satisfactory / unsatisfactory Date of Test M 45-D Data Calibrated After Test 4/!R Satisfactory Unsatis factory _ Pressure bb PSGTime 4 M \O Temperature 71 Results: Satisfactory / Unsatisfactory W Bobb 2
~wr-Itc_ UO tED Leakage at 68 PSI Gr- . Comments:
a Signec i l b
. Assemoly anc Test N OO OEb Signed h # 5-9 c91 i -
Quality Control /Date 1 Signed Autnorizea Inspector / Witness O p. B-6
I R National Sc:entife Testing Owision Technicei . Services 20988 West Goicen Tnangte Acae
,i Systems Grouc Canyon Country. Cahfornia 91351 Tet 805 259 8184 ' TEST RECORD Shell Test Obi MMb (Fill in all blanks or indicate NR) Seat Test W HYOROSTATIC PNEUMATIC OTHER _
Job No. 'OC 3 $1 Job Name klVIG-L Assembly Owg. No./Rev.
' Description (size, type) Y Mark No. of Valve fr 2 - 20 5 3 - 0 2. - A.i - O/ U A t. v g l Serial Number of Item Tested M 2_ 70 9 L i m i f- O/>e: #2.A-fo AL Test Procedure No: $ '2 T*PI/ Rev. #- Date /- v - 1 3 Calibration of Pressure Gage S/N [ /f 2r I Date Calibrated Before Test A-/f-47 Satisfactory v' Unsatisfactory Date of Test 'V 7 J Date Calibrated After Test M!4 Satisfactory Unsatis factory Pressure C[ PSISTime Mu.'s Temperature 7 f 7 Results.:4 V' Unsatisfactory ya A ot- boS tisfactory o ,x a M o /s./ -
Leakage at 44'~ PSI Comments: .S ass elzel-- 82 Ase , aole+r3 a in G </ S'igned @= "
- Assemoly ano Test Signed N9'83 Qua11:y Contro1/Date Signed Autnorizec Inspector / Witness O
B-7
..m -
f' National Sc:entific Testing Division Technical Sennees 20988 West Golcen inangte Acac
, Systems Grouc Canyon Country. Canternia 91351 Tel: 805 259 8184 TEST RECORD Shell Test
-) _g g g (Fill in all blanks or indicate NR) Se t Test (N HYDROSTATIC PNEUMATIC d OTHER Job No. 6 2 % O S I Job Name hMCL Assembly Owg. No./Rev.
Description (size, type) @ Mark No. of Valve 3'2.- 2.0 s 's - O '*.5 - )J -0 ) v ALU E Serial Number of Item Tested T 2 - 90 2A - $~ 0 9 dutA, e et_ Test Procedure No: 54-Oc iS \ Rev._ A- cate Ja 4 /Oss. Calibration of Pressure Gage S/N h \ '2_ %(o $ , Data Calibrated Before Test M 4 3 Satisfactory V Unsatisfactory bate of Test N'~25-8 3 Data Calibrated After Test h!f Satisfactory Unsatisfactory Pressure SS pS wTim. 4 rmo Temperature 7L % Results: Satisfactory V Unsatisfactory { .Ol M k a 1 ~ Leakage at 68 PSIC:r-sohp c.Mex Bs. con.c. map 6yrtEmeFT *C GAWM, MG'9Y) Coments: Lhm ai smuu . mu ic i _ etc. ictg cb oc gr
--LEAK A04:L tuna 7_ 7 h bhtcs o n_ \ .O \ celm O Signed
- Assemoly anc Test b k Signed #-25 -B 3-Quality Control /Date Signed Autnor1 rec Inspector / Witness O
B-8
. m T National Sc:entife Testing Division
'7 Technical Servces 20988 West Goscen inang:e Acac Systems Grcuo
, , Canyon Country. Canternia 91351 Tet 805 259 8184
- TEST RECDRD g ggg4 Shell Test (Fill in all blanks or indicate NR) Seat Test M HYDROSTATIC PNEUMATIC W OTHER Job No. K2x n or/ Job Name 14tr*&~L Assembly Dwg. No./Rev.
