ML17320A581

Seismic Simulation & Radiation Test Program on Seven Pressure Switches

ML17320A581
Person / Time
Site:	Cook
Issue date:	10/26/1978
From:	Thornberry R WYLE LABORATORIES
To:
Shared Package
ML17320A578	List: ML17320A576 ML17320A581
References
44285-1, NUDOCS 8307120451
Download: ML17320A581 (62)

Text

0!v SEVEN PRESSURE S '5"C.lZS cQR

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SE/Sl',4)C SIMULATtlON Vest Report REPORT NO.

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'8 I cr WYLE JOB NO 44285 CUSTOMIER P.'0. NO.

PAGE 1 OF PAGE REPORT DATE October 26, 1978 SPEC~F(CAT[ON (S)

See Rof<<ences in Section

7. 0

'1.0 CUSTOMER The Mercoid Corporation ADDRESS 4201 Belmont Avenue, Chicago, Illinois 60641 2 0 TFST SPEC(MEN Seven Prcssure Switches (see Paragraph 5. 2) 3 0 MANUFACTURER The hlercoid Corporation

>.0 SUMViA>cY Seven (7) Pressure S~itches, as described in Paragraph 5-2> hereinafter called the specimens,

<<ere subjected to a Radiation and Seismic Simulation Test Program as required by The Hercoid Corp@ration Purchase Order Number 61733, and Nyle Laboratories'eismic Test: Plan 541/6528-5/ES, dat:ed Hay 19, 1978, Revision A.

The radiation test program consisted of irradiating the non-operative specimens with Cobalt 60.

The seismic test program consisted of resonant search testing anc biaxial sine beat testing in 'each of two test: orientations.

The specimens were instrumented with accelerometcrs, electrically powered, pressurized, and monitored for functional operation during thu seismic test program.

It was demonstrat:cd that t!Iu st)ccimens possessed sufficient int='-rity to wit:hstand, without compromise of st:l.uct:urus or functions, the prescribed simulated seismic environment.

Ala.

1>I c> t 5":.',ional Eng.

License No.

6363 STATE OF ALAOAMA COUNTY OF MADISON James M. Foreman

, t<rrlrlr><tot)t 5)Vol ~),

Ite>)O>cs i)nri Says.

The

~ ~<toro'0><on I'r)nlornecl

~ <1 ll>>5 <el)o< I

~ s ll)e <e\\nll ol

~ conn>lole Jn<l cere><It>sr sor r.tert tests et<It Is lo ll>> >III>>t h<5 5 no)srtertgc lroe 0<)tt Cr> ~ ~ errt)< 5 I I

~

gt>IIS Mtlfn r)nct sren

~ ro 5 lore n)I tl)rs 1 +~

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>lyte,t.l<J 7g Nnl )'V I'lrtfc.' r),trill hrr Ihl' n ~roly ol Mr)<><sr>><, ' l,lh nl At,it>rlrn,l WylCS>eetelrehOSA>IS>yteraS<r))rysetaht)rha>O>1<sr)herfrh>1 ny Ihttrahc>stetntOr eohsn>eeht

CS)r<S)rt<'5. <CS<ttrher trhrh

)ry ~'C 5 t)r I<v'er>>0<5 Cove<i'a ty >tits rcoort PREPARED BY APPA VE BY WYLE Q. A.

L.

>51.

l) IVit.::

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SclCNTIF IC SERVICES At(DSYSTEMS GAOOP RE,PORT HO.

44285-1 4.0 SUl I:lARY (Con tinued)

Table I contains a desc-'pt'on of the sine beat test runs and the actual input accelerations.

Photo@ra"h 1 shows the specimens installed in the s'de-to-side and vertical orientation for biaxial testing on the Nyle Aulciaxis Seismic Simulator Table.

Photocraphs 2 and 3 show the specimen response accelerometer mounting locations.

Appendix I contains the Certification Letter of tne raciat'on test.

Appendix II contains transmissibil'y plots of the spec'men response accelerometers from the resonan" search tests.

Aopendi>; IIX conta'ns tne Inst umentation Log Sheets an" the nstru-mentat'on 2"uipment Sheets.

Appenciz IV contains the Nyle Laboratories'eismic T st "=lan 541/

6528-5/KS, dat d ~lay 19, 1978, Revision A.

The test resu's fo"

. tern 8, as descri"ec in "h iivle Test Prccedur" (Appendix IV), are given in Nyle Laboratories'est RepOrt Yunher 44285-2.

%VI~ U4"-$6%76-"l>m SCI ENTIF IC SERV ICES AND SYSTEMS GROUP PAGE NO.

REPORT NO.

5.0 5.1 TEST. REQUIREMENTS Radiation Test The spec'mens, as described in Paragraph 5.2,

"-hall be uniformly exposec to 6 x 10 RADS ecuiva'ent ai" dose gamma rac'ation.

The specimerts sha' be inoperative during -he 'rradiation tests.

5.2 Soecimen Nountina Bnd Orientation The specimens shall be placed on a Wyle-fab 'ted wall-...ount fixture.

The mounting hole attern in each specimen shall be trans"erred to "he test fixture.

The holes shall be drillep and the specimens attached using three (3) each Grade 2 Numbe 10-32 screws.

The test fixture sha'1 be welded to the test table in each tes" orientation.

The mounting o+ the spec'mens shall simulate the in-service mounting con-figuration as closely as pract'cal.

