ML20155H149
| ML20155H149 | |
| Person / Time | |
|---|---|
| Site: | Vogtle  |
| Issue date: | 05/14/1985 |
| From: | FISHER CONTROLS CO., INC. (SUBS. OF MONSANTO CO.) |
| To: | |
| Shared Package | |
| ML20155H119 | List: |
| References | |
| FQP-11A, FQP-11A-RC, NUDOCS 8605130342 | |
| Download: ML20155H149 (479) | |
Text
{{#Wiki_filter:I; . 7 , '9G10-AXLAC03-5060-9 001 l-i FQP-11A, Rev. C ! May 14, 1985 l FISHER ENVIRONMENTAL QUALIFICATION REPORT I Type 9200 Butterfly Control Valve Assembly Alvin W. Vogtle Nuclear Plant Georgi a Power Co. I Bechtel Power Corp. XSAC03 Series l ! 7 A O \/ PR0PR'C'a.g[TI gI*
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FQP-11A c Fisher Controls Doccmact Ocwor Sheet Vogtle Environmental Qualification Report for
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w .,, 3 ~, 8 0 4 g ga Type 9200 Butterfly Control Valve Assembly - ( Page 0.1 og Rev i eFisher Controls s c,w l E- J - r - Tinet Page Revisson Page Reveson Page Roweaan Page Revison Numcor Level Number Loved Numcor Levet Number Leve6 0.1 c Att. A-9 A 0.2 C Att. A-10 A 1 C 2 S 3 B
, 4 c 5 B 6 S 7 C Att. A-1 A Att. A-2 A Att. A-3 A l
l Att. A-4 A { Att. A-5 A Att. A-6 A Att. A-7 A Att. A-8 B Ths page is the cover sheet of all documents containing 3 or page will be made when any page of this document is revise , more pages of soecifications. The table above snows the When refernng to this docurrhant specify tne revision leven revisen level of each page of tNe document. A revieson of the this page. i __a
9 'M O - O'" ^ r " ' ""'" "' Mehet CentFOIS FISHER QUALIFICAT10N REPORT F0P-11A C Vogtle Environmental Qualification Report for 4 "F
# - ' r- W Type 9200 Butterfly Control Valve Assembly _ 7 ,. ,c . ; . q -
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- Y" hd 2-,3 W TABLE OF CONTENTS Title Page............................................................ 0.1 Table of Contents..................................................... 0.2 1.0 Scope............................................................ I 2.0 Selection of Test Valve Components............................... 2 3.0 AcceptanceCriteria.............................................. 2 4.0 C on du ct of E n vi ronne n t a l T es t . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 5.0 Suma ri za ti on of En vi ronnental Test Resul t s. . . . . . . . . . . . . . . . . . . . . . 3 5.1 N o rna l L o a d F u n c t i o n a l T e s t s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 5.2 T he rma l A g i n g S i nul a t i on. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 5.3 Radiation Exposure.......................................... 3 5.4 Seismic Aging Simulation.................................... 3 5.5 DBA Load Test............................................... 4
- .6 Qualified Life Determination................................ 5 5.7 Ext ens i on o f Qu al i f i ed L i f e. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 5.8 Extension of Qualified Life................................. 6 t
- 6.0 Conclus ions Based on the Envi ronnental Test Progran. . . . . . . . . . . . . . 7 i
( Attachnents: t A-1: Wyle Environmental Test Report No. 45088-1 (Includes FQP-19 as
- Addendum I, FQP-23 as Addendun II) l A-2
- Discussion of Anomalies Noted During Environnental Test, NA-29 A-3: Modifications and Exceptions to FQP-19, FQP-23, and NA-29 for l Application to the Vogtle Project, NA-47 i A-4: Wyle Lab Report No. 45390-1, Temperature Transients and Seat Leakage Tests A-5: Isomedix letter, dated Fearuary 3,1981 A-6: Continental Mechanical Aging Test Report No. 92-395, NA-30 A-7: Fisher Lab Problem 1685-3, Report 11 " Determination of Activation Energies for Nuclear Service Elastomeric Materials" A-8: Arrhenius Rate Equation Calculations A-9: Effects of Gamma Radiation Exposure to 200 Mrads on 20" Type 9220 Valve with Bettis Actuator
( A-10: Correspondence relevant to NOA #4, NA-29 (see Attachment A-2) d N19-ll/ 8 L J
9510- AXG AC 0 3- 5 0 /& 9 009 gg FISHER QUALIFICATION REPORT FQP-11A c-Vogtle Environmental Qualification Report for b cm g- g _ g,
, Type 9200 Butterfly Control Valve Assembly Aovo cv a-n-%
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OFeher Controis 1.0 Scope This report sunnarizes the procedures used and test results obtained in the course of Fisher's Environnental Qualification Test on a Bettis-actuated Type 9200 butterfly valve assembly. The test prograr. was originally conducted to satisfy the requirements of another qualifica-tion project. The progran is now presented, with nodifications as noted, for qualification of the Seismic Category I butterfly valves for the Vogtle project. The original controlling documents, FQP-19 and FQP-23, are provided as addenda to Attachment A-1. Discussion of anonalies noted during the environnental test is presented in Attachnent A-
- 2. Modifications and exceptions to the test procedures that pertain to the Vogtle project are provided in Attachment A-3. The progran verifies qualification of the valve tested for a normal service life in a nuclear power plant environnent and verifies the capability of the valve to subsequently survive a Design Basis Accident (DBA) and perform its safety-related function. Re-instatenent of quali fied li fe in successive increments, to a naximun of 41 years total, is also discussed.
Therefore, this document furnishes suitable evidence of equipnent ( adequacy under environnental conditions required for the Vogtle project. In conjunction with any of the individual Vogtle valve group reports, this volune furnishes complete qualification information in keeping with Speci fication X5AC03, Rev. 11, including Appendix EA, Rev. 3 and d Appendix QG, Rev. O, as interpreted by FQP-11AB and FQP-11C. 1.1 Extent of E vironnental Test in accordance with FQP-19, radiation exposure, artificial aging, seismic vibration, and exposure to a design basis accident environnent were used to verify qualification of a 20" Type 9200 butterfly valve with an elastomeric EPOM T-ring seal and a Bettis Model T420B-SR2 Rotary pneunatic actuator. Activation energy testing of elastoneric materials is also included to determine qualified life for the T-ring seal and other elastoneric components. 1.2 Extension of Test Results Test results can be extended to other Type 9200 valves, since the test valve was of typical construction design and naterial. Other sizes of Type 9200 valves can be qualified since all components required in perfomance of safety-related functions utilize the same materials and design principles as the test valve. Although various models of Bettis' actuators could well be qualified by results of this environmental test progran (since all components of the Bettis actuator required to perform the safety-related function utilize the sane design principles and material as the N19-11/ 1 L 1
9510- Axvr 0 3- 50 M1 'l 005 Fisher Controls FISHER QUALIFICATION REPORT FQP-11A 6 Vogtle Enviromental Qualification Report for W 6-16 0 Type 9200 Butterfly Control Valve Assembly
^* FD T \
RMM. " Page 2 9-2/-8) of cFisher Controls pj l g.f; g4 tested unit), this report does not purport to qualify the Bettis a ct ua to r. Qualification documentation for the Bettis Actuators is being provided by the supplier (G.H. Bettis, Waller, Texas). 2.0 Selection of Test Valve Components Test valve cmponents were selected as being representative of both the 9200 Series valve bodies and the Bettis actuator line. It was Fisher's intention to test the largest body and actuator sizes possible, inasmuch as the largest valves on the previous project were subject to the rest stringent envi ronmental speci fication requi rements. Consequently, the T420B-SR2-12 Bettis actuator was combined with a 20" Type 9200 butterfly valve body, since this was the largest actuator / body combination that could be accmmodated in the Wyle Lab environmental test chamber. (Both major components had been qualified seismically in earlier tests.) The vibratory sequences in this series of tests were conducted specifically to provide seismic aging to the test valve. 3.0 Acceptance Criteria ( FQP-19 provides a listing of acceptance criteria for the various envi ronmental test val ve components. These include leakage criteria for the val ve and speci fic actuator. As required by the Qualification Plan, any malf unctions are to be reported for evaluation. The Wyle Envi rorcental Test Report No. 45088-1 (Attachment A-1) provides this notification by means of a series of designated " anomalies" that are f urther di scussed in Attachments A-2. However, it must be noted that the "anmalies" primarily indicate deviation from test procedure or f acility limitation, rather than equipment shortcoming. None of tne
" anomalies" listed was found to prevent satisf actory performance of the val ve's safety-related function.
4.0 Conduct of the Environmental Test The test was conducted in accordance with FQP-19 and included readjust-ment of the elastomer T-ring seal following the high temperature accelerated aging process. This adjustment was performed to compensate for the unrealistic compression-set tendencies of the elastomer T-ring material resulting from the accelerated aging temperature, which would not have resulted from a real-time, 5-year aging period at 170*F. (Field service infomation has confimed that Type 9200 valves regularly provide satisfactory shut-of f capability and exhibit no excessive compression-set tendencies af ter 5 years of real-time, nomal-service operation.) So the planned adjustment served to ensure that the test valve was very comparable to production units aged at nomal operating t empe ratu res. (. N19-11/ 2 S 4 t . c ,---o. -
l 9G10- AXW o'n u /
- c FISHER QUALIFICATION REPORT FOP-11A b Vogtle Environmental Qualification Report for O'#0'OA
'g Type 9200 Butterfly Control Valve Assembly " FOT 9 8J l k
% 3 eFleher ConeWs D{fp/ /J-/'- B f Following the post-aging re-adjustment of the T-ring seal, the valve assembly was exposed to radiation equivalent to putting the valve assembly in its end-of-life condi tion. This radiation (1x107 rads equivalent air dose) was followed by the Design Basis Accident simulation, which included seismic aging, a 30-day steam and chemical exposure profile, and an additional radiation exposure bringing the accumulated exposure to 1x10e rads. Supplementary irradiation was provided, as certified by Isomedix in the Attachment A-5 letter to bring the total dosage accumulated to 2 x 108 rads, satisfying the Vogtle requirements. A sumary of the high radiation level tests and results is presented in Fisher Laboratory Test Report 8, Problem 1685-3 which is provided as Attachment A-9 to this report (FQP-11A).
5.0 Summarization of Envirornental Test Results The original environmental testing program was based on Fisher Qualification Plan FQP-19 and is fully documented in Wyle Test Report No. 45088-1, furnished as Attachment A-1 of this volume. (The Wyle Report includes a copy of FQP-19, designated as Addendum 1.) Results of various portions of the test program are summarized bcVow. 5.1 Nomal Load Functional Tests - The test valve was subjected to a series of ( baseline and nomal load functional tests at elevated temperature. No seat ~ leakage was noted tring the 75 psid gaseous nitrogen (GN 2 ) testing or during 150 psid water testing. Sections II, III, and IV of Report 45088-1 ( Attachment A-1) document the procedures and results of these tests. 5.2 Themal Aging Simulation - The test valve was cycled 1000 times tring the 281/2-day heat aging process and leak-checked at 228'F four times during the period. No leakage was detected during any of the four required leak checks at high taperature with 75 psi pressure drop. A subsequent 75 psid functional test at abient temperature also produced no leakage. Compl ete procedures and results appear in Sections V and VI of Wyle Test Report No. 45088-1 ( Attachment A-1). 5.3 Radiation Exposure - No visual evidence of damage or degradation of the unit resulted from exposure to 1.0 x 107 Rads equivalent air dose radiation. Post-radiation functional tests initially indicated very minor leakage past the piston of the Bettis' actuator, but the leakage ceased after operating the valve several times. No leakage was observed past the valve disc during
- the 15-minute test period. Sections VII and VIII of Report 45088-1 ( Attachen A-0 report the complete test procedures and results. Supplementary radiation exposure , as documented in AttacMents A-5 and A-9 provides evidence that total exposure of the test valve assembly reached 2 x 108 rads. Note that catastrophic failure of the T-ring did not occur even at the highest radiation level (200 Mrad). The main effect of the environmental test sequence was increased leakage after return to abient (70'F) temperatures.
5.4 Seismic Aging Simulation - The test valve operated smoothly throughout the
. sine-beat seismic tests.
