Block Diagram Of Deceleration And Strain Measurements The .
3.4 Deceleration and strain measurementsduring a drop impactThe measuring instruments used to measure the deceleration and strainare as follows:Acceleration converterStrain gaugeBridge boxDynamic strainmeasuring instrumentData recorderDigital memorySynchroscopePen recorderKyowa Electronic Instruments Co., Ltd.dittodittoAS-10TA (1000 G(max))KFC-5-D17-16(Orthogonal 45-degree tri-axis type)DB 120KDPM- LOBR270Aduring recording and playback.)cm/sec19isspeedtape(TheDM305Ltd.Iwasaki Electric Co.,SS-5215dittoTYPE-3052CorporationYokogawa ElectricdittoTEAC CorporationFig. (II)-A-App.9 shows the deceleration and strain measurement circuits.Fig. (Il)-A-App.9Block Diagram of Deceleration and Strain Measurementspositions at 0, 90,The acceleration converter is fixed with screws on a plane machined flat atboth ends on the line.180, and 270 degrees of the shell of this packaging body, 320 mm fromThe strain gauge is attached to the packaging body with a cyanoacrylate adhesive. After that,a coating agent is applied to the strain gauge to ensure water resistance.(1)-A.App-25
Fig. (II)-A-App. 10 shows the installation position of the acceleration converter and straingauge.ZA-EdZ axisaxsX axisTop SideXaxis90PDBottom SideC axis(Oblique)7(Vertical)270'J (Comer)[ Fig. (1i)-A-App.10: Acceleration converter(D' Strain gaugeDrop directionInstallation Positions of the Acceleration Converter and Strain GaugeDeceleration and strain readingsThe phenomenal waveform recorded in the data recorder is reproduced to the synchroscopeand pen recorder via the digital memory. Therefore, it is read.The deceleration was read from the waveform whose high-frequency component waseliminated because the high frequency, due to the natural vibration of this packaging body duringdrop impact, is contained in the phenomenal waveform. As shown in Fig. (II)-A-App. 11, thecenter point of each wave is connected to produce a smooth waveform. The peak value at thattime represents the maximum deceleration.(II)-A.App-26
Peak valueTimeFig. (II-A-Aop.llPhenomenal Wave of DecelerationStrain is not greatly influenced by these natural vibrations. In other words, the high-frequency component of this deceleration wave does not greatly influence the strain measurement.This is shown by the simple experiment outlined below.To examine the influence that natural vibrations exert on the acceleration converter and straingauge, the converter and gauge are installed under the same conditions as during a drop test.Then, the shell of the cask body is struck with a hammer. After that, the vibration of theconverter and gauge at that time is examined.The results of this test indicated that no vibration waveform could be observed in the straingauge, although an attenuation curve of 1300 to 2600 Hz (shown in Fig. (II)-A-App. 12) wasobserved in the acceleration converter.IIl-------- V[I-.-V - -"---' "I !-HI 1-"-------1 Div 1.506msr utOu tnW av efo rm of th e r-rS HammerHammer Stroke(II)-A.App-27Ac e e a i n C n er eol w n