Item i

Descr'=t'on Pressure Pan~e Te t pressure 1

2 3

6 7

DAW 7023-804B R SS DAW 7023-804B R llS DAW 7023-804B R 12S DAW 7023-804B R 10S DAW 7023-804B R 6S DAN 7023-804B R 15S APNT7041-804 R 33

'0-200 psig 50-1000 -s'g 100-1500 psig 25-600 ps'g 5-i 00 os'-

500-5000 psig 0-50" H20 100 psig 500 psig 5'JO psxg 300 psl,g 50 psig L

0 pslg 28" H2C The specimens snail be ini"ial'y oriented in the (SS/V) or'entat'o>>.

or the seconc test or'entat be rotatec 90 cegrees

'n the horizontal p'ane to ve>>t'ca'(:B/1.'rientat'on.

si"e-to>> si"e anc vert

'a'on, the specimens

=-ha:

5.3 Resonant Search r'zontB'ly Bnd vert sha

be pe

=ormted he sweep rate sht c

the s'rte sweeps A 'w<<le ve 1

',appr'x'atelI 0. 2 g hc s'ne sweep'r.

each

" s= cr'nt "i-n 35 H" "o

. stabli=-h ma.-'or resonances pe" minute.

Transmiss bil' pl'ots

- in the test report.

c 'ly) b'ax'a'

~ 0 iz to a'1 be one oc=ave seal I be 5.4 S ne Beat Tests

'i i f 14<<f

<< i e e o; n osc 0 i ~t.t

=inc bear tests sha

be perfor'.nec bia<ialiy

" "re-haI = cc"a;e l.. ze vals Bill at the <<esonan

<<et uvnc es de ec'ced ul inc>>'e search tes"s escr'hed in Paragraph

5. 've>> the =rect ency rane to 33 i z ~

A t>>aini of 'e (5) ea s sftaI be er o,nec wi tions oe heat a".

a tuo-e'fI( oaSe etween bt'B s

~

The e

performed uith "he her'zontal and vtartical 'nr.uts 'n-"itase and with the inputs out-of-c:hase.

Tht. ~xcita"'on 'n::ut ahai:

he horizont 'ly anc l.ti -:et "i"a'1':, or "o t':;e 'imitations o= ti.e

'ISIS 0'-.~VRP7QKM SCIENTIFIC SERVICES ANQ SYSTEMS GROUP PAGE NO.

REP0RT No.

5.0 5.4 TEST REQUIRE(~IEI"TS (Con tinued)

Sine Beat Tests (Continued) machine.

Zt is 'anticipated that the required inpu" will be obtained at freauencies above approximately 5 Hz.

5.5 Specimen

Response

5.6 A total of fourteen (14) specimen-mounted uniaxial piezo-electric accel-erometers shall be utilized during "he test program.

Placement of the accelerometers shall be at the d'scret'on of the (~lercoid Technical Representative.

Transmissibility plots o" the resonant search in each orientation shall be provided in the test report.'4r Electrical Powerin and Electrical Loadin 120'VAC, 60 Hz, single-phase oower at approximately 11 amperes res's-i'e load shall providea or a ro mall( closed (NC) cortact on items 1

through 6.

120 VAC, 60 Hz, sinale-phase power at approximately 5 amperes resistive load shall be prov'aed for an NC cortact on Item 7.

r 5.7 Electr'al ~aonitcrina Seven (7) electrical monitorinc channe's (one eaci: specimen) s'na' be provided to monitor a

'AC contact o

each switch.

Each channel shall be recorded on an oscillog aph recorder c r'ng the Seismic S'mula--'on e.at Prog-am.

These channels may be "sed to ascertain elec"r'ca co;t'nu'ty, current/voltage levels, spuricus one at'on, contact cehatter, etc. before, during and rter ti:e seismic excita"'cn.

3 ~ 0 Pneumazics GN') oressuxe

=ou>>

esp fo the 3 ec mens l o>>

s descr e

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0"-era-'ooa're-seismic and "ost-se'smic ope at'cra'ests shall be performed by ra'sing anc 'ewer'ng t?>e ooera-'ng

" essure of each svitch abo'.

ser point.

%4~& LABQRA7Cia~m SCIENTIFIC SERVICES ANO SYSTEMS GROUP PAGE NC.

REPORT HO.

pl< 'lgC

(.

I 6.0 PROCEDURES AND RESULTS 6.1 Radiation Test Procedures The specimens, as described in Paragraph 5.2, were un'rmly exposed to 6 x 10 RF.DS.ecuivalent ai" dose gamma radiation..The spec'mens were inoperative during the 'radiat ion tests.

6.1.1 Radiation Test Results lt was demonst ated that the specimens possessed su ficient integrity to withstand, without compromise of structures or f nct'cns, the prescribed rad'tion environment (re erence Ce".tixication Letter in Appendix I).

6 2

S ecimen Nountina and Or'entation Procedures iL)

The specimens were placed on a Nyle-fabricatea wal'-,.o nt fixture.

The mountin~g hole pattern in each specimen was t" ns erred to the test fixture.

The holes were d 'ied and the specimens a"tac;ed usi g three (3) each Grade 2 Number 10-32 crews.

The test fixture was welded to the tes" table in each test or'entation.

The mounting or ti:e spec'mens simu'ated the 'n-serv'ce mounting configurat'on as closely as practical.

The specimens were initially '..stalled on the Seism'c Simulator Table in the SS/V test orientations, as shown in Photogra=n 1.

=-or the second orientation of tests, the spe imens we e

otat d 90 degrees

'.". the ho 'i-zontal plane to the FB/V test orientation.

6.3 Resonant Search Procedures A low-evel

{approximatel ~ 0.'2 g hor'"ont lly and 'vert'ca ly) biax'ane

-weep was performed in the SS/V and the "B/V orienta 'ons.

The

<<ec~ e."c:

<<a. ge cf the sine swee~s was from 1 Hz to 35 iiz at a sweep rate of one oc"ave per minute.

5.3.1 Res"rant Search Resu'"'s Tab'e contains a description of the test runs.

Transmissibit, plots o the specimen response acce'ercmeters rom the resonant search test in each orientaticn are contained 'n Appendix

VJVU-tIMBG"C~tIv;.~'-. ~

SCIENTIF IC SERVICES At40 SYSTEMS GROUP PAGE NO.

nEPORT VO.