, N19-11/ 3
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9D10- Ax5 Ar n a- rm /.n- N nn7 N FISHER QUALIFICATION REPORT F0P-11A G tr # # ' ' #~ C Vogtle Environnental Qualification Report for Type 9200 Butterfly Control Valve Assembly % /r- "- r;- L Pese 4 W OFisher Conerois ,, s r- r ,p - 5.4.1 Some minor difficulties were encountered, as shown in the designated " Notice of Anonaly" sheets included in Wyle Test report No. 45088-1 (Attachment A-1 of this volume), but, as previously mentioned, most refer to deviations f rom test procedure or to facility limitarions, rather than to equipment shortcomings. Further discussion of these
" anomalies" is presented in Attachment A-2. See Attachment C
A-10 for clarification of N0A #4 in NA-29 (Attachment A-2). 5.4.2 Electrical monitoring, stroking time tests, and seat leakage tests all showed favorable results before, during, and after the seismic tests. 5.4.3 Post-seismic functional tests produced no difficulties that have bearing on the Vogtle project. (See Section IX of Wyle Test Report No. 45088-1.) Valve stroking time was shown to be consistently in the range of 20 seconds and there was zero leakage with 75 psid across the valve disc for 15 ninutes. [ 5.5 DBA Load Test 5.5.1 Tne test valve met all the specified criteria, including satisf actory performance of the safety-related function by closing and staying closed. The Wyle test facility was unable to meet the rapid change of temperature specified, but the slower temperature ramp achieved actually was a more severe test than that specified. The val ve perf orned satisfactorily throughout, with no leakage past the valve disc. DBA Load test procedures and results are discussed in Section XI of Wyle Report 45088-1 (Atachment A-1). 5.5.2 Additional thermal transients and seat leakage tests were performed as discussed in Section X11 of the Wyle report. The tests were necessitated because of Wyle Laboratories' inability to accomplish the intended 381 F temperature transient during the DBA load test sequence. No leakage was detected at 10, 20 and 30 psid, but leakage increased from one bubble per minute at 40 psid to 1167 cc/ minute with a 75 psi differential pressure across the valve disc. This leakage is well below the allowable test procedure leak rate of 1472 cc/ minutes for the initial functional tests at 75 psid. 5.5.3 Specifically to satisfy the requirements of the Vogtle project, further thermal transients and seat leakage tests {. were performed as documented in Wyle Test Report No. 45390-1, N19-11/ 4
9010- AXG AC O 3- 50 611- 4 Out: Fisher Control 3 FISHER QUALIFICATION REPORT FOP-11A E Vogtle Environmental Qualification Report for 5S-85 gg. Type 9200 Butterfly Control Valve Assembly ^*'8 707 .9 4 / _ g; Page 5 ' CFisher Controls fjgg /2-/J -84 Attachment A-4 The test valve was pre-heated to 200*F for 11 hours, moved to a 400*F oven for 15 minutes, stabilized at 125'F for one hour, and then leak checked with 2.5 psig air for 15 minutes. Zero leakage was noted. Oven temperature was lowered to 100*F and maintained for one hour prior to another leakage test. Again, no leakage was noted. 5.6 Activation Energy Testing The thermal aging of elastomeric parts was based on a conventional aging relationship (10*C rule; F0P-19 page 4) for the original test program. Activation energy testing has been added to the test program for the Vogtle project. The results from this testing permit a more accurate prediction of qualified life. The purpose, procedure, results and conclusion of this testing are recorded in Attachment A-7. 5.6.1 The results from activation energy testing show that the lowest activation energy for any elastomeric material used in the Vogtle butterfly valves is 0.79 eV (See Attach-ment A-7). The relationship between activation energy and themal aging is explained in IEEE 382-1980; Appendix C,
" Rationale for Nomal Service Thermal Aging.
5.6.2 The aging simulation done for this environmental qualification program (227.8'F for 28.5 days) can be shown to be equivalent to 5 years, 30 days at 126*F, based on an activation energy of 0.79 eV. Calculations are provided in Attachment A-8. The environmental testing supports a four year life at a continuous envi ronmental or internal temperature of 131*F. The calculation for this is also provided in Attachment A-
- 8. If the temperature is greater than 131*F, the maximum life will be stated in the final report.
5.7 Qualified Life Determination Page 4 of F0P-19 provides a general discussion of the rationale used in Fisher's selection of the accelerated aging techniques employed in the envi ronmental test program. The maximum time period for which the following equipment shall be qualified 's the same as that described in Paragraph 5.6.2:
?
k N19-11/ 5 \ c
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9510- AXGAC O 3- 50 60 'l 00Y Fisher Control] FISHER QUALIFICATION REPORT F0P-11A 6 Vogtle Environmental Cualification Report for 8-O E gg. Type 9200 Butterfly Control Valve Assembly ^* FO7 9-2 /- g g Page C' 6 CFisher Controls l )p/ /2- /2.-8 d 5.7.1 Fisher Type 9200 style valve bodies with elastomeric T-ring seals (This qualification also utilizes cycle aging infonration presented in the Continental Mechanical Aging Test Report No. 92-395, Attachment A-6 of this report.) 5.7.2 Bettis spring-return pneumatic piston actuators of similar design anc materials. [This qualification presumes acceptance by Vogtle of the qualification documentation furnished by the actuator manufacturer (G.H. Bettis).] 5.7.3 Model EA180-31302 and EA180-32302 NAMC0 limit switches. (This qualification presumes acceptance by Vogtle of the qualification documentation furnisned by the limit switch ma nu f acturer.) 5.7.4 Model NPK8316A74E and Model NPK8321A2V ASCO solenoid valves. (This qualification presumes acceptance by Vogtle of the qualification documentation furnished by the solenoid manufacturer.) k 5.8 Extension of Qualified Life of the Vogtle Butterfly valves 5.8.1 Ouali fied life is primarily a function of elastomer longevity under the rigors of themal and mechanical aging, seismic vibration, irradiation, and chemical profile exposure. Seismic Category I butterfly valves installed in the Vogtle nuclear plant are designed for a 41-year service life. This design life (or installed life) is in compliance with the project speci fications. Quali fled li fe can be re-instated in increments (as explained in Paragraph 5.6.2) up to a 41-year maximum, contingent upon regular performance of requi red maintenance operations. 5.8.2 Regular maintenance must include replacement of all elastomeric parts, i .e., T-ring seals, 0-rings, packing components, and gaskets, if qualified life of the unit is to be extended for another period. 5.8.3 The requirement for replacement of elastomers at periodic intervals is based ca use of the Arrhenius rate equation with activation energy values for the elastomers as detemined by test. Fisher research data, Lab Problem 1685-3, Report
- 11. "Detemination of Activation Energies for Nuclear Service Elastomeric Materials" is included as Attachment A-7 to this report.
N19-11/ 6 l l
9G10- AXLAC0 3- 506&- S 010 No. Flefter Centrol8 FISHER QUALIFICATION REPORT FQP-11A C h N P 'P C Vogtle Environmental Qualification Report for Type 9200 Butterfly Control Valve Assembly
- tr : 9 -2/- e.:
g Peo* 7 0' Rev OFehet Connie r!&u) r-a - (c-5.8.4 All maintenance should be performed in accordance with instruction nanuals provided by Fisher or by the appurtenance manufacturer. 6.0 Conclusions Based on the Environmental Test Progran 6.1 The environnental test sequence completed in accordance with the FQP-19 test plan is documented in Wyle Test Report 45038-1. It was demonstrated that the valve assembly would perforn satisfactorily for the intended period between maintenance cycles. 6.1.1 Stroking times were found to be slightly shorter at the conclusion of the DBA simulation than at the beginning of the progran, indicating no detrirent to valve operability due to increased friction. (See Section XI Results.) 6.1.2 Post-DBA leak-test showed no leakage at low pressure dif ferentials and less leakage at the 75 psid level than that allowed for the initial functional tests. (See ( Section XII Results.) 6.2 General condition of the valve and its successful operation at the conclusion of FQP-19 DBA sinulation and supplemental tests denonstrate successful completion of the test progran and verify its ability to perforn its safety-related closure function as required. (See Section XIII of Wyle Report ;5088-1, Report 45390-1, and Fisher Report 8, Problem 1685-3.) 7.0 Report Summary Information presented in this report is accurate and was compiled as a result of the test prograns and calculations described or referenced herein. Prepared by: Reviewed by: YrW
- 0. V Jon Whitesell / C. Dresser Johf Qualification Specialist g
Qualification Analyst Date: Nu,9 14 7 WSi Approved by: W ignage Tloyd Lj. Jury, Enginepring Qua lTific (on and Analysis N19-11/ 7 ,
S'510- AXGAC03- G068-9 011 Rev. A L . Attachment A-1 to Vogtle Quali'ication Report, FQP-11A Wyle Environmental Test Report No. 45088-1 Dated November 21, 1980 (Includes FQP-19 as Addendum I and FQP-23 as Addendum II) { i 4 e M38J1
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{ ADDRESS Pest ce a x 0, 205 south center S ueet, Marsha11tewn, Iowa 50158 Type 9200, 20" Butterfly Valve with a . H. Bettis Actuator l u TEST SPme nsher conucls cmpany 3.0 MANUFACTURER 4.0
SUMMARY
One (1) 20-inch, Type 9200, Butterfly Valve with a G. H. Bettis Actuator, hereinafter called the test item, was subjected to a Qualification Test Program as spec fied in Fef erence 5.1 and in accordance with References 5.2 and 5.3, to meet the intent of References 5.4, 5.5 and 5.6. The test item is used as a contain=ent isolation valve and is Class IE, safety-related. Paragraph 6.0 contains a description of the test ites. The Qualification Program was performed to confirm the adequacy of design of the test item to perform its required function in Nuclear Power Generating Stations under nor.a1 and abnor=al conditions as specified. STaTI op ALAS 4 MA Com op mao 6som " CA Professional Eng. " "__"._ M"7*O,"",,*_"_7.""" m . , , . m .. . - Reg. No. 2635 PREPARED BY - M
._ua e some, osso .no me. The mee,m.noa cent.a.e a me room m
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, SCIENTIFIC SERVICES AND $YSTEMS GROUP HUNTSVILLE. ALAsAMA
9510-AXGACO3-5068-9 013 PAGE NC. 11 TEST REPORT NC. 45088-1 i l 4.0 SQWARY (Continued) Its test item complied with all specified requirements, although ten , (10) anomalies w re noted. The test sequence, test item compliance with requirements, and Notices of Anomaly (NQh's) are discussed briefly below in tabular for:s and in detail in the appropriate sections of this report. TEST PROGRAM ANOMALIES CCHPLIZD REPCRT WITH ICA SEC"*!CN ""YPE TEST REQUIRDEWS REQUIRDENTS NO. REMARKS I Protest Visual Yes - N/A Inspection Inspection
- Baseline Cporate and Yes -
N/A Functional I.mak-Check II: Normal Operata at Yes - Replaced "T" Eing Load Test 120*F, 120*F k and 170*F. Imak-Check.
"7 Post-Nc m l Cperate and Yes -
N/A Icad Functional I4ak-Check 7 Aging 14n alternata Ye s ..1,-_....._ghambe r _t a=p . out,-e f _. Simulation high temp. and
' ' ' ~
toleratice fer approxi-humidity cycles, mately 30 =inutes. ~~
~
leak checks, and 1000 full strokes V Post-Aging Operate and Ye4 2 Cracked flexible cenduit. ,, Functional Leak-Cieck Luhricant leak. . Inters:.t-tant limit switch operation. No electrical measurements were made. Seat leakage ~ of 4102 in.3/ min of CN2 -
,, ,. . Adjustad " "-Ring.
1 VI: Radiation 1.0 x 10' Rads Ye s - N/A l gamma air equi'ralent. VIII Post-Radiation Operate and Yes 3 Shipping damage to 1/4" Leak-Check ( Functional tut:n . Leakage past the actuator piston of approxi-mately 314 cc/sec. WYLE LASONA70mm m Poemfy l i t
9510- AXboCO3- G060 ' 01 '! PAGE NO. iii TEST REPORT NO. 45088-1 4.0 SCMMARY (Centinued) TEST PROGRAM ANCMAI.IES (Continued) IX Seismic FQP-23, Yes 4 Intermittent limit switch. Rev. 9. Icose bolts between actuator mounting bracket and valve body. Test ter=inated. X Post-Seismic Cperate and ,Ye s 5 Icose wire in junction box Functional Imak-Check and loose condulet. 6 Rairline crack in the ju.% tion box. XI Accident valve must close Yes 7 First temp. transient (CRE) and stay closed. took 13 min and 37 sec. Si=ulation 381'F sax temp and g 30 days test leak check centinuously. e m ess he steam leakage. 9 Second temp. transient of 381*F was not accomplished; ( high temp was 365'F. The test c.hr camp was out-of-tolerance en the high temp. side for apprcximately 2 hours. 10 2.e te se cha=ber tamp. was out-of-tolerance for approximately 4 hours. 30 min, on the icw teep, side. Add 9 hours, 30 si.% to overall test ti=e. XII Thermal 381*F for 2 Yes - N/A Transient min, leak-(ICCA Addendum) check. XIII Po st-IDCA operate and No - Infezzation only. Functional I4ak-Check.