Description (size, type) b" Mark No. of Valve 1!r2. - do S '5 -<> E - A.) -O / v At.v 6. 4 Serial Number of Item Tested ff 2 Cid 2.9 - S O p S /2f y ro W _ Test Procedure No: S2&-oesy Rev. A Date Calibration of Pressure Gage S/N k /3M Data Calibrated Before Test N'N Satisfactory V Unsatis factory
*Date of Test @2$ 43 Data Calibrated After- Test M[R Satisfactory Unsatisfactory _
Pressure 55 951 Time 4 alzu Temperature 7 5"F Results: Satisfactory V Unsatis factory l.00CC/ Min ~ Leakage at 56 PSI SOAP CHEC' K /3EFogd7 m &9sWEE MSU7~of Z81KdzCf, MorfD
, Comments: sfAkA66 ht) SMkL DowZl MW L d;u/MP /MG- Bu-r"
- sEAxA&c uAs 38 8088.63 ok' I <60 .CC/MW Signed g (~'M _
mo ' anc Te t Signed 5 'M-b
, QuaTity Contro1/Date Signed Autnor1zec Inspector /Witnecs O
B-9
9 National Scientrfic Testing Division {'g Tschencal Services 20988 West Goicen inangte Acaa
., Systems Grous Canyon Country. California 91351 Tet 805 259 8184 , TEST RECDRO Shell Test
), ' (Fill in all blanks or indicate NR) Seat Test v HYDROSTATIC PNEUMATIC g Other l ll OTHER Job No. D ~ @ 3\ Job Name NL- , Assembly Dwg. No./Rev. Description (size, type) M Mark No. of Valve vha v E. g2. - 205 S -o 1-M -O / - lt Serial Number of Item Tested O PGT2Atart F 2 - @ 2_.9 - / Test Procedure No: 5'2 o 4 5 / Rev. A Date Calibration of Pressure Gage S/N I329$ Data Calibrated Before Test ~~hSatisfactory / Unsatisfactory
'Date of Test 5'b O 3 Data Calibrated After Test A/!R Satisfactory Unsatis factory Pressure Sb PSI Time h87/AJ Temoerature 73 Results: Satisfactory V Unsatis factory
~
Leakage at 55 PSI Comments: sor+fA. Dn check AJO gecons WA && _mensva.emnr of w-A wn- % - Signed pg %}ie_. Assemoly anc Test Signed W N-83 Quality Control /Date Signed Autnor1:ec Inspector / Witness O B-10
q Natkmat Sc:entrfic Testing Division jO Techn6 cal Systems Senmes Groco 20988 West Golden Tnangte Road Canyon Country. Cahfornia 91351 Tel: 805 259 8184 TEST RECORD I Shell Test i (Fill in all blanks or indicate NR) Seat Test Other HYDROSTATIC PNEUMATIC d OTHER Job No, b I ~~ b D Job Name kN Assembly Owg. No./Rev. Description (size, type) Mark No. of Valve v P rt A> S. 7 2_-J.oS 3- 07-p - o 1 Serial Number of Itam Tested ODGifLAtTo/t w 2. - G et ? A -/ Test Procedure No: $D 'O f $$\ Rev. b Date Calibration of Pressure Gage S/N Data Calibrated Bef stl M atisfactory V Unsatisfactory Date of Test _ b 3 Data Calibrated Af r Test /l!8 Satisfactory Unsatisfactory Pressure PSI Time E\IL Temperature Results: Satisfactory / Unsatisfactory . Comment K
\
Signed emoly anc Test C" PoS4- S O . Vo - Signed b ' 9 -63 Quality Control /Date Signed Autnor1reo Inspector / Witness O B-11
m Report 528-0951
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-. APPENDIX C RES0 NANCE SURVEY AND DYNAMICS TEST ON 24-Inch AIR OPERATED ACTUATOR.
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