6.0 PROCSDUR<'S

~v'D RESULTS (Cor.tinuea) 6.4 Sine Beat Tes" Procedures The specimens were subjected to biaxial sine beat tests in each tes" orientat.'on.

Sine beat tests we" performed at eacn one-half oc< ave frequencv interval over the frequency "ange oz l Hz to 35 Hz, since no resonant frequencies were "ound during the resonant search te'sts.

="ach sine beat test consisted of a train,of rive beats with ten oscillhtions per beat ar d with a minimum two-secona pause between beats.

The minimum excitation input was 1.5 g horizontally and l.0 a vertically, witnin the limitat'or.s c the tes" macnin..

The actual input accelerations are contained. in Table I.

The sine -eat tes"s we e performed with the hor'-

zontal and ver"ical inputs in-pnase ana repeated with tne inputs out-o=-

phase.

6.4.1 Sine Bea>> Tes" Results Xt was demonst ate" that'the spec'mens possessed suz ic'ent s-ructural integr'y to withs"ana the resc ibec biaxial sine beat tes" envirormen-.

Tes" run descriptions, ir.eluding input acce'erations, are p esented

,Table 6.5 Soecimen Res"onse Pzocedu es A total oz =ourteen (14) un'ax'al piezo-electric accelerometers

<frere locatea on the soe i...ens as shcwn 'n Photographs 2 ana 3.

The plac ment of the accele ometers was at the discret'on of the Mercoid Techn'cal Represen""ative.

N tape and oscocra"h recorders provided a record o

each accelerometer response.

Th" hor'zcntal a'ccelerometers were oriented in the si"e-"o-sice direct'on dur'ic "he SS/V testing and re-or'ented to the ""on"- o-back c'rect'on "u '..c -he =B/V "esting.

~

~ J.

Specimen Resccrlse Resul ts ar.smissibi'i-v clo"s o=

he s"..c'...en res"onse acce

~ eroneters from "he rescfIant sea c:1 est 1tl eacn or'n ta: 0 i are ccntairle 1.1 Appendix r r 0 AC Blectr'cawerin" and "=lectr'"a'oa"'n" Proced 'res 120 VAC, 60 Hz, single-pnase

=owe at approximately 11 ar.".peres load was provi "ec

=o a normal'y c'csed

('AC) contact on I"ems 6.

Al o, 120 VnC, 60 Hz, single-chase powe at approx'mately resist've load

<.'as provided for an

.'IC contact on Item i.

resi sti ve amper-s

" V&7~ ~~J~-GRAY~;z'm~

SCIEICTIF IC SERVICES AND SYSTEMS GROUP PAGE NO.

REPORT NO.

442S5 6.0 PROCEDURES PHD RESISTS (Conr'nued) 6.7 Electrical Honitorin Procecures Seven (7) electrical monitoring channels (one each spec'men) were prov'ded to monitor a NC contact of each switch.

Each channe'as recorded on an osc'llograph recorder during the ~Seismic Si..Iulat'on Test Program.

The top te...inal block of Items 1, 2 and 3; the side terminal block of Items 4, 5

ard 6; and the left terminal block of Item 7 were monitored during the test program.

6.7.1 Electrical Yonitorin Results It was demonstrated tha" the specimens possessed su"f'cient ele "rica'ntegrity to withstand the prescribed simulated seismic environment.

No contact chat er or spur'ous operation was recorded d'uring the simu'ated se'smic tes"=ng.

6.8 Pneumatics Procedures

(,'.p GN2 pressure

sources, as desc ibed in Paragraph 5.2, were provided for he spec'mens prior to, during md a ter the prescribed tests.

Qoerat'cnal Test Prccedures P"e-se'smic and post-seism'c operational tests were "e formed by ra'sing anc 'owering the operating pressure of each switch abcut its sea, point.

6.9.1 C"-erat'onal Test Results

= was demonst ared that

". ne spec'mens possessed sufficient in= g ity to withstand the prescribed test =rogram.

func"iona'

~

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V@%5= L"~F;W I 'Il<',.

SCIENTIFIC SLAVICES ANO SYSTEMS GROUP PAGE NO.

REPORT NO.

7.0 REPEBENCES 7.1 Hercoid Corporation Purchase Order NunIber 61733.

7.2 Njle Laboratories'eism c Test Plah 5'4l/6528-5/'S, dated Hav 19,

1978, Revision

.~.

7.3 ZEEE Standard 344-1975 Specification entitled "RecorIzended Practices for Sei mic Qualification o" Class 1 Electrical Ecuipment for Nuclear Po~ser Generating Stations".

PJVt

~". EP'PJ~1t

<<,."."7""::~

SCICNTIFIC SEAVICES AiYDSYSTI!hlS GROUP PAGE NO.

nEPORT NO.

TABLE I TEST RUN LESCRIPTXON SIDE-TO-SIDE/V R ICAL "PONT-TO-BACK/VERTICALAXIS REiN NO.

FREQ.

(Hz)

PHASE INPUT ACCELERATION (a)

HORXZ.

VERT ~

RUN No.

r BEQ.

(H-)

PHASE INPUT ACCELERATION (a)

~

HOR:E.

V R 6

7; 8

10 12 13 15 1-35 1.0 1.4 2.0 2.8 4.0 5.6 8.0 11.3 16.0 2246

32. 0 35.0 35.0

32. 0 In In In In In In Xn Xn I n Xn I n Out Out 0

0.32 0.45 0.65 0.95 1.5 1.5 1.5 1.6 1 ~ 6 1.6 1.6 1.6 0.2

0. 32 0.45 0.65 O.95

'l. 05

l. 05 1

1.2 1.2

1. 05 1.5 27 28 29 30 31 32 33 36 37 38 1-35 X.O 1.4-2.0 2.