- TO Namenne Feuey
9510- AXGACO 3- 50 60 el 015 PAGE NQ. iv ( TEST REPORT NO. 45088-1 4.0
SUMMARY
(Continued) mis final test report contains the follonng sections. Ihe qualification Program was perfezzed in the sequence indicated by Section Numbers I through IIII. Section I Protest Inspection Section II Baseline Functional Test Section III Normal Ioad Conditions Test Section IV Post-Narmal Ioad Functional Tests Section V Aging Si=ulation
^
Section VI Post-Aging Simulation Functional Tests Section VII Padiation Exposure Section VIII Post-Radiation Functional Tests Sectic:m IX seismic Simulation ~ Section X Post-SeisELic Functional Tests f Section II LOCA (OBE) Simulatica I Section XII Thermal Transient Test (Addendum *w LOCA) Sectica XIII Post-LOCA Functicnal Tests Addandum I - Fisher Document TQP-19, Pavision F Addendum II - Fisher Docu=ent FQP-23, Pavisien 9 5.0 K57ERENCIS 5.1 Fisher Cont.rols Ccarpany. Purchase Order Number H-217770 5.2 Fisher Ibcument FQP-19, Revision F
- 5.3 Fisher Document TQP-23, Revision 9 l
5.4 IZEE 382-l'972', Trial-Use Guide for ?/pe Test of Class 1 Electric
~
Valve Operators for Nuclear Power Generating Stations. l 5.5 , E~ I23-i974,'"I522, StandMafor Qualifying Class II Equip =ent l , for, Nuclear Power Generating Stations". 5.6 a 344-1975, " Seismic Qualificatien of. Class II Equipment for l Nuclear Power Generating Statiens". 1 1 ( MMM Mumenne recany
4 VG10- AXGACO3- 5068- 1 016 PAGE NO. Y t TEST REPORT NO. 45088-1
\
6.0 'EST
. ITEM OESCRIPTION
' The test item is used as a containment isolation valve and is classified 2E, cafety-related. The following tabulation shows the test item, actuator and appurtenances that were subjected to the Qualification Program.
20", Type 9200, Fisher Controls Company ,, Butterfly Control valve Bettis T-4205-SR2-12 Pneumatic Actuator ASCC NP8320A185V 3-Way Solenoid Valve Namco EA18031302 and EA18032302 Limit Switches Fisher P595 Filter with Brass Element Fisher 95E Regulator Texsteam 35R Pressure Relief Valve l esffman Junction Box w/G.E. #EB-25 Terminal Strips
- _ versa VSP-3501-155H Pneumatic 3-Way Valve 7.0 Ct"4.!TY ASSURANCE All test equi; ment and instr.: mentation used in the perfor: nance of this test program wre calibrated in accordance with Wyle Laboratories' Ctality Assurance Policies and Procedures Manual, which confor=s to the applicable portions of ANSI N-45.2,10 CYR 50, Appendix B, and Military Specification MIL-C-45662A. Standards used in perfor='"q all calibrations are traceable to the National Bureau of S*xdards.
(
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9510-AXGAC03-5060-9 017 PaGE NO. I-l ( TEST REPCRT NO. 45088-1 SECTICN I PRETEST INSPECT!CN 1.0 REQ"!3E.ET:'S A visual inspection shall be performed to assure that the test item is not damaged due to shipping or handling since manufacture. 2.0 PROCZ:CPIS The test item was visually inspected upon receipt at Wyle Laboratories. A photograpn was made showing the as-received condition of the test item. 3.0 RES'ATS The test ites was sub]ected to the operations required by Paragraph ( 1.0 and as described in Paragraph 2.0. There was no visual evidence of damage due to shipping or handling since the test item was
=anufactured.
A photograph showing tne as-received condition of the test itan is presented in Appendix . mm m-m untev.% Pacihty
l Page No. I-2 Report No. 45088-1 l s P.ds page intentionally left blar,x, 1 a
9G10- AXL AC 03- G060- 9 019 PAGE NQ. I-3 fts7 AEPORT NO. 45088-1 1 4 4 e e e APPENDIX I PHOTOGPAPH mm -T aww ciw Faco.ty
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9G10- AXGACO3- G068-9 021 PaGE NC. II-l TEST MtPORT NO. 45088-1
.f SECTION !!
BAS C NE FUNCTICNAI. TESTS 1.0 REQUIREMENTS Functional tests shall be perfor:ned to ensure that all ccaponents perform without malfunction prior to any condition simulation. Base-line measurements shall be taken on various parameters as noted below: A regulated gas supply shall be connected to the solenoid valve of the test valve assembly. Nominal flow, as received frca the gas supply when the solenoid valve is actuated, shan be used. Se functional tests shall be performed with a voltage to the electrical appurtenances of 90 VDC, 125 VDC, and 140 VOC. The functional test para =eters to be measured shall be as fonew: Time duratien of the operating streke Opening and closing *dnes shall be recorded. (A cycle is defined as going from the full-closed to the full-cpen and back to the full-closed position. ) ( seat leakage at 75 psid shall be recorded (reference Addendum I, Page 39, Table 5 of this report). Pressure of regulated gas supply to solenoid valve shan be 70 psig. Regula:Or inlet and outlet pressures shall be rec rded. The type of gas being used shall be recorded. I Se voltages to the solencid shall be recorded. The voltages to the limit switches shall be recorded. ne functienability of indicater lights and proper indication of
" closed" and "open" shall be recorded.
2.0 PROCE00RES The test item was wired electrically to a variable D.C. power supply to operate the solenoid and limit switches. "he GN2 source was
- plumbed to the test specimen regulator. The test item was cperated at 90 VDC, 125 VDC and 140 V c, frem closed to full-open to closed at each voltage. The regulated GN2 pressure
- : the regulator and to the j solenoid was visually menitored. The GN2 pressure was 140 psig to the j
l t f regulater and 70 psig to the solenoid. l WYLE t.AaceATosses m,ni m = P unay
FaGE NO. II-2 TEST REPORT NO. 45088-1
.)
2.0 PPCCIDUES (continued) The test itan's operating time at each vol. age was measured by monitoring the electrical signals to the solenoid and limit switches on an oscillograph. The functionability of the lanps on the test item control box was visually monitored and recorded. Additionally, the solenoid coil resistance was measured and recorded, ne centact resistances of the limit switches were naasured and recorded. 3.0 ES C.".1 "he test item was subjected to the tests regaired by Paragraph 1.0. The tests were condu.ted as outlined in Paragraph 2.0 above. *he test item complied with all regairements without exception. There was no seat leakage observed at 75 paid. "'he lights on the control bcx were functional, indicating open or closed as reTaired. he valve's opening and closing times were as follow: Solenoid Stroke Times C erating voltace Pressure to Solenoid Close to Ocen Coen to Close F. 90 VDC 70 psig 16.75 see 19.88 sec 125 VDC 70 psig 16.80 see 19.35 see 140 VDC 70 psig 17.20 see 19.55 see A typical oscillograph recordi.ng showing valve stroking time is presented in Appendix I. Photographs showing the test setup and instr.: mentation are presented in Appendix :. Oata Sheets showing the data obtained are presented in Appendix :::, and an Instrumenta-
~ tien Ercipnent Sheet is presented in Appendix IV cf this Section.
1 w m i.aaonaromas utowie Fes nety
9510- AXU ACO 3- 50/,0 #1 023 PAGE NO. II-3 TEST REPCRT NO. 45088-1 { APPE.*0IX I TYPIO.;L., CSCIMPAPH PICOEDIG i ( WYLE LASONATORIES wuntevme penry
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9510-AXGACO3-5060 et 02Y paGE too. ( II- 9 TtsT REPomi No. 45088-1
- APPCCIX :::
OATA SHER!S t '4 1
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Page No. ::.10 Report Ms. 45088-1 DATA SHEET Customer risher Centrols Comnany
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Part No. Tv-* C700 AmD. Temp. y yop J b No. aos v -g . c 2 - 5:e:Ji = %. - % ->aaa* '08-19 Photo Ems Report No. ~ oars. 20 Test Med. CN- Start Date Y ~8 - D
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--- Specimen Temp. #M5 /e#
GSI Tegt Title BASELINE rf)N*TIONAL i i 90 VDC 125 VDc ILO vot Tvse of Gas ON. GN. ay_ i
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- 70 ibSI 7D P3 I 7 0 'f2 3 / I Regulater Pressure A QS9 -
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7!**S** "'* Seat Lea < age t. 75 ptra l 're voc /d 5' v O C / 4'o >> O C l fe- sc minu es S e'. r'O L e A CJ 4'e- l l ,,
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Sheet No. / of I ' Approved IA ' s W H- 614 A
9510- AXG ACO3- G 0 68- 9 031 , Page No. II-ll Report No. 45084-1 DATA SHEET ( - Customer hilt 3 e /* bart b /S scuimen Jo A df-- #/v M /ae wYL LAsonAronies Part No. N,D* 9000 Amc. Temp. l'Y#$ 100 No. O_TO S T ~ 0 2 soec. N~ A~ -- T @/fPMoto Y"' Report No. ~ Para. 2h rest ued. CM' start care * - T- F o sin Specimen Temp. b mIoen~'~ GSE AlO re , rwe Li.. z t~,/ I Snler,;cA fR sin % c. : T ,,- m , ~ 1 J +, 3 In th. h 9 3 g. u n ; i l i C ta < f 9-si,# n n L .+ch is 2 a7n n m !_ l OJie- / ~J D r~,t, + . L ,,) 2 - sw;M 'cin, ,,4 I I I GntJ AL,,s c- L;M w2 se s r, n m/,,,, (-.. , lj> ;< . 3 an l u G fa d GJH su,in. A clin,.,) 1 S t n,,;d A% isle e- to Gtwn d . L gn. /2 Ewdc - l
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NO A Written Sheet No. of T A00r0Ved ^'A A b ~ M/I W H-614 A
Page No. II-12 Report No. 45088-1 DATA SHEET wustome7 ris5er Controls Coatoany ') WYLE LABORATORIES S:e*imen "" '"****#1" "'"" Part No. va* 4796 Amb. Temp. Jec No. # U~o 3
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Start Oate # ~~/# ~ PO S .,N
--- Specimen Temp. me W F
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GSI Tegt Title 9a5 EL f NE rt.'Ntit 0Nat I ' 140 VDC 90 VOC 125 VDC Tvoe of Oas GN. GN_ ON_
~
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<-,.--u of Gas to 70 PS I G. T o P s s G. 70 p's I c. :
Regulator Pressure !
,-,... /40 951 rac PSI /?: e:S / \
Outlet: 79[$/ 7o 851 7.1 [S! i Time duration of r., l n-,-,,r-- ._.-1,. \ , Closec to Cpen: /6.7 f SFC / 4 . TO .5 EC . / ?. J C .5 r. C M en to Closed. 10 0 T SEC. r e 4 T S E C. r e_ _e"S SEC ' Indicator Licht Function D /( O'// /") /( 1l I <<-, , . -- <-,.--rs 90,/OC /2 s tiO C rao V.Oc l MS*
- 90 VDC l/.Q5~VOC / 4' C s/ DC l Seat Leakage *. 7S PSID e , i = - - .- . . Ze r. ., Led e , __
f I e Specimen Failed Testec By Cate: # "'/ N ~ I d I See:imen Passed [ witnes[ ~ Oate:
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Approved 'A - M' A I
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W H-614 A J
v.. ~ ,' 9G10- AXUAC03- G068- 4 003 , PAGE W. II 13 k TtsT mapoRT No. 45088-1 "'~
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9G10- AXG ACO 3- 0060 'I l'10 k , ** Tas7 REPORT NC. 4$088 1
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9510-AXGAC03-G068 el 03G PAGE NO. III-l TEST REPCRT No. 45088-1 SECTICN III NCRNAL LCAD CCNDITICNS TESTS 1.0 REQUIRD'.ENTS The test item shall be installed in a test chamber and the test chamber temperature stabilized for 24 hours at 120*F. The test item shall be operated through ten (10) complete stroking cycles. ,, O.e test cha=ber tecperature shall be reduced to ambient temperature and subilized for a period of 24 hours. A seat leakage test shan be perfor=ed using gaseous nitrogen at a differential test pressure of 75 psid. Upcn completion of the above, the same tests shall be repeated. Seat leakage measurements shan be recorded and any measurable increase in
. seat leakage shan be repcrted inunediately to the Fisher Test Engs.neer for evaluation.
j The test chamber shall be stabilized for 24 hours at 140*F. O.e test i item shall be operated through five (5) complete streking cycles. O.e test cha=ber shan be reduced to ambient camperature and stabilired for a period of 24 hours. A sea leak test shall be perfor=ed using water at a differential test pressure of 150 psid. O.e seat leakage shan be collected and measured. Upon ccepletion of the above, the same tests shall be repeated. Seat leakage measurements shall be recorded and any measurable increase in seat leakage shall be reper ed immediately to the Fisher Test Engineer for evaluation. O.e test chamber shan be stabilized for 24 hours at 170*F. O.e test item shan be operated through two (2) ccmplete stroking cycles. O.e test chamber shan be reduced to ambient tamparature and stabilized for a period of 24 hours. A seat leak test shan be performed usmg water at a differential test pressure of 150 paid. O.e seat leakage shan be conected and measured. Upon ecmpletion of the above, the same tests shall be repeated. Se at leakage measurements shall be recorded and any measurable increase in seat leakage shan be reported i= mediately to the Fisher Test Eng:.neer for evaluation.
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2.0 PROCEDURES The test item was placed in a temperature-controlled environmental chamber. The test item was elec rically wired and plumbed to be operational. . The test chamhar temperature was increased to 120'r and stabilized i for 24 hours. The test item was operated through ten (10) complete
" closed" to "open" to " closed" cycles. The voltage to the solenoid valve was 125 VDC. The pressure to the solenoid valve was 70 psig.