3.5 Leakage testTo check for the leakage before and after a drop test, a halogen leakage test (1 x 10'atm. cc/sec) is conducted on the specimen body.Test summary(a)A halogen leakage test is conducted on the O-ring sealing part of the front lid, rotatingplug lid, and penetration hole lid of a 1/2-scale model of the packaging. The halogenleakage test applies the pressure method to measure the leakage rate with a detectionsensitivity of 1 x 106 atm -cc/sec. Enclosed halogen gas has a purity of more than99.9%. Halogen gas is enclosed after the part which holds the gas is exhausted to aboutThe enclosing pressure is 4 kg/cm 2 abs.1 0 t".Test equipment(b)Halogen leak detector(i)a)b)(ii)a)(iii)Suzuki Kosakusho Co., Ltd.Leak detection sensitivityToshiba CorporationLeak detection sensitivitySK AZ-21 x 106 atm-cc/secHAL 6I X 10-6 atm -cc/secStandard leakG.E (USA)Full scaleLS-203 x 10-6 atm cc/sec10 x 10' atm. cc/secHalogen gas (Freon 12)Asahi Flon Gas KogyoPurity of 99.9%3.6 Test resultsTable (II)-A-App.6 is a record of the test results. Fig. (I1)-A-App. 13 shows the accelerationwaveform, while Fig. (II)-A-App. 14 provides photographs taken during a drop test.(1I)-A.App-28
Table (II)-A-App.6 Test Conditions and Measurement Results (1)No.Horizontal drop 1Test name1Test No.WeatherRainDrop test I (-)8 CTemperatureTest date16 : 15, March 7, 1980ObserverMr. Konno and Mr. Uruwashi (the Fast Breeder Reactor DevelopmentHeadquarters, PNC main office)Shock absorberTopB%Humidity(1)Test orderFuel supporting can and dummy pipe AContentsABottom9 mDrop heightMeasurement itemsItemRemarkRecordItemAcceleration (strain gaugetype)maxA2 212G(Z)Contents damageLeak (halogen leak)Acceleration (spring type)0210G (300G),340G (500G)Strain distribution0MaxS2 1404ti (A)Packaging body damage0Not damaged.Lid unit damage0Not damaged.RemarkRecordNot damaged.0No leaks.Shock absorber deformation-Drop attitude and statusStill photograph(in mm)Deformation and damage statusStrain accelerometer" Spring accelerometerV Strain gaugeSProjectionShock absorber deformation00 TheBpackage bounces severalTfomtteosedwtoend.ZV47063STPG withone endclsed B:o STPG wtho: pipeModelt endsopeAcceleration (strain gauge type): Tni-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensorStrain gauge: KFC-5-D 17-16(Il)-A.App-29
Table (II)-A-App.6Test Conditions and Measurement Results (2)No.2Test date13 : 12, March 10, 1980WeatherFineTemperature16.5 0 CObserverMr. Konno (the Fast Breeder Reactor Development Headquarters, PNC main office)Mr. Kano and Mr. Nakamura (the Irradiation Fuel Assembly Testing Room, PNCOarai)Shock absorberTopBBonortHumidity1 32 %(3)Test orderFuel supporting and dummy pipe AContentsA1mDrop heightHorizontal drop 1 Drop test II (center)Test nameTest No.Measurement itemsItemRecordItemRemarkAcceleration (strain gaugetype)maxAl 193G (z)Contents damageAcceleration (spring type)90G (300G)55G16OG(IS0G),(500G)Leak (halogen leak)Omax Si 6511p (A)Packaging body damage0Damaged.Lid unit damage0Not damaged.Strain distributionRemarkRecordNot damaged.0No leaks.Measured at only one point.Shock absorber deformationDrop attitude and statusStill photograph(in mm)Deformation and damage statusM Strain accelerometer4 Spring accelerometerY" Strain gaugeI ProjectionBody absorberPackaging///body .damage" - -- - - /Shock"'Bounded and then dropped whilemoving in the directionRndicated by the arrow.Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(1)-A. App-30/55TI