8'.0 5.6 8.O 11.3 I

16.0 22.o

32. 0

35. 0 35.0 32.0 In Xn Xn Xn Xn In Xr Ini n

T Xn In Xr.

Ou Out 0.2

0. 32 0.45 0.65

0. 95 1.5 1.5 1.6 I

1,6 1.6 1

0 1.5 3..6 L ~ 0 0.2

0. 32 0.45

0. 65

0. 95

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3..1 1.2 3.2

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ATTACHMENT 2 TO AEP:NRC:0001C

AC'royal

~ COBPOAA'AQR Test Report No.

No. of Pages 4ll f=Oa

• SEISMIC ANll ENYIRONMEfhTAL TESTING OF MERCOID PRESSURE SWITCHES FOR AMERICAN ELECTRIC POWER SERYICE CORPORATION 30ÃAL3 C.

COOK NUCLEAR.PLANT::.

XCCr'r ZS Zan ala j3, OFi ELECT. GZH. SECT. AEPSC, H.

THADSiGTTAL TO DOCUHZi~ITAT OH FILF: 2'-QUIHFD:

MTE& f. Sl YuS 1%0 Purchase Order No.

I I

. SECT. PILL~'i CT>

C Preparedby: ~~

Phil arizi I

Reviewed &

Approved by:~

Ric ard S. Gilfoy Dat

~%

Date r ~,

r Pif sf

TABLE OF CONTENTS SECTION ADMINISTRATIVE DATA

'l.O TEST ITEMS

2. 0 TEST REQUIREMENTS 2.1 RESONANCE SURVEY TEST REQUIREMENTS 2.2 MULTIPLE FREQUENCY TEST REQUIREMENTS 2.3 ENVIRONMENTAL TEST REQUIREMENTS 3.0 TEST PROCEDURES 3.1 TEST t<OUNTING 3.2 TEST MONITORING 3.3 RESONANCE SURVEY 3.4 MULTIPLE FREQUENCY TEST 3.5 OPERATION TEST 3.6 ENVIRONMENTAL TEST 4.0 TEST RESULTS 4.1 RESONANCE SURVEY TEST RESULTS 4.2 l<ULTIPLE FREQUENCY TEST RESULTS 4.3 ENVIRONMENTAL TEST RESULTS TEST EQUIPMENT LISTS FIGURES 1-'11 PAGE 1

'8."

21 Re Tt g 16013-2 I

ENVIRONMENTAL

.r'CSTINa

't TON r,'

l~'ORPORATION Page~

~I

Seismic vibration testing of fifteen (15) various Mercoid pressure switches and one (1) Mercoid

'differential pressure switch and environmental testing of two (2)

Mercoid pressure switches.

Th I<

id C

p i

Chi g

. tL Refer to section 1.0 e ~

~

AETC Test Procedure 16013 American Electric Power Service Corporation Test Procedure No.

EGSP-061280JM, Rev.

4 Fifteen (15) Hercoid pressure switches One (1) Mercoid differential pressure switch Unclassified /

June 26, 1981

.C. Pilotte, P. Lizotte, M. Bastien Sent to Indiana 8 Michigan Power Co.

~

D. C.

Cook Nuclear Plant Operation Dept.

Page

. ESllF4Q CORPORATION

1.4 TEST ITEMS The following -items were submitted by American Electric Power Service Corporation for seismic and environmental testing at Acton Environmental Testing Corporati on (AETC).

Manufacturer:

The Hercoi d Corporati on

Chicago, IL ITEhi NO.

82075 82076

'82077 82078 82079 82080 82081 82082 82083

,82084 82085

. 82086 82087 82088 82089 82090 t<ODEL NO.

DAM-7033-153 DAM-7033-153 DAM-7033-153 DAH-7033-153 DAW-7033-153 DAW-7033-153

. DAM-7023-153 DAW-7033-153 DAH-7033-804 DSW-7233-153 DAH-7023-153 DAM-7023-153 DSM-7233-153 DSW-7233-153 DSM-7233-153 BBE-221-3 RANGE 1

5.

6 7

9 15S 3A 5

6S 13S 1

3A 25S Re poI't Na 16013-2 ENVIRONMENTAL ACTOR k II Page

e 1.0 TEST ITEl~)S (continued)

Items numbers 82075 to 82089 are pressure switches with single-pole/double-thro<<

snap-action switches; one circuit closes as the.other. circuit opens.

The model numbers with the suffix -153 designate units with a single SPDT switch; the model number with the suffix -804 designates a unit with dual SPDT

switches, two close, two open.

Those model numbers with the prefix DAt!- designate units with double adjustment set points, one high. pressure set point and one low pressure set point.

The dif'ference between the high and low set points is the operating differential between "on-off" switch operation.

Those model numbers with the prefix DSH-designate units with single adjustment set points.

The single set point sets the pressure where switch operation

, occurs; the operating differential is fixed.

Item Ho. 82090 is a differential pr essure switch which received a high and a low pressure input.

Switch action is 0

determined by the difference in pressure between the two inputs:

This unit was not electrically 'monitored for switch action during the testing.

A11 16 t'est items were subjected to the seismic vibration testing as specified in section 3.0.

Items 82079 and 82084 were eP rt No. 16013"2 ENVlAONMENTAL TESTlNQ

' 'CTON

)

CORPORATION Pago

I 1.0 TEST ITEMS (continued) also subjected to the environmental test, specified in section 3.0, subsequent to the seismic testing.

RcPol f No 1 601 3-2 CNVIRONML'NTAL

.:'CTOR TESTINQ ty CORPORATION Page~

2.0 TEST RE UIREMENTS 2.1 RESONANCE SURYEY TEST RE UIREHENTS

.The purpose of the resonance survey specified in section 3.3 was to monitor the mechanical response of the test items to determine any resonant frequencies in the seismic bandwidth and to determine each test item's ability to withstand the specified vibration without evidence of mechanical damage or deterioration.