Gaseous nit ogen was used to actuate the test item. The test chamber was returned to room ambient cenditions and stabilized for 24 hours. A seat leakage test was performed using gasenus nitrogen at 75 psid as the test media. 25e same series of tests was performed a second time at 120*F. A second seat leakage test was perfermed at room ambient conditions using 4 gaseous nitrogen at 75 psid as the test media. The test chamber temperature was increased to 140*F and stabilized for 24 hours. The test item was operated through five (5) c:nplete " closed" to "open" to " closed" cycles. Se voltage to the solenoid valve was 125 VDC. The pressure to the solenoid valve was 70 psig. Gaseous j nitrogen was used to actuate the test ites. I The test chamber temperature was reduced to room ambient conditions and stabilized for 24 hours. A seat leakage test was performed using water at 150 psid as the test media. The same series of tests was performed a second time at 140*F. A second seat leakage test was performed at room ambient conditions using water at 150 psid as the test media. Se test chamber temperature was increased to 170*F and stabilized for 24 hours. Se test item was operated through two (2) complete " closed" to "open" to " closed" cycles. The voltage to the solenoid valve was 125 VDC. The pressure to the solenoid valve was 70 psig. Gaseous nitrogen was used to actuate the test itas. Se test ckamhar temperature was reduced to room ambient conditions and stabilized for 24 hours. A seat leakage test was performed using water at 150 psid as the test media. The same series of tests was performed a second time at 170*F. A second seat leakage test was, parformed at room ambient conditions using water at 150 paid as the test media. 1 i I WYLE LASORATOINES wasseine pessury A
9G10- AXGACO 3- 0 0 60 #1 037 PAGE NO. III-3 k TEST REPORT NO. 45088-1 3.0 FISULTS
':he test item was subjected to the tests required by Paragraph 1.0.
The tests were perfor:ned as described in Paragraph 2.0. I dare was zero seat leakage past the valve disc after the required temperature transients frca room ambient temperature to 120*F, from roca ambient temperature to 140*F, and fr:m room ambient temperature to 170*F. There were two transients performed at each required temperature. The test item complied with all test regairements without exception. At the req.:est of the Fisher Technical Representative, the test item's disc seat ("T"-ring) w s replaced with a new unit and adjusted to seal at 150 psid across the disc. Typical circular char. recordings showing test chamber temperatures are presented in Appendix I. Photographs showing the test setup and lea.k test equipeant are presented in Appendix II. Data obtained is presented en a Data Sheet in Appendix I!!, and an Instr :=entation f Fgaipment Sheet is presented in Appendix I7 of this Section. s wvu u Tom.
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9G10-AXGACO3-5068-9 097 pm so. III-13 k TEST REPORT No. 45068-1 APPENDIX III
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Page No. : -14 g Reecr* No. 45088-1 ) DATA SHEET Customer FISHER CONTROL 5 20" BUTTERFLY VALy! WYLE LA80 AATORIES Soe:tmen Part No. TYDE #200 Amc. Temp. 78 8 Joe No. 45098 Spec. resugg reo.go REV E Photo I'd5 Report No. Pa ra. 6.0 Test Med. G M' Start Cate M/4/#O S/N -- Specimen Temo, GSI Test Titte N*A' 'W
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1-r rwe Start 120*F 9///,/go dd*/ g No. of 'uff ,teske, (12c r) e /g End 120*r Y//7//d d8//f Leak rate (ON at 75 esid) 2rM O ,
! i !s a-t 120er 9//g/fo o f.VS No. of *utt strewes (120*r) /0 !End 120*F 9//f/88 d EW teak este ION, at 75 osid) EEd'O t ' start is0 r #'zeNo /o:20 ~e. e< <uit it ek., r u.0 ri 5 I )
End IkO*F [2//70 /d l40 Leak rate (H.0 at 150 ostd) E4 4 0 - I I start ILO*r /t2/d o //.' J S ye. essuit strek., tiha r) e f ! End 140*F I[J-T/80 /// 2 S Leak rate (H,0 at 150 ostd) fea sp l l ! Start 170*F [Jf//'o /7/10 No. of #UII strokes (I70*rl k End 170*F Y/!2 f/OD / Tf IC teak -a . (w.c at f co = f 4 N88d
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9G10- AXG AC O 3- 5 0 613- 4 001 e ls PAGE No. IV-1 . TEST REPORT NC. Report No. 45088-1 SECTICN IV PCST-NORMAI. ICAD CONDIT!:N TLN. CTICHAI. ':ESTS 1.0 REQUIRDtENTS . Se requirements for these tests are described in Section II, Paragraph 1.0, of this report. 2.0 PROCEDURES 2.e procedures for these tests are described in Section II, Paragraph 2.0, of this repor.. 3.0 FISU:.TS The test item was subjected to the tests required by Paragraph 1.0. ( ?.e tests were conducted as outlined in Paragraph 2.C. A rotary potentiometer was attached to the actuator position indicator to record the true stroking time of the test item. Previously, the stroking time was :neasured from the signal to the solenoid until
- the appropriate limit switch was actuated.
S.e test item stroking times wre as folicw Stroke Times Voltace to Solencid Pressure to Scienoid Cicsed to Ocen Ceen to Clesed 90 VDC 70 psig 21.60 sec. 20.30 sec. 125 VDC 70 psig 21.60 sec. 20.05 sec. 140 VDC 70 psig 21.60 sec. 19.40 sec.
':hore was zero leakage past the disc at 75 ;sid for 15 minutes.
A typical oscillograph recording is presented in Appendix !. Data obtained is presented on Cata Sheets in Appendix II, and an Instr.=enta-tion Equipment Sheet is presented in Appendix III of this Section. WYLE LASONATORIES
P2g3 No. .'/-2 Report No. 45088-1 r
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- AX S A C03 6 0 68 - 5 PAGE NO. W- 3 TEST REPORT NO. 45088-1 k
APPCiDIX I YPICAL CSCILLOGPAPH RICCFDING
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Customer Fisher Controls Cemeanv' . Specimen 7m" A"*earflu '>=fva ) Part No. Tvne 4700 Amb. Temp. 78'F Job No. O~377*88-2377 2 Spec.Fi ee r Onco-am e . F0P-19 Photo 4'd Fieport No. Para. 2.0 Test Med. CN- Start Date l' '4) Si,N Specimen Temp. A~b
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9010- AXG ACO3- G0 60 'I 061 PAGE NO. V-1 Tgst REPCRT No. 45088-1 g A. SECTION V AGING SLMUI.ATICH 1.0 REQCUEMENTS ,' 9 The test valve assembly shan be subjected to ten (10) alternate cycles of temperat= e and humidity with concurrent streking of the valve during the humidity cycle. The valve shall be stroked using a pressure of 90 psig to the actuator. Each temperature cycle shall be 2.85 days at 237.8'r (108.8'C) . Total exposure at temperat=e shan be 28.5 days (10 cfcles) . Each humidity cycle shall be 48 hours at 140*r (60'C) and 95 percent humidity. Total exposure to humidity shall be 20 days (10 cycles) . The test valve shall be actuated for 1,000 operating cycles which shall be evenly divided between the ten humidity cycles. The voltage to the electrical appurtenances for operating the valve shall be 125 T.4. When j not stroking, the valve shall remain in the closed position. The pressure i to the solenoid shal1~be 90 psig. Both the opening and closing streke times, as measured frem the change in solancid energization to the limit switch contact at the opposite end of travel, shan be ceasured and recorded during the first full cycle stroking operation of each humidity cycle.
"hroughout the aging simulation sequence, the special test fixt=e spool-pieces shan remain in place en the valve. A bell flange shall be attached to the inlet side of the valve test fixture and shall remain in place throughout the aging simulation so that the inist side of the valve can be pressurized when required. The outlet side of the valve fixture shan remain open so as to fully expose the T-ring seal to the test chamber environ =ent.
In order to previde a realistic evaluation of any seat leakage change which might occur during the heat aging simulation, the inlet ten flange shan be pressurized periodically and the seat leakage observed while the valve is experiencing one of the high temperature (227.8*F) cycles. If any leakage is cbserted during this inspection, a bell flange shall .he instaned on the outlet side of the valve test fixture so that the leakage can be collected and measured. This test shall be perfor=ed at the end of the first, fourth, seventh, and last high ta=perature cycles. (Reference Table 5, Page 39, Addendum I of this report.) mm m To Mumswue Pecdoty
DASE NO. V-2 TEST REPORT NO. 45088-1 2.0 PROCEDURES Se test item was placed in the environmental cha ber and made operational. The special spool pieces were bolted in place and remainad in place throughout this test. The "T"-ring was exposed to the r% mhar environment. A blind flange was attached to the inlet side of the test item for leak checking purposes. The pressure to the actuator was 90 psig. The voltage to the solanoid was 125 VDC. The chamber temperature was increased to 228'T and maintained fer a period of 2.85 days (68.4 hours) . A leak cheex using gasecus nitrogen at 75 psid for 5 minutes was performed t.: this temperature. The chamber temperature was decreased to 140*F, 95 !O percent relative humidity, and maintained for 2 days (40 hours) . During this period, the valve was operated through one hundred (100) full strokes from
" closed" to "open" to " closed". The above sequence was repeated for a total of ten (10) times. Leak checks were performed at high temperature (228*F) cycles ene (1) , four (4), seven (7) , and ten (10) .
The valve was stroked a total of 1,000 ti=es from " closed" to "epen" to " closed *, in ten equal segments of 100 strokes each at 140*F. Valve stroke times were recorded and reasured on the first stroke cf each equal sognent. When not stroking, the valve re uined in the cicsed position. , t l' The total time at the high temperature was 28.5 days. The total time at 140'F, 95 percent relative humidity was 20 days.
"'he leak checks at .228'T were perfor=ed as required.
The 1,000 full strokes were perfor:ned at 140*F, 95 M percent relative h.= tid'.t.y in ten equal segments as required. 3.0 _ RESULTS . The test item was, subjected to the tests required by Paragraph 1.0. The tests were conducted as outlined in Paragraph 2.0 above. The test item complied with all specified test requirements, although one (1) anomaly was noted (reference Notice of Anm.aly No.1, Appendix I, this section) . This anomaly is described below. Notice of Ancealy No. la A facility power outage lasting for approxi-mately 30 minutes caused the thermal aging chamber temperature to be out-of-tolerance. The lowest temperature recorded was 210'F. The test was in the second high temperature cycle. The test item showed no evidence of seat leakage at 75 psid for 5 =inutes - in each of the required four (4) leak checks at the high temperature (228 . Muniseene Penmey
9G10- AXGACO 3- 3060- 9 063 . paos No. V-3 k TEST REPCRT No. 45088-1 3.0 Rest 13 (Ccatinued) 2.e test item was successfully stroked through the 1,000 full strcke cycles as required. Che hundred (100) strokes were performed during sach humidity (140*F, 95 + p) cycla. The test itam's st:cke times are shown below: Closed to Coen Ocen to Closed Cycle el 12.38 see 19.55 sec cycle 4101 13.15 see 19.00 see ofele $201 13.44 see 18.23 see cycle $301 12.63 see 16.50 sec ofcle *401 12.35 see 19.19 see Ofele 4501 12.25 sec 20.63 see Cycle 9601 12.13 see 17.25 see Cycle 8701 12.13 see 17.88 see ofcle 9801 12.15 see 17.40 see
\, Cycle #901 12.13 sec 21.44 see Notice of Anomaly No.1 is presented la Appenclx 2. ?fpical circular charts shewing the test chamber environments are presented in Appendix
- . Cecillograph recordings shewing the test item strcke times are presented in Appendix : . Photographs showing the test setup and leak check equipment are presented in Appendix IV. Oata Sheets sheving the leakage data obtained are presented in Appendix 7, and Instr.:=enta-t on Equi;mant Sheets are presented in Appendix V*.
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9G10-AXGACO3-5068 'l 065 . PAGE No. V-5 - TEST REPORT No. 45088-1 APPENDIX I - ICTIC.I T A'EMALY ( WYLE LAacmA7tNum aumeaw amary
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NOTICE OF ANOMALY . 1 WYLE JOB NO. 45088 NOTICE NO. _ P. O. NUMSER: CONTRACT NUMBER: , C TEST EQUIPMENT DATE: 5/9/80 CATEGORY: O $PECIMEN O PROCEDURE Fisher Controls Bill Haslett TO- ATTN: 2S" nuet. siv valse PART NO.
*I PART NAMEt Aging simulation 1. D. NO.
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TEST-SPECIFICATION:FQP-19. Rev. E PARA.NO. 40 NOTIFICATION MADE TO: IIII "**I'** DATE: 5/9/80 E. Campbe1I VIA: Tele done NOTIFICATION MADE BY: l REQUIREMENTS: khe test valve assembly will be subjected to 10 alternate cycles of temperature and humidity with concu'.-rent stroking of the valve during each humidity cycle. Each ter perature cycle wl!! be 2.85 cays ar. 227.8*F (108.8*C).