Table (lF)-A-App.6Test Conditions and Measurement Results (3)No.WeatherFineTemperatureTest date12 : 00, March 10, 1980ObserverPNC mai ofm)Mr. Koo (tb Fast Breeder Rýctor DevelopmaA Headquarters,Mr. Tno, Mr. Kane, ard Mr. Nakamum (the Irradiation Fuel Assembly Testing Room, PNC Oarai)Shock absorberTopBContentsABottom1mDrop heightHorizontal drop 1 Drop test II (eccentric)Test name3Test No.16.5 0 C34 %Humidity(2)Test orderFuel supporting can and dummy pipe AMeasurement itemsItemItemRemarkRecordRecord0Acceleration (strain gaugetype)0maxAl 99G(Z)Contents damageAcceleration (spring type)0255G (50G), 50G (50G)Leak (halogen leak)RemarkNot damaged.maxStrain distributionS3 245 /t (A)Shock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusStill photographDeformation and damage statusM Strain accelerometer(in mmm)" -4 Spring accelerometerV Strain gaugeAL Projection@ absorber damageSShockThe stainless cover is broken partially, .and a hole that is21.5 mm deep is made by the projection.Strikes the projection,IIbouncesThe cover of thisportion is broken.strikes it again.48-V**Slightly strikes the23projection, thenslips off to the side.Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(II)-A.App-31
Table (H)-A-App.6Test Conditions and Measurement Results (4)No.TestNo.4ITest nameHorizontal drop 2Drop test IDrop heightTest date17 00, March 10, 1980ObserverMr. Konno (the Fast Breeder Reactor Development Headquarters, PNC main office)Mr. Toyokawa (the Irradiation Material Testing Room, PNC Oarai)Shock absorberTopBBt 1 Weather I FineAContents160CTemperature9mI Humidity32 %Test order(4)Fuel supporting can and dummy pipe AMeasurement itemsItemRecordAcceleration (strain gaugetype)Acceleration (spring type)0Strain distributionRemarkItemmaxAl 231G (Z)Contents damage190G (300G),320G (500G)Leak (halogen leak)RecordNot damaged.00Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusm Strain accelerometer" Spring accelerometerV Strain gaugeStill photographDeformation and damage statusShock absorber deformationProjectionShock absorber damageEANo leaks.SmaxS3 1038 A (A)Shock absorber deformation Remark3008OG0 OOG1890,S94902318028'.13MM425Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensorStrain gauge: KFC-5-D17-16(II)-A.App-32(in mm)
Table (HI)-A-App.6 Test Conditions and Measurement Results (5)Test No.5Test dateNo.IITest nameHorizontal drop 210 20, March 14, 1980WeatherDrop test II (center)CloudyDrop height80 CTemperatureObserver1mHumidity59 %Test orderShock absorberETopBottmBContents(13)Fuel supporting can and dummy pipe AMeasurement itemsItemRemarkRecordItemRecordRemarkAcceleration (strain gaugetype)0maxAl 124G(Z)Contents damageNot damaged.Acceleration (spring type)090G (150G)Leak (halogen leak)No leaks.Strain distribution0max S1 789a (A)Measurcd at only one point.Shock absorber deformationPackaging body damage0Damaged.Lid unit damage0Not damaged.Drop attitude and statusW Strain accelerometerStill photographDeformation and damage status(in mm)4 Spring accelerometerY Strain gaugeProjectionIBody dent10G6Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(II)-A.App-331
Table (Il-A-App.6 Test Conditions and Measurement Results (6)No.Test No.6[ Test nameHorizontal drop 2Drop test II (eccentric)10 0 CTest date11 : 00, March 11, 1980ObserverMr. Konno (the Fast Breeder Reactor Development Headquarters,PNC)Shock absorberTopBBototmWeatherAFineI TemperatureContentsDrop height1mHumidity27 %Test order(1)Dummy pipe BMeasurement itemsItemRecordRemarkItemAcceleration (strain gaugetype)0maxAl 47G(Z)Contents damageAcceleration (spring type)o25G (50G), 2G (50G)Leak (halogen leak)6oG (150) , 130G (300G)Strain distributionRecord0RemarkNo leaks.maxS3 103t4 (A)Shock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusm",vAStrain accelerometerSpring accelerometerStrain gaugeProjectionDeformation and damage statusShock absorber damage5GaAStill photographBModel pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TAI000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(1)-A.App-34(in mm)33-mm deep on average