The pressure switches were not pressurized

. during the resonance survey.

2.2 MULTIPLE.FRE UENCY TEST RE UIREMENTS The purpose of the multiple frequency test specified

.in section 3.4 was to determine the test items'bility to

.withstand such vibration without evidence of mechanical

damage, deterioration, false closure of open contacts for longer than 3 milliseconds, or false opening of closed contacts for. longer than 10 milliseconds, or any other interference with proper operation as determined by opera-tional tests performed before and after the multiple frequency vibration.

CNVIRONMENTAL TESTlhKL AGTON paga

2.0 TEST RE UIREMENTS (continued)

The multiple frequency test was conducted in such a

manner that the Test

Response

Spectra (TRS) at which the units were qualified would correspond to the SSE level of the Required

Response

Spectrum (RRS) or, if a failure occur red at that level, to the maximum level at which the unit would fulfillthe above acceptance criteria.

Items 82075 to 82089 were pressurized and electrically monitored as specified in section 3.2.during all multiple frequency vibration testing.

Item. number 82090 was pressurized as specified in section 3.4 but not electrically monitored during the multiple. frequency vibration testing.

2.3 ENVIRONMENTAL TEST RE UIREHENTS The purpose of the environmental test specified in section 3.6 was to determine the test item s ability to withstand the elevated steam temperature and pressure conditions without any evidence of mechanical

damage, deterioration, false opening or closing of contacts, or

.interference with proper operation as determined by operational tests performed before and after the environ-ga 1 601 3-2

,. fmvtnaNMrnrrw

'TESTING

~

ACVON CORPOAATICP4 Page

A

~

2.0 TEST RE UIRENEHTS (continued) mental testing.

The test items were pressurized and electrically monIitored as specified in section 3.6 during the environmental testing.

Re rtNo ENVIMNMENTAI TESTING ACTON COO POR ATION

3.0 TEST PROCEDURES 3.1 TEST MOUNTING Each Mercoid pressure switch was mounted on the vertical surface of.a steel plate vibration test fixture in the manner shown in Figures 1 and 2.

After eacli Hercoid pressure switch was plumbed and mounted, the test fixture/test item assembly was securely attached to the 45'iaxial table of the AETC seismic test facility.

The use of the 45'iaxial. table results in equal horiiontal and vertical input components.

3.2 TFST MONITORING During the multiple frequency vibration testing, test items 82075-82089 were electrically monitored to indicate any spurious opens and closures of the single-pole/double-throw switches.

Across each of the open and closed contacts of the SPDT switches,'

chatter monitoring circuit was connected.

The chatter detector was set to monitor the open contacts for false closures longer than 3 milliseconds and to monitor the closed contacts for false openings longer than 10 milliseconds.

The output from the chatter monitor's gate circuitry was connected to an oscillographic recorder to record when Report No.

ENVlRONMCNTAL TEST1NQ

'CYON

'cemaAmoN page 8

3.0 TEST PROCEDURES (continued) contact chatter occurred in excess of the above specified times.

Each contact set of the SPDT switches was also connected directly to the oscillographic.recorder input circuit to record the switch status and to record false opens and closures.

The visicorder records are included with this test report.

During the resonance survey, test items 82075-82083,

82085, 82086~ 82089 and 82090 were each monitored with one {1) triaxial group of 'three (3) accelerometers to determine each unit s mechanical response.

One triaxial group of three accelerometers wa's also attached to the test fixture to serve as control accelerometers monitoring the test input.

Test items 82084, 82087 and 82088 (tested V

at an earlier date than the above) were each monitored

'with one (1) biaxial group of two (2) accelerometers, with one biaxial group also attached to the test fixture to serve as control accelerometers.

During the multiple frequency vibration test, all test items with the exception of item 82084 were monitored with triaxial groups of accelerometers as described above for the resonance survey.

Item 82084 {tested at an earlier 4NVIRONMENTAl I

TEGTlt'A

,". ACTON CORPORATlCÃ4 Page

3.0 TEST PROCEDURES (continued) date) was monitored with one biaxial group of two accelerometers.

During each set of -tests performed on groups of three Mercoid units, the accelerometers were mounted and numbered as follows:

TRIAXIAL ACCELEROMETER NO.

2 3

AXIS ORI FNTATIOH Front-to-back Side-to-side Vertical ITEM ATTACHED TO

82075, 82078,

82081, 82086 82088~

5 6

Front-to-back Side-to-side

Vertical, 82076,

82079, 82082,

82083, 82087+

7 8

~

9 Front;to-back Side-to-side Yertical

82077, 82080,

82085, 82089, 82090 10ll

à >12 Front-to-back Side-to-side

.=Yertical On test fixture (control)

• During multiple frequency test only - see next table.

Report No.

ENVIRONMENTAL J

TESTINQ ACTON coApoRATlcwi Page

~

~,

3.0 TEST PROCEDURES (continued)

BIAXIAL ACCELEROr~ETER NO.

2 AXIS ORI ENTATION In-axis horizontal Vertical ITEt1 ATTACHED

'TO 82084 3

In-axis horizontal Vertical 82088~

5 6

In-axis hor izontal

.Vertical 82087+.

7 8

In-axis horizontal Vertical On test fix-ture (control)

• During,resonance

.survey on'ly J

1 During the resonance

survey, the output f)'om all accelerometers, through appropriate signal conditioning, was recorded on visicorder recording paper included with this test report.

During the multiple frequency test, the output from the triaxial control accelerometers was used for response spectrum control.

The output from the control accelerometers, through appropriate signal condi-

'tioning, was analyzed by a Spectral Dynamics SD321 Shock Spectrum Analyzer and the X-Y plots of the Test

Response

Spectra are included as part of this test report.