~
DESCRIPTION OF ANOMALY:
- A facility power outage lasting for 230 .eInutes caused the thermal aging chamber
-
- be out of the required test temperature. The lowest temperature recorded was ,
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. The test was in the second high tersperature cycle.
DISPOSITION - COMMENTS - RECOMMENDATlONS: At Wyle Laboratories' suggestion and with the customer's approval. 30 minutes will be added to the test at the end of the second high temperature cycle, , I cisTaeeUTloN: TEST WITNESS ENGINEER QI on,ase Dem. QUALITY CONTROL N 2 c.
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9G10-AXGACO3-G060-9 100 . PAGE NO. VI-l TEST MEPORT NO. 45088-1 SEC:'ICN VI PCST-AGING SIMUI.ATICN FUNCTICNAI. TESTS 1.0 RzQUIREMENTS At the conclusion of the entire aging simulation sequence, the valve assembly shall be stabilized at ambient temperature and functional tests performed. The seat leakage test at this point shall be performed for infor=ati n only because of the unrealisti: nature of the compression set which is expected to occur dur:.ng the high temperature phase of the aging simulation. Following the functional tests described above, the T-ring seal shall be readjusted fer a shut-off pressure differential of 75 ;sid. Follcwing readjust =ent of the T-ring seal, functional tests shall be perfor=ed. 2.0 PRCCEDURES
?.e procedures for these tests are described in Section ::, Paragraph
( 2.0, cf this repcrt. t 3.0 PESUI.TS The test ites was sub3ected to the tests required by Paragraph 1.0. The tests were conducted as outlined in Paragraph 2.0 above. ~here was one (1) Notice of Ancmaly written and described belcw. Af ter the O.er=al/ Cycle Aging Test was ecmpleted, the following anomalies were observed: The flexible cerhalt fr:m the junction box to the contr *. box was split or cracked in 3 places. A quantit/ of ichricant (* 1 pint) had leaked fr:m the Sectis Actuat.or. The Type EA180 (closed position) Namco I.imit Switch had the nor=al open set of contacts sticking and intermittent. The electrical measurements required by Paragraph 2.0, TCP-19 Pav. F, were not perfor=ed prior to adjusting the
*T2ring per the Customer's request. Cnly streking ti=e and leak checks were ;erformed. O.e seat leakage was 4102 cu/in./
min.cf gaseous nitrogen at 10 psig differential across the fisc. (, I WYLE LASCRATORIES n ucew.sw amuey i i I
PaGE NO. VI-3 TEST REPORT NO. 45088-1 3.0 FISUI.TS (Continued) After adjusting the T-ring, there was :ero leakage across the disc l at 75 psid for 15 :ninutes, and the test item complied with all specified test requirements. The test item's stroke times after the T-ring adjustment are shown I below. Stroke Times Voltage to Solenoid Pressure to Solenoid Closed to open Open to Closed 90 VDC 72 psig 24.00 sec. 18.53 sec. 125 VDC 73 psig 23.95 sec. 18.55 sec. 140 VDC 72 psig 23.50 sec. 18.13 sec. Notice of Ancraly No. 2 is presented in Appendix I. Typical oscillograph recordings are presented in Appendix II. Photographs showing the cracks in the flexible conduit, and the lubricant leak are presented in Appendix
- . Data Sheets showing data obtained are presented in Appendix IV, and an Instru:nentation Equi; cent Sheet is presented in Appendix V of this Se ction. *
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WYLE LABORATORIES P99ftte,iase Fac6 sty
9G10- AXGACO3- 5068- 9 102 , Paos No. VI-3 Ttst Rapont No. 45C88-1 APPENOIX : No C C CT ANCMA:lt (. ( - - , .
PAGE NO. v:-4 TEST RE*0stT NO. 45088-1 NOTICE OF ANOMALY NOTICE NO. 2 P. O. NUMB ER: H-2I7770 WY1.E JO8 NO, b5000 CONTR ACT NUMBER: N /A CATEGORY: D SPECtMEN 3 PROCEDURE C TEST EQUIPVENT DATE; June 26. fe80 TO: 'Isha' CoStreft ATTN: Orfin C inkefus. 3111 wasleet 20" Butterf ly '.'a lve wi th a PART NAME:_ Type T-4208-$R-2-12 BettIs PART NO. 7 von *W Actuator TEST: Ther*al/CveleAcInc I. D. NO. - SPECIFICATION: risher-rop-to a n y. r PAR A. NO. 4.0 and 4.6 NOTIFICATION MADE TO: 83Il Haslett DATE: June 26, 1980 NOTIFICATION MADE BY: Earl Car-obell VIA: Vertal REQUIREMENTS: Each temperature cycle will be 2.85 days at 227.80F (108.80C). Total exposure at temperature will be 28.5 days (10 cycles). 5 Each humidity cycle will be 48 hours at 1400F (600C) and 95+0 per cent humidity.- Total exposure to humidity will be 20 days (10 cycles). The test valve will be actuated for 1,000 operating cycles which will be evenly divided between the ten humidity cycles. DESCRIPTION OF ANOMALY: Af ter the Thermal / Cycle Aging Test was completed, the following anomalies were observed:
- 1) The flexible conduit from the junction box to the control box was split or cracked in 3 places.
- 2) A quantity of tubricant (sp i pint) had leaked from the Bettis Actuator.
- 3) The Type EA180 (closed position) Namco 1.imit Switch has the normal open set of contacts sticking and intermittent.
- 4) The electrical measurements re' quired by P.G. 2.0, FCP-19 Rev. F were not performed per the customer's request. Only stroking time and leak checks were performed. The seal leakage was 4102 cu/In/ min of GN2 *t 10 PSIG differential.
DISPOSITION - COMMENTS - RECOMMENDATIONS: Make "T" Ring (Saal) adjustment and perform functional tests and leak check tests per the customer's request.
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9G10- AXUACO3- 5068- 9 119 paos No. VI 15 inst marcRT No. 45088-1 . I h AFFENDIX iv CATA SIGZTS I D. i - . WYLE LASONATORIES wee.no ame.ty i I
Pcg3 No. VI-16 DATA SHEET aei:o.: no. 45088-1
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d'2C*do O 2S Test Med. CN- S art Cate Dara. sin --- Soe:imen Temp. ' dad. GS: , tusCTt:Nat An too, 7 bac N J~us 7 m a 7 Tent Title l 90 VDC 125 VDC Ike VDC Tvse of Gas ON. 09 09.
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9510-AXGACO3-5060 el 116 Page No. VI-17 DATA SHEET ae w so. 4scas-1 ( Customer Fisher centrets ca.eany Scecimen 9a" ene..rst. v , t .,. WYLE LABOR ATORIES Part No. 'v"* '7"O Amc. Temc. 82 8 Jcc No. Mfo a 5 Specfieha" O^P"**m* - '"8 'S Photo ##f Report No. - Para. L3 Test Mec. CN- Start Date 4 2r #o Si,N
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Page No. VI-18 . D ATA SH EET reper no. 45 a8-1 Custome, Fisher Controls 20" Butterfly Valve WYLE t.A BO A ATORIES Specimen Part No. Type 9200 Amb. Temp. 82 */ Job No. Leone Spec. FQP-19, Rev. E Photo #el ** Report No. Para. 2.0 Test Med. 6 4)
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Specimen Temp. AM A . C,51 Test Title brf tau &l A/Ed I o Solenoid Resistance 3 Terminal 2 to 3 In the box 84// A
- f o Contact Resistance. Switch No. 2 Wire 1 & 2. Centact A& B (Switch closed) 063 ~ rb @ /m.
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- Vf . I t ? Emmene* AE R Ibitch esen) /* 3 # /d M.n @ S'oe VD c-o Contact Resistance. Switch No. 2 Wire 3 & 4. Contact G & H (Switch open) /. 94 /o f Av.cs e goo /c c Ar-blent Temosrature: 8 7, *,#
Relative Humidity: 447, Lishts on Box: d. R .
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9510- AXUACO3- G068- 9 110
. o. v:-1, TEST mePORT reo. 45088-1 I
I APPENDIX Y [
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INSTRUMENTATION EQUIPMENT SHEET Date _ICZi$ Ed Job No. 4 5d 23 d3 Test Area Eno;rneemIal
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Tecimician 4 %< e _ Customer Wacl*r r fe airnk s lype Test Sc/- TInz.cau./ Aoi J Moriel Sertal Wyle or Catitwation Manufactures k h Gov 1 h flange Accesacy On Due No instreament a-too dhb 4 I. _l ..nn el e r- 1 d yirm A s thGQ 482.31:S 'Ifdo3 _. n-tan. s - 57. in . rn rci in =La %o
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- 12. _ Brae r.ud,.- h .t 2mh. ._itu r.-c 23,4 5068-5 I Pag 2 No. VII-5 RepM2 No. 45088-1 MINIMUM REQUIREMENTS FOR RADIATION TESTING l A. Irradiation Performance
- 1. Butterfly Valve
. Start Date 7-4-80 End Date 7-10-80
- 2. Cumulative dosage in air.
- 3. Irradiation geometry (See attached sheet.)
- a. Irradiation chamber or room,
- b. Source location (s), size, quantity, & distance (s) to specimen.
- c. Dosimetry location (s) ,
- d. Specimen location.
- e. Was specimen or source on a conveyor, turntable, or moved during testing? Yes B. Nomenclature:
- 1. Wyle Purchase Order Number: 4-4613-S
- 2. Test Specimen description
- a. Manufacturer: Fisher
- b. Specimen name(s): 20" Butterfly Valve C. Irradiation Source:
- 1. Type of source: Encapsulated source
- 2. Isotoper CO-60
- 3. Type (s) of radiation: Gamma 4 Energy of radiation: 2.5 MEV/ disintegration
- 5. Source quantity or power used for irradiation:
. Approx. 1.1 Mci D. Dosimetry Used:
- 1. Type: Red Perspex
- 2. Manufacturer and model number: Harwell 4034 J
- 3. Accuracy 2%
- 4. Calibration traceability to NBS: Yes.
Latest calibration date - June 6, 1980
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9510 - Ax 5 A C03.5
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P*g3 No. VII-6 0 68-h Report No. 45088-1 O s 4 m': *
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ISOMEQ1X ~. CLIENT: M IS ' Ms- CATE CXPOSURC BCCAN: ?- 4/-Po PURCHASE ORDER: 4/-4%/'d -S DATC EXPOSURC COMPLCTED: 7-/o -Po PROJECT NO. - TOTAL HOURS OF EXPOSURE: 99 TEST ITEM (S) f a ** A,77/rft.f (4:1mc
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m.. I / DISTA::CES: Source guard to midpoind of test item: //o in. Source guard to closest point of test item: /dt. in. Source guard to farthest point of test item: /?f/ in. Number of times that test item was rotated for improved uniformity or cose: M6 (Calculated) Distance Exposure Measured Average COSIMETRY RI;SULTS Dosimoter To Guard Tine Cosc Docc Rato Total Type: No. (in) (hours) (Mrd) (Mrd/hr) Mrd g Harwell Red A 99 A, // /(). 9 B C AECL'Perspex C D PREPARED BY: / c2 /~~ . M DATE 7 .2/-7c7 ISOMEOlX INC. I .. . . . . .
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9G10- AXGACO3-G060-9 126 PAGE NO. VIII-l TEST REPCRT NO. 45088-l SECTICN VIII POST-RADIATICN FUNCTIONAI. *ESTS 1.0 REQUIREMDTS e me requirements for these tests are outlined in Section :, Paragraph 1.0, of this report. I 2.0 PRCCIOURES I The procedures for these tests are described in Sectier. II, Paragraph 2.0, of this report. I I 3.0 RESUI.TS O.e test itas was subjected to the tests required by Paragraph 1.C. The tests were cenducted as described in Paragraph 2.0 above. The test ites ec= plied with all specified test requirements although I{~ one anc=aly was noted (reference Notice of Anomaly No. 3, Appendix I, of this Section), and is described below. g The 1/4" cepper tube, connectdr.g the solenoid valve and versa valve, was bent during shipment. There was gaseous nitregen leakage past the pisten of the pneumatic actuator (Bettis P/N T4203-SR2-12) at a rate of 314.3 cc/sec. . I O.e leakage past the actuator piston stepped after the valve was cperated several times.
"he test item's s rcke ti=es are shown below:
Stroke Times voltace to Solenoid Pressure to Solenoid CIosed to Coen Cten to 01csed 90 VDC 72 psi 25.20 sec 18.75 sec 125 VDC 72 psi 24.00 sec 18.68 see 140 VDC 72 psi 23.75 sec 18.55 see There was zero leakage past the valve disc at 75 ;sid for 15 =inutes. WYLE LABORATOmlES mune n. pecany i
PAGE NO. VIII-2 TEST REPORT NO. 45088-1 3.0 RES*OTS (Continued) Notice of Anomaly No. 3 is presented in Appendix !. A typical oscillograph recording show1.ng valve stroke time is presented in Appendix II. Photogrpahs showing the bent 1/4" copper tube on the versa valve and the test setup are presented in Appendix III. Cata sheets showing the data obtained are presented in Appendix IV, and an Instrzsentation E@tdpment Sheet is presented in Appendix V of this Section. u i l i i i mm -- Hunternie receury 0-
9G10- AXGACO3-G060 el 12D PAGE No. VIII-3 TEST REPORT No. 45088-1 6 4 l t
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APPCCIX I NOTICI CF ANCMAI,Y
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Pcg3 No. VI ~-4 Repor- No. 45089-1 NOTICE OF ANOM ALY 3 P. O. NUMB E R : H-217770 WYLE JOB NO. NOTICE NO. N/A CONTR AC* NUMBER: CATEGORY: U SPECIMEN O PROCEDURE O TEST EOUIPMENT DATE: A'v ?a_ teon Fisher CentreIs ATTN: ^-- d'-k"'" * ' "*** TO.