Table (I)-A-App.6 Test Conditions and Measurement Results (7)No.Vertical dropTest name7Test No.I WeatherDrop test IFine90CTemperatureTest date17 : 00, March 11, 1980ObserverMr. Konno (the Fast Breeder Reactor Development Headquarters,PNC main office)Shock absorberTopABot.,24 %Humidity(6)Test orderDummy pipe BContentsC9 mDrop height( -)Measurement itemsItemItemRemarkRecordRemarkRecordAcceleration (strain gaugetype)0maxAl 236G(X)Contents damageAcceleration (spring type)0200G (300G),350G (500G)Leak (halogen leak)0No leaks.maxS1 -4551t (A)Strain distributionShock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusStill photograph(in mm)Deformation and damage statusW Strain accelerometer" Spring accelerometerIv Strain gaugeProjectionShock absorber deformation and damageDeformation: 47 nmm on averageAT500G004This part of the shockabsorber sinks.180"t43I 5041Ci7/7497777T-I7-1 T15'(42; 270'W90'54All the bolt holes of the shock absorber exhibit64complex buckling. The bolt holes becomecompletely clogged.ýAModel pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(1)-A.App-3526/7/F/T17717-6
Table (I1)-A-App.6 Test Conditions and Measurement Results (8)No.Vertical drop1 Test name8Test No.WeatherDrop heightDrop test II (center)Fine13.5 0 CI TemperatureTest date16 : 00, March 13, 1980ObserverHeamdqUaft, PNC main office)Mr. Kormo and Mr. Uruwi Me Fast Bremdr Reactor DnIvoecopITIUMr. Masai, Mr. Tsuzuli, and Mr. Kitano (Hig)h-Lvel Radioactive Material L-aboratory Corotruction Group, PNCHumidityI1 m1 37 %(12)Test orderTokai)xShock absorberContentsBETopFuel supporting can and dummy pipe AMeasurement itemsItem0Acceleration (strain gaugeItemRemarkRecordRecordRemarkContents damagemaxAl 75G(X)type)075G (150G)Strain distribution0maxS2 -98ju (A)Shock absorber deformation0See S-8.Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusW Strain accelerometer" .4 Spring accelerometerV Strain gaugel ProjectionI E0Leak (halogen leak)Acceleration (spring type)No leaks.Still photographDeformation and damage statusShock absorber damage-- 0Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(Il)-A.App-364(in mm)
Table (II)-A-App.6Test Conditions and Measurement Results (9)No.Vertical dropTest name9Test No.WeatherFine7-CTemperatureTest date11: 30, March, 12, 1980ObserverMr. Konno (the Fast Breeder Reactor Development Headquarters, PNC main office)Mr. Tsuzuki, Mr. Masai and Mr. Kitano (High-Level Radioactive Material LaboratoryConstruction group, PNC Tokai)Shock absorberTopABottoContentsC1mDrop heightDrop test II (eccentric)30 %Humidity(7)Test orderFuel supporting can and dummy pipe AMeasurement itemsAcceleration (strain gaugetype)maxA2 34G(X)Contents damageLeak (halogen leak)Acceleration (spring type)015G, 17G (50G)Strain distribution0maxS I -74/A (A)Shock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusItemRemarkRecordItem0 Strain accelerometerRecordRemarkNot damaged.0No leaks.Still photograph(in mm)Deformation and damage status" Spring accelerometerV Strain gaugeX ProjectionShock absorber damageAT93-mmn deepIG'90"5050CImj-C0,(.,279'00Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(1)-A.App-37 -,180'