Re rt Na "O"'-2 t NVIRONMENTAL h,

vesmea ACTOR COBPORATlON

.Page

3.0 TEST PROCEDURES (continued)

During the vibration testing, the tlercoid pressure switches were visually monitored for signs of mechanical damage or deterioration.

Item number 82090, the Nercoid differential pressure

switch, was monitored visually only, without any additional electrical monitoring.

3.3 RESONANCE SURVEY The resonance survey consisted of a biaxial sinu-soidal input with peak horizontal and vertical accelera-tion components of 0.2 g at frequencies from 1 to 35 Hz.

The resonance survey was performed at a sweep rate of 1

octave/minute.

For each group of test items, the input was applied in two (2) horizontally perpendicular biaxial directions of excitation as follows:

Front-to-back and vertical Right-.to-left and vertical 3.4 MULTIPLE FRE UENCY TESI The multiple frequency test consisted of a biaxial pseudo-random excitation.

The shaker table test input was recorded on a 14-channel tape recorder, each track having discrete frequency sine beats recorded at a different lip N.~

ENVIRONMENTAL TESTINa

, CLCTON CORPORATION Page~

3.0 TESl PROCEDURES (continued) frequency and delay between beats.

All frequencies were recorded at maximum level.

The outputs from the 14 channels were played back and combined in.a 14-channel mixer which resulted in the pseudo-random multiple frequency test input.

.The indivi-dual mixer channels have attenuation controls so that the.

level of each tape channel output passing through the I

mixer could be controlled.

In this manner, the Test

Response

Spectrum was shaped by controlling the level of the individual frequencies.

/

The test input was adjusted such that the Test Response" Spectrum from the control accelerometer, computed at /=20, 2 1/2X damping, enveloped the appropriate Required

Response

Spectrum

'shown in Figure 10.

The test inputs were applied seven (7) times in each of four (4) horizontally perpendi-cular biaxial directions of excitation.

The test duration for each input was thirty (30) seconds.

The levels of the first five (5) inputs in each biaxial direction were such that the TRS from the control accelero-meter would envelope the OBE RRS shown in Figure 10.

The levels of the sixth and seventh inputs in each biaxial o

16013-2 ENVIRONMENTAl.

TESTINQ

'CTDN PCORPORATION Page

l 3.0 TEST PROCEDURES (continued)

. direction were such that the TRS from the control accelero-meter would envelope the SSE RRS shown in Figure 10.

For each group of test items, the inputs were a'pplied in'our biaxial directions of excitation as follows:

~

Right-to-left and vertical Front-.to-back and vertical Left-to-right~ and vertical Back-to-front and vertical In order to verify that the.test items were operating '

properly, the operational tests specified in section 3.5 were performed prior to the vibration testing of each group of items and before and after test run b7 of the multiple frequency test in each biaxial di rection of excitation.

During each run of the mu'Itiple frequency test, the electri-cal monitoring of the SPDT swi tch contacts, as speci fied in section 3.2, was performed.

For each test item, a pressure input was applied and held constant during each run of the multiple frequency test.

During the, first six test runs in each biaxial direction of excitation, the pressure input was held constant at the Test Condition Pl level (see below).

For the seventh test run, the Ro r) No 16013-2 CNVIRONMENTAL TESnNC ACTON COAPORATlON Pago

3.0 TEST PROCEDURES (continued) pressure input was changed to the level of Test Condition b'2.

The pressure settings to which the set points of'ach test'item were adjusted, the level of the p> essure input for Test Conditions 81 and 82, and the adjustable operating range of each Hercoid pressure switch were as shown in Table l.

~

~

Report iso.

ENVlRONhfEMTAL ACTON CORPORATION Pago

ITEN NO.

ADJUSTABLE OPERATING RANGE PS I6 HIGH PRESSURE SET POIHT, PSIG LOM PRESSURE SET POINT PSIG)

TEST COH DITION Pr1 PS IG TEST CONDITION 42 PSIG 82075 82076 82077 82078 82079 82080 82081 82082 82083 82084 82085 82086 82087 82088 82089 1/8 - 15 1 - 35 2-60 5-100 5 - 150 10 - 300 500 - 5000 1/8 - 20 1 - 35 2 - 60 5-100 300 - 2500 1/8 - 15 1/8 - 20 1 - 35 17 30 50 75 150 2000 10 17 3.8 50 1000 15 10 20 40 120 1000 I-5 10

.'..-.NA 35 700 NA 12 20 40 60 90 190 2500 12 20 60 1250 10 lo 20 15 50 100 800

'30 500 10

tIT.Et< IO.

40JUSTABLE

=

'HKQH '.PRESSURE

.OPERATING SET:P01NT,

'RANGE PS IG> *:<PSIG GLOM IPRESSURE SET 'POINT

'PSIG'EST

= = 'CONDIT'ON 1

PSIG-TEST CONDITION k2 PSIG

~

~

82075 8207,6

.82077 82078 82079 82080 82081 82082

.82083 82084 82085 82086 82087 82088 82089 1/8 - 15 1 - 35 2 - 60 5 - 1.00 5 - 150 10 - 300 500 - 5009 1/8 - 20 1 - 35 2 - 60 6 - 100 300 - 2500 1/8 - 15 1/8 - 20 1-35 7

30 50 75 150 2000

't0 3.8 50

- 'f000

.7 10 20 40 120 1000 I-5 10

...-'JlA 700 NA 12 20 40 60 90 190 2500 40 60 10

'l0 20 15 35 100 800 30 500 10

3.0 TEST PROCEDURES (continued)

Item number 82090, the Hercoid differential pressure

switch, was-supplied with a 13 psig pressure input to its high side and a 12.75 psig pressure input to its low side.

These pressures were maintained constant during the multi-pie frequency te't runs.