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PART NO. PART N AMER
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Post-Radiation Functional Test 1. D. NO. TEST-
** " *** PARA.NO.3' c.pfCIFICATION:
NOTIFICATION MADE TO: Bili Haslett DATE: 7-24-80 ar! Ca-eeell VIA: Veetal NOTIFICATION MADE BY: REOUIREMENTS: Following the radiation exocsure, functional tests shall be perfo*med per Section 2.0. The seat leakage test at tnis point will be performed for information only. DESCRIPTION OF ANOMAL.Y: The 1/k" to00er tuDe, connecting the solenoid valve and Versa valve. was ber.t j during sniement. There was GN leakage past the piston of the oneumatic actu- / ator (Bettis P/N T420B-SR2-12)2at a rate of 314 3 cc/sec. DISPOSITION - COMMENTS - RECOMMENDATIONS: The bent copper tube does not impair the operability of the test item. Continue testing per tne Customer's request. o:STResurioN: ENGINEER gi [ ore, c Deet. TEST WITNESS QUALITY CONTROL #% 2 b.
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PROJECT M AN AGER N/b ') f REPRESENT!NG 8T ic co o., , (/ } WYLE LASoRATOR!ES - SCIENT1Ptc SERVicSB AMO SYST9W ORoWP - HUNTSVILLE. ALASAaAA 20S4374411
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H O - AX 5 A LU; 5 0 68-5 PAGE NO. VIII-5 TEST REPORT NO. 45088-1 ( APPE:: DIX II TIPICAL CSCII.LOGRAPH RECORDING ( l 1 i i l l ( WYLE LASORATORIES wurisvine Facany
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9G10- AXGACO3- 5060- 9 132 PAGs NO. VIII-7 ( TEST REPORT NO. 45088-1 8 I I APPENDIX III _ PHOTOGRAPHS
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9G10- AXG AC03- G U 60- 9 139 4 Page No. VIII-9 Report No. 45088-1
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Pcg3 No. VIII-10 Report No. 45088-1
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9G10- AXUACO3-5060 el 136 PAos NC. v:::-11 Test MPORT NC. 45084-1 I i
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Page No. VIII-1 Repor*. No. 45088-1 DATA SHEET Cus:cmer 'iihe" Controit Commanv
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WYLE LABCR ATCRIES
"" *"**-*'iv V-tu, See:imen Fart No. Twa* 8"o Amb. Temp. 9/0 C Joe No, 4_- s i . m
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S pec.F' < '* - Sa-"maa * - fop-19 Photo YE9 Report No. Para. 2.0 Test Med. "N- Start Cate MTb S /,N
--* Specimen Temp.1 - A mt-csi Tegt Title EASEL'NE rustTicyAt 73 4 Q; , a k ,,
I 90 voc 125 VDc ILO VDC -Tves of Oas GN. CN_ *N_ ! fressure
-e s .nss of Gas to . <pg g ;2 Oc G Regulator Pressure i ,-i... -
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! Outlett "? 9sIG *1-P4TG 9174 M > Time duration of l e-.-n.i - a v-1.- fe.ri Closed t6 Cpen: 7.5. 24 MG- TA.co W. T.3. 4 sc.c W A,flosed- t C 'c *n i t ce s er . tt s C 4ee.
Indicator Licht Function a . ic e . t' e. .
~5. .. -- t-1.--t4 4euAt 124 oJ t idoVAc '
Noitage to Limit of.-* gg ege ,4a e .l e Seat Lea < age t.i0 ,..,
'f e r ig .in_..., 75 P*t O ECM L4M uC @ 74~~EST6 a
See : men Failec Testec By M 9' - Cate: 7 U IC
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Sce:: men Passed witness Date: . l NOA Wntten Sheet No. / of 1 Acorovec S - d e A W H- 614 A m-
9G10- AXGAC03-G068- 9 130
. o Page No. VIII-13 Repor*. No. 45088-1
-- DATA SHEET Customer Fisher Controls e W Yl.E LA BO R ATO RIES Spa mn 20" Butterfly Valve Type 9200 Amb. Temp. 9 f
- t: L Co 8 R - e Part No. Job No.
spec, FQP-19, Rev. E Photo YM Report No. " Para. 2.0 Test Med.
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Start Date 'I "lT Ed SlN Specimen Temp. 7- A 'a
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G.Sl est Title N' 7 * ~ k m- Leka \ i o Solenoid Resistance 9 2 2. A i l - Terminal 2 to 3 in the box o Contact Resistance, Switch No. 2 gg m.,gg., A Qgg
- Vire 1 s 2. ceneact A &B (Switch closed) e e- . .. s .;....r. or .+ wn ? 1C. 6 m \\ , Am< @lWh_
- Vire 3 & 4, Contact G & H (Switch closed) o Solenoid Resistance to Ground d. c, ( x t e 4 M mus M Mec o ce_
( o Contact Resistance. Switch No. 2 \.7_.x,uG M, A m. d 4 c o t/ O C,
- ur-. 1 e1 emn.nr. A en (swiees es.3)
, o Contact Resistance, Switch No. 2 1.-lgx,ic6 M, h . @ geevoc
- Vire 3 & 4, Contact G & H (Switch open)
Ambient Te.moerature: R/ o p-Relative Humidity: 72 % Lights on Box: d. E. l Specimen Failed Tested By <r--L _ T a Cate: Mk ( Specimen Passed Witness - Date: NC A wntten Sheet No. 2- of 2 Approved3,k b.0 4C-M M i W H-614 A
Page No. V;;;.g4 Report No. 45088-1
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Ms page b*.anthna11Y le*t blank. s.
9G10- AXG ACO3- 5068 #1 1/12 4 F sGE NO. IX-1 , k/ TEST AEPCAT NC. 1 43Cgg.1 4 i SECTION IX S EIS.V.:0 SI.WLAT*0N 1.0 TEST REQUIPOL"T:'S Se Seismic Test Progrs= shall be perfor=ed in acccrdance with ce Fisher Centrols Seiscu.c Qualification Plan FQP-23, Revisien 9 (see
~
Addendum ::, Section XV of 21s Test Report), and the specific instructions as g:.ven by the Fisher Centrols Technical Papresentative (see Appendix 7 of this Section) . 1.1 Speci=en Metr. ting I The specimen shall be attached to a 'fyle-fabricated =cunting fixture
,. and the fixture, in turn, shall be placed on the *.fyle Multiaxis Seis=ic Si=ulater Table such that the base of the test fixture shall be flush with the top of the test table. te specimen shall be criented initially such that its longitudinal axis shall be colinear with the lengitudinal axis of the table. For the second orientation of tests, 2e specimen shall be rotated 90 degrees in the horizontal plane.
)
1.2 Resenance Search A 1cw-level (apprcxi=ately 0.2 ; hericentally and vertically) biaxial I sine sweep in each test criantatica shall be performed to establish
=ajcr resonances. The tas:s shall be perfer:ed ever the frequency range of 1 Hz to 40 H: at a sweep rate of one-third ccrave per minute.
The test shall be performed with ce hericental and ver.ical inputs in-phase (0*) and repeated with the inputs cut-of-pnase (13C'! . A resonance is defined as a response in line with the input and with an orfer of =agnitude three (3) times the input. Se tests shall be per-fermed with ce valve in the closed pesi icn with a 75 psig internal air pressure. 1.3 Sine Seat Tests g 1.3.1 Non-crerating Tests The specimen shall be subjected c biaxial sine beat tests in eacn test orientation at the frequencies and input levels shcun in Table IX-: ( (wicin the limita:icns of the test table) . Each sine hea: :es: sha l'. j ) censist cf ten (10) escilla:1cns per beat, five beats per tes frequency, with a wo-second pause between tea:s. ne tosts shall be perfer:ed wi-h l the valve in the closed positien with a 75 psig internal a:.: pressure. , Oe tests shall he perfer:ed with the hericenta' and ertical :.nputs n-Phase (0*) and repeated wi n ce inputs cut-of-phase (130 *) . t WYLE LASCAATORIES p ums..no reca.ev
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#4 QDGE NO. *X-3 TEST 2i?CRI NC. 43053-1 1.0 UST REQU~REENTS
. (Continued) 1.3 Sine Seat Tests (C ntinued) 1.3.1 N:n-0;eratine Tests (Continued)
Af ter testing at 5 Hz, 15 'Ez, 25 Hz, and 33 Hz in ea:h phase in each crienta-ion, the fasteners en the specimen shall be checked for tight-ness. Leese fasteners on the specimen shall be tightened and their locations de :=ented. Prior to each fastener tightness inspe :icn, the specimen shall be :y: led fr:m :lesed to open and back :: :lesed to verify tha: the specimen is still operational. 1.3.2 0;eratin: Tests In additi:n to the sine beat tests described in Paragraph 1.3.1, the speci=en shall be subje :ed o operating tests in each test orientation. Each test shall ::nsist of :y: ling the specimen from elesed to open and back to 02: sed dhile simultaneously exciting the spe:i=en with five (5) biaxialjsine beats. The test duration shall be the time required for the specimen to cycle from closed to epen to closed. The cycling cf the speci=en shall be performed with a 75 psig internal air .:ressure. ~he timing of the five (5) sine beats s'..all be spaced over the eyeling duration such that at least one (1) sine beat is applied during each pertien of the cycle.
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The o.:erating tests shall be perfor=ed at the following frequencies a) Majer resonant frequencies b) Frequency of maximum speci=en response (=easured at the actuator center of gravity) c) Frequency where malfunctions er deviatiens o::urred during the resonance search tests. 1.4 Speci=en A :eleration Reseense Fifteen- (15) unidirectional pie o-electric accelerometers shall be located on the specimen. The placement of the acceler==sters shall be at the discretion of the Fisher Controls Technical Representative. Oscillograph recorders shall provide a record of each accelerometer respense. Tabulated data of the speci=en response accelerometers fr:m the sine beat tests shall be included in the test repo.~.. 1 kVYLE LABORATORHHB numsvaee Facuar I
9G10- AXGACO3-5068- 9 199
. PAGE NO. !X-3
( TEST REPORT NO. 45089-1 1.C T12T PEQUIREME:iTS (Continued) 1.5 Streking Time Tests Streking time tests shall be performed prior to and after the seismic testing. The tests shall involve streking the valve from closed to open to closed using the pushbutt:n centrol bcx pr=vided with de specimen by Fisher Ocntrols. The tests shall be perfor.ad with an internal air pressure of 75 psig in the test fixture. Streking ::se and valve pcsition versus time shall be recorded. 6 1.6 Pressure Inteeritr Tests a Pressure integrity tests shall be performed prior to and after the seismic testing. The tests shall be performed for a three-minute
, period with the speci=en in the open position and an approxi= ate internal air pressure of 75 psig.
1.7 _ Sea *aakace Tests Seat leakage tests shall be performed prior to and after the seissi: g( testing. *he seat leakage tests shall be perfer=ed for a ene-m:.nute peried with appr xi=ately 75 psi air press =e differential across the valve.
' l.3 Pneuma:i Surelf caseous nitr: gen (GN2 ) at pressures of 140 psig and 75 psig shall be provided by Wyle during the test progra=. The 140 psig pressure shall be supplied to the 95H regulator for the Operatien of the specimen.
The 75 psig pressure shall be cennected to the test fixture to perf::= leak tests and to si=ulate in-service leads. 1.9 Electrical Pcwer Electrical pcwer cf 125 VOC f=r operation of the spe:isen shall be furnished by Wyle during the test program. I 1.10 Electrical Menit:ri c Two (2) electrical monitoring channels shall be prtvided during the test progra=. One (1) channel shall =cniter the supply voltage (125 l V::C) to the solenoid valve and the c:her channel shall =cnit:r a
, potentic=eter so that the valve motion can be =easured.
~he streking ti=es of the valve shall be recorded.
I( Scth =enitoring :hannels shall be recorded on an esc 111: graph ree:rder. Any deviati=ns shall be recerfed and the Fisher Occ:rols Techni:21 Kapresentative netified. I I WYLE LA50,RATORIES
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s Pa3E NO. IX-4 TEST RE* ORT NO. 45096-1 1.0 TEST REQUIREMENTS (Continued) 1.11 Pressure Monitorinc
"'hree (3) pressure transducers shall be provided during the test program o monitor the pressures at the following locations:
- 1) Inlet pressure to the 95H regulator
- 2) Outlet pressure of de 95H regulator
- 3) Operating pressure into the actuator cylinder.