Table (II)-A-App.6 Test Conditions and Measurement Results (10)No.Comer drop10 1 Test nameTest No.WeatherFine14 : 30, March 12, 1980ObserverMr. Konno (the Fast Breeder Reactor Development Headquarters, PNC main office)Humidity9 CTemperatureTest date9mDrop heightDrop test I ( - )1 36 %(8)Test orderMr. Tsuzuki, Mr. Masai and Mr. Kitano (High-Level Radioactive Material LaboratoryConstruction group, PNC Tokai)Shock absorberATopBoutcFuel supporting can and dummy pipe AContentsDMeasurement itemsItem0Acceleration (strain gaugeItemRemarkRecordmaxRemarkRecordContents damage0Not damaged.Leak (halogen leak)0No leaks.Still photograph0Photo. No 10-1-10-20A2 160G(X)type)0Acceleration (spring type)162G (300G)maxS1 -2 18jx (A)Strain distributionShock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusM Strain accelerometer(in mm)Deformation and damage status",Spring accelerometerY' Strain gaugeA ProjectionShock absorber deformation230300300/180615(fModel pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(II)-A.App-38330
Table (II)-A-App.6 Test Conditions and Measurement Results (11)No.Comer dropTest name11Test No.WeatherDrop test II ( - )Fine17: 00, March 12, 1980ObserverMr. Konno (the Fast Breeder Reactor Development Headquarters,PNC main office)Shock absorberTopBotom(9)Test orderDummy pipe BContentsD33 %Humidity8.5 CI TemperatureTest dateA1mDrop heightMeasurement itemsItemItemRemarkRecordAcceleration (strain gaugetype)0maxAl 53G(X)Contents damageAcceleration (spring type)030G, 35G (50G)Leak (halogen leak)Strain distribution0maxS1 731t (A)Shock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusW Strain accelerometerRecord0RemarkNo leaks.Still photograph(in mm)Deformation and damage status" Spring accelerometerVAStrain gaugeProjectionShock absorber damagedeep500G88-mm50G40G180,Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(1)-A. App-39I 80
Table (II)-A-App.6Test Conditions and Measurement Results (12)No.Oblique testname12 -TestTest No.WeatherDrop test IFineI TemperatureTest date13: 30, March 13, 1980ObserverMr. Konno (the Fast Breeder Reactor Development Headquarters, PNC main office)Shock absorberTop9mDrop height( -)130 C34 %Humidity(10)Test orderMr. Tsuzuki, Mr. Masai and Mr. Kitano (High-Level Radioactive Material LaboratoryConstruction group, PNC Tokai)DM"tFuel supporting can and dummy pipe AContentsEMeasurement items and imitation pipe AItemAcceleration (strain gaugetype)0Acceleration (spring type)-ItemRemarkRecordmaxAl 242G(Z)RecordRemarkContents damage0Not damaged.Leak (halogen leak)0No leaks.maxS1 -675ku (A)Strain distributionShock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusStill photographDeformation and damage statusm Strain accelerometer, Spring accelerometery Strain gaugeA1 ProjectionShock absorber deformation Angle"ADropped top first so that the comer30strikes at 270 degrees of the specimen'sorientation.90*1''Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(II)-A.App-40(in mm)of the shock absorber