For those test items which failed to fulfillthe qualification acceptance criteria during the SSE levels of multiple'frequency testing (test runs I5'6 8 87),

additional testing was done at lower vibration input levels until a maximum level was'etermined at which the unit would qualify.. The additional multiple frequency testing was conducted using RRS curves of 3/4 SSE, 1/2 SSE, and 1/4 SSE as shown in Figure ll.

The additional test runs were each 30 seconds in duration.

3. 5 OPERATIONAL TEST Operational tests were performed on test items 82075-82089 before and after vibration testing as specified in section 3.4, and before and after environmental testing as specified in section 3.6.

The operational status of each Mercoid pressure switch was verified by the following operati on test.

1601 3-2 CNVlRONMEMTAL YKSTlNA Page COAPTATION

3.0 TEST PROCEDURES (continued)

After the set point indicators were adjusted to the values specified in Table 1 of section 3.4, the pressure input was varied above and below the set points and the SPDT switches siere electrically monitored to verify that the contacts changed state.

The contact monitoring was performed using the oscillographic recorder input circuit to record the switch action.

The pressures at which the switching action occurred were observed as the input pressure was varied to below.the low set point and above the high set point.

3.6 ENVIRONMENTAL TEST Following the completion of the multiple frequency vibration test, i.tems 82079 and 82084 were subjected to the following environmental test.

The test items, mounted 'vertically as shown in Figure 1, were pla'ced inside an AETC high pressure test chamber.

The pressure switches were plumbed and wired through the chamber wall such that

~ the switches could be pressurized and electrically monitored during the elevated temperature and pressure test.

RePoI't No 1 601 3 2

ENVlRONMENTAI TI:-STINO ACTOR CORPORATION Page

3.0 TEST PROCEDURES (continued)

The set point indicators on the two test items were set as follows:

ITEN NO.

HIGH SET POINT LOl< SET POINT 82079 82080 75 psig 3.8 psig 55 psig Operational

testing, as specified in section 3.5, was performed on the pressure switches.

After the operational "

testing, the pressure inputs to the switches were set as follows:

ITEt~ NO.

TEST PRESSURE

, 82079 82084 90 psig 25 psig The test chamber was sealed and steam at 15 psig aiid a minimum of 120'C was applied for a minimum of 10 seconds.

The test was considered coranenced when the chamber attained a steady-state temperature of a minimum of 120'C and a

pressure of 15 psig.

The steam temperature and pressure were continuously recorded during the testing.

Report No.

CNVlRONMENTAL msmNa AGTOl'8 '~

Page 12

3.0 TEST PROCEDURES (continued)

The SPDT swi tches were electrically monitored continuously using a chart recorder input circuit to record the switch status.

Following completion of'he high tempera-ture and pressure test, the chamber was vented to atmospheric conditions and the operational test was repeated.

ThIt', pressure inputs to the switches were then set as follows:

ITEM NO.

82079 82084 TEST PRESSURE 50 psig 1 psig The high temperature and pressure test was repeated in the same manner as above.

After the test, the chamber was again vented to atmospheric conditions and a final operational test was performed.

RePOrt'O.

CNVIRONMGNTAL 7ESTINO ACTON CORPORATION Poge 20

4.0 TEST RESULTS

4. 1 RESONANCE SURVEY TEST RESULTS There were no structural resonant frequencies detected for any of the Yiercoid pressure switches in the 1 to 35 Hz frequency band.

, 4.2 MULTIPLE'RE UENCY TEST RESULTS For test items 82075-82083, 82085 and 82086, there was no evidence of mechanical damage, deterioration, false

\\

closure of open contacts for longer than 3 milliseconds or false opening of closed contacts for longer than 10 milli-

seconds, or interference with proper operation detected during or as a result of the multiple frequency test per-formed at the full SSE shown in Figure 10.

For test items 82084 and 82087-82089, there was no evidence of mechanical

damage, deterioration, false closure of.

open 'contacts for longer than 3 milliseconds or false opening of closed contacts for longer than 10 milliseconds,.

or interference with proper operation detected during or as a result of the multiple 'frequency test performed at the following,levels, shown in Figur'e 11.

Report No.

CNV!RONh1LhffAL

'rCSTlNQ ACTON

~

Page ~>

J

~

N l

4.0 TEST RFSULTS (continued)

ITEm NO.

QUALIFICATION LEVELS 1'EST CONDITION /I1 TEST CONDITION j/2 82084 82087 82088 82089 SSE 3/4 SSE SSE 3/4 SSE 3/8 SSE 1/2 SSE'/2 SSE 3/4 SSE 4.3 ENVIRONMENTAL TEST RESULTS For test items 82079 and 82084, there was no evidence of mechanical damage, deterioration, false opening or closing of contacts or interference with proper operation detected during or as a result of the environmental test I

specified.in section 3.6.

RePOrt NO.

ENVlRONMENTAL t

I TESTINO

'CTON

. CORPORATlON Page~

TEST EgiJIPHENT LIST MFGR.

MODEL SER.NO.

RANGE ACCURACY INV.P CAL.FRE Accelerometer Accelerometer Accelerometer Accelerometer Accelerometer Accelerometer Accelerometer Accelerometer Accelerometer

'ccelerometer Earthquake Simulator-Hydraulic Actuator Controller Power Supply Power Supply PCB'CB PCB PCB PCB PCB PCB PCB PCB PCB MTS 302A 302A

'302A 302A

'302A 302A 302A 302A 302A 302A 908.34-01

- 204.63S MTS/Dennison 443.115 Mod. 63 483M23 Shock Spectrum SDC Analyzer Yisicorder HON SD321 906C Yisicorder HON

.960B 715E CO-100A (701 C)

Recorder, X-Y MFE Sweep Oscillator Ling 1772 1773 1774 1

Hz 5 KHz 1

Hz - 5 KHz 1

Hz - 5 KHz 1775

1 Hz - 5 KHz 1777 1779 1780 1781

.- 1805 1807 1

Hz - 5 KHz 1

Hz -'5 KHz 1

Hz - 5 KHz 1

Hz - 5 KHz 1

Hz - 5 KHz 1

Hz - 5 KHz 24" DA max.