The output signals of _the pressure transducers shall be recorded on an oscillograph recordar. A pressure iage shall be used to meniter the 75 psig pressure in the test fixture. s - J 2.0 TIST PROCI3t*RES
;The Seismic Test Program was perferned :.n accordance with the Fisher g Controls Seis=ic Qualification Plan FQP-23, Revision 9 (See Addendum };
II, Section XV of this Test Repert), and the specific instructions of the Fisher Controls Technical Representative as given both verbally - and as documented'in Appendix IV cf this Section.
~
2.1 Specimen Mountin; Procedures
'"e.e specimen was attached to a Wyle-fahricated mounting fixture and the fixture, in turn, was"placed on the Wyle Multiaxis Seismic Simulator Table such that the base of the test fixture was flush with the top of i the test table. The specimen was criented initially fer testing in the
- longitudinal / vertical orientation, as shown in Photograph IX-1 (lengitudinal is in line with flow through the spacinen). Fer the second crientation od tests, the specimen was rotated 90 degrees in the her!.
- ental plane to the lateral / vertical eT*.entation. ,
r l 2.2 Resonance Search P'C.' s- y'u.~r
- .a.
The specimen was p nM >s to low-level (app cx:.=ately 0.2 g horizontally and vertically) biaxial sine sweeps in each test crientation. The tests were performed over the frequency range of 1 Hz to 40 Es with a sweep rate of one-third octave per minute. f 7ne tests were performed with the herisontal and ver.ical inputs ( in-phase (O') and repeated'wis. the inputs out-of-phase (180'). < The tests were,peric med.with the valve in the cicsed pcsitica with ! a 75 psig internal air pressure. 1 l l I WYLE LABORATORIES MuntSv6He Peethey
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T 9510- AX5 ACO3- 5068- 9 196 Pa0E No. IX-5 l TEST REPCRT NC. 45088-1 2.0 TEST PROCE URES (Continued) 2.2 Rescnance Search Procedures (Continued)
, The test program was performed in two (2) test series at the request of the Fisher Controls Techntcal Representative. The resonance search tests were performed in the icngitudinal/ vertical orientation during Test Series I and in the lateral / vertical orientation during Test Series II.
p 2.3 Sine Beat Test P recedure s I 2.3.1 Ncn-Coeratine Test Procedures i The speci=en was subjected to biaxial sine beat tests in each test orientatien at the frequencies and input levels shown in Table IX-I (within I the limitati ns of the test table) . Each sine beat test consisted of ten (10) esci11ations per heat, five beats per test frequency, with a two-secend pause between heats. The tests were performed with the valve in the closed position with a 75 psig internal air pressure. The tests were perferred with the horizen al and vertical inputs in-( phase (O') and repeated with the tnputs cut-of-phase (150 ') . At the directi n of the Fisher C ntrols Technical Representative, two (2) additional non-operating tests (Runs 65 and 86) were performed in i the icngitudinal/ver-ical crientation at a test frequency of 19 E: cut-o f-p ha se . The input level for these two tests was adjusted above the required input (for Test Sertes II) to expose the appurtenances :: the desired accelerations determined by the Fisher Centrols Technt:a1 g Representative. After testing at 5 Hz, 15 Hz, 25 Ez and 33 H: in each phase in each orientation, the fasteners en the specimen were checked f:r tight..ess. Pri== to each fastener tightness inspectien, the specimen was cycled from closed to open and back te closed to verify that the spect=en was still operational.
2.3.2 Creratin
Test Procedtres In addition to the sine beat tests described in Paragraph 2.3.1, the i specimen was subjected to operating tests in each test orientation. Each test censisted of cycling the speciren fres elesed to open and l back to :losed while st=ultanecusly exctting tne spect=en with five (5) biaxial sine beats. The test durati:n was the ti=e required for the speci=en to cycle fr:m closed to open to closed. The cy itng cf the speci=en was perfor=ed witn a 75 psig internal air pressure. The t4"dr.g of the five sine beats was spaced ever the eyeling durati:n as p( fell ws: I WYLE LABORATORIES
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DAGE NO. IX-5 A TEST AEPORT NO. 45088-1 2.0 "TST PROCCURES (Centinued) 2.3.2 0:eratin- Test P ocedures (Continued)
- 1) The firs two (2) sine beats were applied (2 seconds apart) during the stroking cycle from closed to cpen.
- 2) he third sine beat was applied after the speci=en had reached the fully-open position.
- 3) The last two (2) sine beats were applied (2 se: nds apart) during the s reking cycle f:cs open to closed.
All Operating tests after Test Run 78 were performed using the above timing sequence. During Test Run 78, all five (5) beats were applied dur:.n; the closed to open pertien cf the stroking cycle. Test Run 79 was a repeat cf Test Run 72 except the above ti=ing sequence was used. O.e operating tests were perfor ed at the frequencies of =ax1=.:= spe:1:en response determined during the test:.ng described in Paragraph 2.3.1 and at the res:nant frequencies (below 33 Hz) date:=ined during the resonance search testing described in Paragraph 2.2. :;o malfunctions or deviaticas occurred during the resonance search tests. In the longitudinal / vertical criantatien, the operating tests were /\ perfer=ed at the follown.g test frequencies (as directed by the Fishar Cent:bls Technical Represen.ative) : 31.5 Hz, 19 Hz and 15.5 H:, cut-cf-phase 31.5 H:, 22.5 H: and 15.5 Hz, in-phase. n the lateral / vertical orien_ation, the operating tests were perfor=ed at the following test frequencies (as directed by the Fisher Controls Technical Representative): 33 Hz, 30 H:, 17.5 H: and 19 H:, out-of-phase; 30 Hz, 31 Hz and 33 H:, in-phase. 2.4 5:ecimen Aereleration Reseense Procedures Fifteen (15) unidirectional pie o-electric accelerereters were located on the specimen as shown in Photographs IX-2 through IX-5. he place-ment of the accelerometers was at the discretion cf the Fisher Centrols Technical Representative. Oscillograph recceders provided a ree::d of each accelerometer response for all test runs. TM tape ree rders pro-vided a record of each accelerometer response for selected test runs. O.e horizontal and vertical cent:01 ac:elerometers were located on the neck flange of the fixture as shown in Photograph IX-3. WYLE LABORATORIES wunte oe F u aity e
9G10-AXGACO3-G068-9 19G PAGE NO. IX~b k TEST REPCRT NO. 45088-I
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r PAGE NO. *X-6 A TEST RE* ORT NO. 45088-1 2.0 "T30 PROCIOURIS (Continued) 2.5 Strokine Time Test Precedures 3.roking time tests were performed pric: to and after the seis=ic tests. The tests involved stroking the valve frem closed to open and back to closed with an internal air pressure of 75 psig. 5::cking time and valve position versus time were recorded. De specimen was operated using a pushbutton centrol box provided by Fisher Centrols as
. ar: cf the test specimen.
A: the re:;uest of the Fisher Controls Technical Representative, an additional stroking time test was performed prior to re ating the speciran from the longitudinal / vertical orientation to the lateral / vertical orientation. 2.6 Pressure Intecrity Test Precedures Pressure integrity tests were perfomed prior to and after the seismic testing. "he tests were perf:=ed for a three-minute period with the specime. in the open positica and an appr:ximate internal air pressure of 75 psig. The packing seal and retaining ring were cbserved for leakage. A soap solution was used to detect leakage. At the request of the Fisher Controls Technical Representative, an additional pressure integrity test was performed prior to rotating the - specimen from the longitudinal / vertical orientation to the lateral / vertical orientation.
-2.7 seat *.eakace Test Procedures
. Se a leakage tests were performed pric: to and after the seis=ic tests.
'"he sea: leakage tests were performed for a one-minute period with approxi=ately 75 pqig air pressure differential across the valve.
' At the request of the Fisher Centrols Technical Representative, an addi.icnal seat leakage test was performed prier to rotating the specimen from the lengitudinal/ vertical orientation to the lateral / vertical orientation. 2.8 Pneumatics Procedures Gaseous nitrogen (GN 2 ) at pressures of 143 psig and 75 psig was pro-vided by Wyle during the test program. The 143 psig pressure was supplied to the 95H regulator for the operation of the specimen. The 75 psig pressure was connected to the test fixture to perform leak tests and to simulate in-service loads. WYLE LABORATORIES MJmonne Facnay
1 9G10- AXGACO3-5068-1 1G0 l 1 PAGE NO. IX-7 ( TEST RE*CRT NC. 45C88-1 2.0 TEST PRCCIOUPIS (0:ntinued) 2.3 Electrical Powering P-Ocedures Standard electrical power of 125 VOC for operation of the specimen
. was furnished by Wyle during the test progrs=.
2.10 Electrical Monitorine Precedures
, Two (2) electrical =enit ring channels were provided during the tes:
program. Cne channel menit: red the supply voltage (125 VOC) to the
, sciencid valve. The other cha..nel =enitored a ;otenticce er so that the valve motion could be =easured. .
e The str: king ti=es cf the valve were recorded.
. 3cch meni:cring channels were re:Orded en an oscillegraph rec =rder.
2.11 Pressure Menit: ring Precedures Three (3) pressurs transducers were provided during the test pr:gra= to monitor the pressures at the follow . ng locations:
)N
- 1) Inlet .:ressure to the 95H regula.or
- 2) Cutle pressure cf the 95H regulator
- 3) Cperating pressure into the actua cr eflinder.
The output signals of the pressure transducers were re =rded en an I escillegraph ree:rder. A pressure gage was used to menit:r the 75 psig pressure in the test fixture. 3.0 TIST RISCLTS 3.1 S=ecimen Mounting Results The specimen was attached to a Wyle-furnished nounting fixture and the fixture, in turn, was counted to the Wyle Multiaxis Seis=ic Si=u'ater Table as shown in photograph IX-1. WYLE LABORATORIES wuntsee pacihty
PAGE N3. IX-8 TEST REPC9T ho. 45033-1 3.0 TEST REST:.TS -(Continued) 3.2 Resonance Search Results
-'he res:ne.nce search tests are described in Tables IX-II and IX-:::,
' including test run numbers, axes, phase, and input accelerations.
Tra .smissibility plots (the in-line specimen response a::alerometers divided by the control acceleroneters) frem the resonance saaren tests (Test Runs 1, 2, 67 and 98) are presented in Appendix !. As determined by the Fisher 0:ntrols Technical Representative, resonances- (belew 33 Hz) were found in the longitudinal / vertical orien a-ion at 15.5 Hz and 31.5 Hz beth in- and out-of-phase and in the lateral / vertical crientasien at 17.5 Hz, 30 Hz and 33 Hz, cut-of-I phase; 30 H: and 33 Hz, ts-phase. 3.3 Sine Seat Te s: Results 3.3.1 3:n-c;eratine Test Results l , Ouring Test Run 21 (at 16 Hz, in-phase), the mounting bolts whien 4 attach the actuator to- the mounting bracket loosened as described in Uctica cf Anomaly No. 4, Revision 3. , i During Test Run 23 (at 17 Hz, in-phase), Tes: Run 57 (at 14 Hz, out-of-l pha se ) , and Test Run 58 (at 15 Hz, out-of-phase) , the mounting bolts which attach the mounting bracket to the valve body loosened as l described in Notice of Anomaly No. 4, Revision 3, and as shewn in Photographs X-6 and IX-7. L A: the directicn of the Fisher Controls Technical Representative, the
~
' test program was interrupted after Test Run 58 (a 15 H:, cut-of-phase).
The test specimen was rs=cved fr:m the tes: =achine for a re-evaluation of the specimen problems and the testing requirements. Test Runs 1 through SS were performed on July 26 and 27, '1930, and are referred to as Test series I. On September 8,1980, the test pregram was resumed with Test Run 59 (at 16 Hz, out-of-phase) . Test Runs 59 through 169 were performed September 8, 9 and 10,1980, and are referred to as Test Series II. The 7/8"-diameter, Grade 5 fasteners, which attach the bracket to the , actuator were replaced prier to test with Grade 8, socket-head cap l screws and torqued to 340 f t-lbf. The 3/4"-diameter, Grade 5 f asteners, ! which attach the bracket to the valve body, were replaced with Grade 8, ! socket-head cap screws and t=rqued to 215 f t-lbf. In additien to the fastener replacement, the maximum required input level was reduced during Tes Series : (from 4.5 g to 3.0 g), as sn:wn in Table IX- . WYLE LABORATORIES Muntsvene Petshly
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9510- AXUACO3-50 68- 9 152 PAGE NO. IX-9 TEST REPORT NO. 45088-1 3.0 TEST RES'ATS (Centinued) 3.3.1 Ncn-c;erating Test Results (Centinued) .- The enly fastener icoseness detected during Test Series II was during the regularly-scheduled fastener tightness inspection performed after Test Run 116 (at 25 Hz, in-phase). "he 4/5"-diameter, Grade a cap screws which attach the bracket to t. e valve body were retorqued to 215 ft-lbf. No further problems with these fasteners or any others were experienced. Scceth cperatien of the specimen was noted during each stroking cycle i prior to the fastener tightness inspectionst hcwever, problems with
, an indicater light were experienced as descrihed in Notice cf Ancealy Nc. 4, Revision B. Pcst-test inspection at the end of the Seismic I Test Program revealed that the prcblems which were thought to be in connection with the limit swit:h were actually caused by a locse I connection in the j=ction bcx on the speci=en, as doc =ented in Notice of Anomaly No. 4, Revision B, and Photograph IX-8.