Table (II)-A-App.6 Test Conditions and Measurement Results (13)Test No.131 Test nameOblique test Drop test II ( - )WeatherFineTemperatureTest date15 : 10, March 13, 1980ObserverMr. Konno and Mr. Uruwashi (tth Fast Bnd&r Reactor Development Headquarters, PNC main offioe)Mr. Yagi, Mr. Matsmnoto, and Mr. Kitm.nura (High-Loyal Radioactive Material Laboratory Construction Group,PNC)DTopShock absorberBottoI ContentsEDummy pipe BMeasurement itemsItemItemRemarkRecordAcceleration (strain gaugetype)0maxA2 44G(Z)Contents damageAcceleration (spring type)030G (150G),25G, 28G (50G)Leak (halogen leak)Record0RemarkNo leaks.maxS2 128/c (B)Strain distributionShock absorber deformation0Packaging body damage0Not damaged.Lid unit damage0Not damaged.Drop attitude and statusStill photograph(in mm)Deformation and damage statusW Strain accelerometer" Spring accelerometer""5G5OGSD T5OG 301y Strain gaugeA ProjectionDropped top first so that the comerstrikes at 270 degrees of the specimen'sorientation.Shock absorber damage38-mm deep! lm-I--Model pipe A: STPG with one end closed, B: STPG with both ends openAcceleration (strain gauge type): Tri-axis acceleration converter AS-TA1000Acceleration (spring type): Acceleration sensor Strain gauge: KFC-5-D17-16(II)-A.App-41
(Test number 1 (Horizontal drop 1, drop test I)SI AA 2Znax 2 1 2 (1iii*1I.-I.4Cýo'),5.0 isec/d i v5.0 i s'ccl/d iv83 A"-;I*.1 "- (: .5. 0In1ssc C./d i vFig. (l)-A-App.13(a) Phenomenal Waveforms Reproduced on a Synchroscopex- 125I/L
((Test number 2 (Horizontal drop 1, drop test II (center)S ,AA IZI11ax,,-I 93 C,i."S\:"7.,.,ill(D2.0Oms.c/d iv5.0 rusCc/dA\2 'III ;iI*'1,17 G.e C'vC.I'-5. 111Fig. (Wl-A-App.13(h)Phenomenal Waveforms Reproduced on a Synchroscopev
((Test number 3 (Horizontal drop 1, drop test II (eccentric)SI AAI ZI[ax 9 9 G. .11',,COC'Itc')M'5.01s ec/dic20 mscc/div0S ,3Aimi x25 5O0-1--1 -*'-*4-I-14-11W10Fig. (IT)-A-Aop.13(c) Phenomenal Waveforms Reproduced on a SynchroscopeSe C/d Iv
((Test number 4 (Horizontal drop 2, drop test I)AIZS IAmaix23 1 Gr:cx-939 /1*1 ,C--1C.)I-,.5.0 cisec/eliv5.0 rnscc/d ivrJ1A2ZSq3Amaxa188 (G.4 / .4.i. ,] ,1"1 , .",t.;.l,. '.'li i. ./IIceaI on5.0 ,n sec/cl i vFig. (Ml-A-ADp.13(d) Phenomenal Waveforms Reprodu-5. 0cedona Synchroscope111Siv;hos.C./d
(fTest number 5 (Horizontal drop 2, drop test II (center)SIAA IZmaXmax 789/L12' (1L,-I:;CiCiC')JA.C')5.0 mscc/di5.0 ISL'C/dl %,A 2VIllax(]GivII,,*,I.C'.5.0 msec/(i vFig. (II)-A-App.13(e) Phenomenal Waveforms Reproduced on a Synchroscopev
Test number 6 (Horizontal drop 2, drop test II (eccentric)S IA; .* -I.11,, 71I-.(1N'k'//0 . .t,*t-.!t2.SI. . . ,.{.*'0.I.Il5.0 msc'c//div"N11-100 /1I.i.20 mnscc/'d.IvS3AIImax7IjI.-20 mst'c./Fig. (ID-A-App.13(f) Phenomenal Waveforms Reproduced on a Synchroscopeli v103/t.
(Test number 7 (Vertical drop, drop test I)S IAA I.XSIii x 23 6 (1r,l t .Ilnaxscc,/d iv*.I-Nrý5.01st'cS5.0.,d' XX00III;I2 '2(1"to 455.0 iii-cc/{livFie. (II)-A-App.13({)Phenomenal Waveforms Reproduced on a Synchroscope-155/t
((Test number 8 (Vertical drop, drop test II (center)S IAA\I Xii;ixin;i\ -53 /75 0Cl*1C'-!1.rnse/' d i v5.0 mscc/d8 2AA 2Xcccx - 98/tG8 CG\.t,v.'I'.,.'7'1tr)\I I'"-\5.0cisc/div;,Aj' 1'5.0 msvc/d i vFig. (fl)-A-App.13(h) Phenomenal Waveforms Reproduced on a Synchroscope
Test number 9 (Vertical drop, drop test II (eccentric)SIAA IXInllaxj2,1 CYiSC''.'ý4tIIISC C/' ir'IaN10 I*311 (GPFie.We¶10In- - Ii.t.f4.5. 0 In C cvA 2X04. .(-)AAp.3iPeoenlWvfomeoueov hocp.,2-74 It:"S'10i max.div"""
((Test number 10 (Comer drop, drop test I)SI :\AIXmINNini;xI I 2 (1-218 /tA"2-o1cccxl*I-.V .i v5.0 Ins c C /5.0 1Ns cc/div'0'0S4 AA 2XLJ.*I.5.0S.I-.s.In ax2. i. 15 8 c/ .-UCIO.5.0 insc/cdiFig. (H)-A-App.13(i). .5.0Phenomenal Waveforms Reproduced on a Synchroscope. .1115cc/di -1. .;-- .v.