DC-200 Hz, 22K force lbs.

%5c/

-'5/o

+5%

. -+5K

+5K ampl.

AC415 6 months AC416 6 months AC417 6 months AC418 6 months AC420 6 months AC422 6 months AC423 6 months AC424 6 months

'AC425 6 months AC426 6 months PE367 6 months 288

'8 99078 9-8687

'I 70154 120

+1Ã NA.

PE384 6 months

+0.5 db PE381 6 months

+1 db RE335 6 months

-1 db RE301 3 months

+0.5X RE342 6 months

+lX SG321 6 months DC to 2000 Hz 120 GPM Max. 3K-5K psi max.

250 Hp 12 channel Xl 8

X5 gain filter frequency 50 Hz Input: 0.1 Hz to 10 KHz Sensitivity31.6 MY to 100 Y F.S.

DC to 2 KHz 12 channels 6" paper DC to 2 KHz 12 channels 6" paper Input: 1=10-100 MY 1-10Y 0.2 Hz to 5.0 KHz O.l to 9.9 octave/minute

TEST EQUIPMENT LIST NAME MFGR.

MODEL SER. NO.

ACCURACY -INV..-".'AL.FRE

Scope, Storage Accelerometer Accelerometer Accelerometer Accelerometer Accelerometer Accelerometer Acce1 erome ter Accelerometer Accelerometer DC Amplifier Power Supply Synthesizer False Contact Monitor TEK PCB PCB PCB PCB PCB PCB PCB PCB PCB HON PCB M/RAD MTX T912 302A 302A 302A 302A 302A 302A 302A

302A, 302A 117 483A 197S 202D T912 B015257 2844 666 672 673 2845 2853 1778 1983 4441 0225TE74

.. 273 19710R 310 DC - 10 MHz Dual Trace 1

Hz 5 KHz 1

Hz - 5 KHz 1

Hz 5 KHz 1 Hz.- 5 KHz 1

Hz - 5 KHz 1

Hz -'5 KHz 1'z - 5 KHz 1

Hz - 5 KHz 1

Hz -'5 KHz 6 Channel.Ol/.02/.05/.1/

.Z/.5/1/2/5/10 12 channel gain Xl Detection:

10 5 100 usec 5/

~507

+5/.

+5/o

+2/0

+Zi AC374 AC375 AC381 AC38Z AC383 AC395 AC421 AC339 AC339 PE409 6 months 6 months 6 f80

6 months 6 months 6 months 6 months 6 months 6 months 6 months PE374 6 months PE393 PE371 6 mo

.,s OS304

. 6 months Oscillator Sweep SDC Servo Amplifier,.DC HON Voltage Ref Source SORE Pressure Indicator USG Pressure Indicator HES Pressure Indicator USG SD114A 117 QR40-2 50489 NA 1404 232 1000-54 20 PI336 H25329 PI371 5 Hz - 5 KHz Dynamic Range:

80.db min.

Gain 0.01/.02/.05/. 1/.2/

.5/1/2/5/10 0-40 VDC 0-2 Amp RIPPLE 150 0 to 200 psi 0-500 psi 250 Div.

0-100 psi uV'EG.

.01Ã

+0.5 psi PI336

+1.0 psi PI305

+17 PI371 6 months 6 months 6 months 6 months

+ll f PE372 6 months

+2 DC PE394 6 months

TEST EQUIPMENT LIST NAME MFGR.

MODEL SER.NO.

RANGE ACCURACY INV.P CAL.FRE.

Pressure Indicator HES Amplifier BB Instrument Filter, Dual

Recorder, X-Y ITH MFE Pressure Indicator USG Visicorder HON MillivoltRecorder BRUSH Power Supply SORE Power Supply SORE Digital Thermometer DORIC Digital Yol ~i ter FLUKE 3088/16.

4302 715 15088 260 40-2 40-2 DS-520 8050A 1404-4 1/4" 25325 1003 35207 70142 0304A 03753 101 107 14954

. '646175

+5ps~

PI321 i year

+15 AM302 6 months

-3Ã AM346 6 months

'+G.55 RE343 6 month+:

6 months 3 months 6 months 6 months 6 months 6 months

+;25Ã PI317' months 0-10,000 psi 1000 Div.

Yolt Gain 1 to 1000 15 Hz to 25 KHz

'l0 -

1 MHz Input: 1-10-100 NV 1-10V Both Channels 24 Channel - Inches

'-1 'db RE348 6 Channel

-+2/o RE318 0-40VDC 0-2Amp RIPPLE 2000V REG..005/

PD331 0-40VDC 0-2Amp RIPPLE 200 uY REG.

.005Ã PD302 Type "T" -310 to +750'F

+2'F TI323

. 10 uY to 1000 VDC - 10 mV to 750

.DC+.03ÃR ML504 VAG True RMS 0-20 Megohms Res.

+2 digits dB voltage 0-15 psi RENTAL EQUIPMENT:.

Honeywell 5600E Recorder 873371 Pressure Transducer 0-200 psia Statham S/N 2702

C/

CiASKC TCD C OvcR.

4 HP KU TAGLC CIKYVRF

~OSC 4RADE 2~ + lO-82 SCRKhlQ TO ATT'ACH SDCCIM< }4 YO FINZdfiZ

bh'ECt COID PR'CS.

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'FIGURE 5 VIBRATION TEST SET-UP BACK-TO-FRONT 8 VERTICAL BIAXIALDIRECTION RePo rt No.

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