Descr:.ptiens of the test runs are centained in Tables IX-II and IX-III, Ecluding run n=ters, test frequency, phase, input levels, and un-filtered speci=en respense accelerations. I Table I'<-IV describes the =axi== desired acceleration levels to whi:h the appurtenances en the test specimen were to he exposed as requested g by the Fisher Ocntrcis Technical Representative. Most of these desired levels were reached at seme point during the regulat:r test pregrs=; how-ever, tw (2) additional tests (Runs 85 and 86) at higher input levels were perf:::ed as directed by the Fisher 0:ntrols Technical Representative g to expcse the j==tien bcx and upper li=it swit:h to the desired accel-eratien levels. In the course of trying to isolate the prcblem with the limit switch, tw (2) centact resistance tests were performed en the pushbutton centrol bex used to operate the test speci=en. Test 1 was perf:rmed after Test Run 124 (at 33 Hz, in-phase) and Test 2 was perfer=ed af ter Test Run 125 (at 40 H:, in-phase). The results of these two tests are included in Appendix II of this Section. With the exception of the pecblems described above and dec=ented 6 g Notice of Ancmaly No. 4, Revision B, it was descnstrated that the specimen possessed sufficient integrity to withstand, without ccm-g pr==ise of structure or =achanical functions, the prescr: bed acn-cperating sine beat testing. 3.3.2 Creratin Test Results i Tacles IX-II and IX-III contain test run descriptions, includ:.ng run nu=bers, test frequency, phase, input levels and stroking times. g S=ceth cpera-icn of the spectren was noted during all cycling tests; however, problems with one of the indicator lights were experienced as
) WYLE LABORATCmES M@f$will8 I 4Cilsfy J
PARE NO. IX-10 TEST REPORT NO. 45088-1 3.0 TEST RESC:.TS (Continued) 3.3.1 C erating Test Results (Continued) described in Paragraph 3.3.1 and Notice of An:caly No. 4, Revision 3. The cause of this problem was deter =ined to be a loose ::nnection in the junction box as shown in Photograph IX-8. With the exception of the problems described above and documented in Notice of Ancznaly No. 4, Revision B, it was demonstrated that the specimen possessed sufficient integrity to withstand, without compr: mise of structure or mechanical fune-J cns, the prescribed operating sine bea testing. 3.4 Seecimen A::eleration Pesconse Results Trans=issibility plots (the in-line specimen response accelerometers divided by the control accelerometers) for the resonance search tests are contained in Appendix I cf this Section. Specimen response unfiltered acceler:seter data (g's) from the sine beat tests are presented in Tables IX-II and IX-III. 3.5 Stroking Time Test Results The opening time was =easured from the time the pushbutton contrcl f energized the solenoid until the movement of the valve disc stepped in the fully-open position. The closing time was measured fr:m the time the pushbutten control de-energized the solenoid until the ecvement of the valve disc stopped in the fully-closed position. The pretest opening and closing ti=es f=r Test Series I were 24.3 seconds and 16.2 seconds, respectively. There was no post-test stroking time tests for Test Series I. The pretest opening and closing times for Test Series II were I5.6 seconds and h.8 se: ends, respectively.
- The mid-test opening and closing times (prior to re-orientation of the test specimen) were 25.1 seconds and 16 sec==ds, respectively.
The post-test opening and closing times were 27.0 seconds and 14.2 seconds, respectively. The longer post-test opening time was the result of a severe leakage in the "Swagalok" fitting which connected a cepper line on the specimen to the inlet of the actuator cylinder. Closer inspection of the leakage at the completion of the Seis=ic Test Program revealed that the flexing cf the c0pper line during the seismic excitation resulted in the fatigue and eventual fract.:re of the copper at the fitting connection, as doc.:mented in Notice of Anecaly No. 4, Revision 3.
"he stroking times for each of -he operating sine beat tests (see Paragraph 2.3.2) as well as prior to each fastener tigh, ness inspec-tion (see Paragraph 2.3.1) are contained in Tables IX-II and IX-III.
9G10- AXGAC03-G060- 9 159 PAGE NO. IX-ll ( TEST REPCRT NO. 45088-1 3.0 TFST FISUI.TS (Centinued) 3.6 Pressure Intecrit_t Test Results The pressure integrity test prior to Test Series I revealed a slight leakage between the retaining ring and the valve body and between the retaining ring and the spool fixture. No packing leakage was obserted. There was no pressure integrity test per-formed at the end of Test Series I. The pressure integrity test pric: to Test Series II revealed a slight leakage at the sa=a locations as observed prior to Test Series I. In addition, a slight packing leakage was cbserved on the actuat:r side of the valve. No packing leakage was observed on the limit switch side of the valve. The leakage cbserved pric to the re-orientati:n of the speci=en was si=ilar to that observed prior to the beginning of Test Series II. The pressure intsgrity test at the completien of Test Series II revealed a slight increase in the previcusly-observed leakage, as shewn in Phe : graphs IX-9 and IX-10. In addition to these previously- { observed leaks, additi:nal leaks were obse: ted in the specimen's pneu=ati: circuit at the filter and at the cutlet of the 95M reg 21at::, as sh wn in Pho:: graph IX-ll. i 3.7 Seat 1eakage Test Rescits No leakage was detected during any of the seat leakage tests perfor:ed pric: tc, during er after the seis=ic tests. 3.8 Pneu=atics Results Sc=e pr:blems were experienced with the pneu=atic cir:ui cf the speci=en as described in Paragraphs 3.5 and 3.6 above and as de::=ented in Notice of Ancmaly No. 4, Revision 3. 3.9 Ilectrical ?cwering Pasults No problems were experienced with providing de electrical powering a requirements. 3.1I Electrical Menitoring Results As described in Paragraph 3.3.1, scoe problems wre experienced with the indicator ligh s on the pushbutton centrol box. I: vas orig:... ally thought that these problems were caused by the faul:y opera:::n Of the upper lisi: swit:h, as docu=ented in Notice of Anc=aly No. 4, Revision ( 3. post-test inspection at the end of the feis=le Test Program revealed ! that the indicator light pr:ble=s were actually caused by a 10cse (an f eventually broken) connection in the juncti:n bcx on the specimen. l WYLS LASONATORIES ums.m. Poemry
PACE NC. *X-12 TEST REPORT NO. 45088-1 3.0 "'IST FISU*TS (Continued) 3.10 riectrical Monitorin- Results (Continued) With the exceptien of the problems described in the foregoing, it was de=enstra ed that the specimen pcssessed sufficient integrity to withstand, without ::= pro =ise of electrical functions, the prescribed si=ulated sais=ic environment. 3.11 Pressure M:.iterine Results It was de enstrated that the specimen possessed sufficient integrity to withs.and, without ce=prc=ise of me:nanical functions, the prescribed si=ulated seis=1: environ =ent. s mmu .. mumevow Feenery L -- -
9G10-AXGACO3-5060-9 1G6 Page No. :x.13 (: navisica 3 9epor*. No. 43cgg.g NOTICE OF ANOM ALy NOTICE NO. 4 M-217773 P. O. NUMBER: WYLE JOS NO. 45CSB CONTAACT NUMSER: N/A CATEGORY: E SPECIMEN C PRCCECURE C TEST ECulPMENT DATE: 9 'M T TO: Fisher 0:ntrols Congany on Milliken ATTN:
, PART N AM E.IU ~ 8"***#f17 V"1"* "***18 A****** FART NO. 605A-1.o TEST: seism:.: si=ulation I. D. NO. N/A SPECIFICATION: Fishe r 707-23. Revisien 9 PARA.NO. 5.0 and 6.c , NOTIFICATION MACE TO: Icn t iliken DATE: 7'2?'90 NOTIFICATION MACE SY: s. Pin.er en/s. Oui.n VIA: verbal I
REQUI R*MENTS: g
- 1) The specinen will he examined for possible daaage follcwing all vicient tests...
- 2) Indi:at:r lights say f;;.eker, fh::er, or din, but nust return es their fully
) il h= nated c ndi:len.
OESCRIPTION OF ANOMALY: .) ( 1A1 Ouring *es: Run 21 (at 16 Hz. in-phase), two (2) mounting bolts (7/8" dia) which attach the Bettis Actua:Or : he mounting bracket iccsened such that excessive relative motion of the Actuator was observed. The safety wire en these fasteners was cut and each was torraed to 150 f -ib.
- 13) During *es Run 23 (at 17 Hz, in-;hase) and again during Test Run 25 (at 19 Nz, in-;hase), the four (4) mounting bolts (3/4" dia) shich attach O w Actua::: neu. ting bracket to e.e valve body 10csened such 9.at excessive I relative ection ef the Actuator was cbserted. The safety wire en e.ese fasteners was cut and each was terraed to 115 f -ib.
- 10) Ouring *es Ru . 57 (at 14 Hz, out-cf-;hase) and again duri..g est Run 58 (at 15 Hz, cut-of-;hase), e.e four (4) 3/4" dia bolts reraired tignteni..g. After rete:Taing to 130 ft-lb (instead of 115 ft-lb), the fasteners continued ::
loosen while atte.pting to set the tes: levels for Test Run 59 (a 16 H:, cut-of phase). After roterraing .o 160 ft-lb and with the applicati:n cf one sine heat at 16 H , the fasteners loosened again. *he four fasteners vers I replaced with new 3/4"-10, Grade 5 holts and ret:rr ed tc 160 f:-lb. With the applicatica of cne sine heat at 16 Hz, the fasteners 10csoned again. I 1D) Post-test inspe::icn at the end =f the seismic test pr: gram revealed a severs leakage in e.e "swagelok" fitting which connected a ==;;er li .e en the s-aciren -I to e.e inle: cf the Actua:Or cylinder. Closer inspection revealed tha: ne flexing =f 2.e cc;;er line during the seisni: exci a:1:n resulted in the ft:17 e and eve..:ual fracture of the copper a: One fi- .i..7 connecti:n. I OistarsuficN: o,..., ee t i : Cee.es C.,etone, Tm witness -.. n y,.
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Page No. IX-14 Ee;Cr* ID . 43233-1 NOTICE OF ANOMALY
- 2) Irra:10 operation of the green indicator light en the push-but-on cont:cl box was Observed du:.ng Test Series I which was thought to be related to a faulty limit switch. Curing Test Series I similar erratic cperation was dete::ed until Test Run 136, at which time the indicator light went out and stayed cu- for the recainder of the test program.
- 570S!!!ON - 00.<C." S - FICO?CT::ATIO::S 1A) At -he dire::icn of the Fisher Centrols To:h.ical Represe .:stive, the tes
- 13) ; :cra= was interrupted after Test Run 58. "he test specimen was removed
- 10) f == the test ma:nine for a re-evaluation of the specimen pr:blems and the tes ing requirements. The test ;rogram was later resu:ned with Test Pm 59 af ter replae:.ng the Grade 5 f asteners with Orade 8 f asteners and af ter reducing the input a::eleration require:nents from 4.5 g to 3.0 g.
- 10) At the direction of the Fisher Controls To:hnical Re; esentative, the damaged end =f the cepper line was repaired and reinstalled into the original Swagelok fit-ing prior to the ;cs -seismic fun icnal tests.
- ) Pes -test inspection at the end of the seisnic test program revealed that the problems which were thought to be in connection with the limit switch were actually caused by a loose connection in the jun= tion box on the specimen.
his loose connection eventually broke and the green indicator lar; would no longer light. The functional operation of the specimen was not affected by the loose or broken c=nnection. At the diree.ica of the Fisher Controls Tech-nical Representative, the broken connection was repaired after the post-seismic functional tests. m msaw passay
e 9G10- AXGACO3-5068- 9 158 Page No. IX-15 Reper: No. 45C88-1 (
,, TABLI 2X-!
SINE BEAT 357 REQUIPE WITS E SIAX2AL INPUT *
- TIST FRI;CINCY ACCII.ERATI"lN LI?E*.,
(Hz) TEST SERIIS I 6 TEST SERIES II i 1.0 1.5 1.5 1.25 2.2 2.2 g 1.6 3.0 3.0 2.0 3.75 3.0 ) 2.5 4.5 3.0 3.15 4.5 3.0 4.0 through 19.0 4.5 3.0 20.0 {' 4.25 3.0 21.0 4.05 3.0 22.0 3.85 3.0 I 23.0 3.65 3.0
. 24.0 3.45 3.0 l
25.0 3.25 3.0 P 26.0 3.05 3.0 27.0 2.95 2.95 28.0 2.75 2.75 I 29.0 2.60 2.60 l i 30.0 2.40 2.40 31.0 2.30 2.30 32.0 2.10 2.10 33.0 2.00 2.00 40.0 2.00 2.00
*Ter actual inputs, see 7thles 2X-II and !%-222
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