((Test number 11 (Comer drop, drop test II)S IAAIX; ."- .-If x5]3,(.7"i .T.-. .1 . fc')5IsS. . . .n.IS. . . : . . . -. .t i.\'C"fI5.0A 2Xi"44Irr,,ii;m x3 8 (141-- 75.0(insecd ivFig. (ID-A-App.13(k) Phenomenal Waveforms Reproduced on a Synchroscopeiseciv(/d
((Test number 12 (Oblique drop, drop test I)A I V, IA2,12 (i11ii1x-.IINi x-G(75/t7i'-JlC'\-,,C11I.45.0 [)s cc/d i v5.0 nisec/d *lvS 4IAA 2/,*N1581x(1IIIa x5. .m sccI/1I'j.C0t05.0in.s.c/.iv5.0.msuc /dIFilg. (MII-A-App.13(i) Phenomenal Waveforms Reproduced on a Synchroscopev18
16-* dcl V-V-(ll)H0Cl)300Gd0041 0 G,, c iiv'1-a0ZnC0CC0CCD*0S.CNZS.OiC-;t74f Udi6.kCCn00CZnCC-flCCS.c-c
Fia. (MI-A-App).14 (a) Bef'ore a Drop Test(11)-A-App. -55
Fig. (1T)-A-App.14(h)Fig. (II)-A-App.14(c)UMHorizontal DropDrop Test 1I on the Shell- 'Fig. (II)-A-App.14(d) Drop TestIIon Circumference of the Shock Absorber(I)-A-App.-56
Fi2. (IM-A-App. 14(e) Horizontal DropFig. (II)-A-App.14(f) Drop Test 11 on the ShellFig. (Il-A-App.14(g) Drop Test 1i on Circumference of the Shock Absorber(II)-A-App.-57
U-Fig. (II)-A-App.14(h) Vertical DropFig. (II)-A-App.14(i)Drop Test II on the Center of the Shock AbsorberFin. (I1)-A-App.14(i)Drop Test II on the End Surface of the Shock Absorber(1)-A-App.-58
CI-.1Cpr6)
Fig. (II)-A-App.14(n) Drop Test II on the Shock Absorber(1)-A-App.-60
3.4 Comparison of the results obtained by evaluation and by a 1/2-scale modelRegarding the deformation value of the shock absorber, for every drop test, the resultobtained on the 1/2-scale model by an analysis applying the same method as used to evaluate theactual packaging is compared with the result obtained by an experimental drop test as shown inTable (II)-A-App.7. All analytical results obtained by drop test I using the code, SHOCK-2,indicate a greater deformation value for the shock absorber compared with the correspondingexperimental results. Therefore, analytical results that are on the safe side are obtained. It ispresumed that the deformation has increased because the contribution by the deformation of thecovering plate is not considered. Regarding the impact deceleration, the values shown in Table(II)-A-App.7 are obtained by adding the effect of the covering plate to the deceleration obtainedby using the code, SHOCK-2, in the same manner as is done when the actual packaging isanalyzed. In the case of impact deceleration, the analytical values are also higher than theexperimental values. Therefore, the values used in the structural evaluation are on the safe side.(1)-A. App-61
Table (II-A-App.7 Comparison of Results Between the 1/2-scale Model Test and Evaluation1/2-model test1/2-model evalu-resultsation results**RemarksDrop test I(1) Vertical drop**Obtained using theAcceleration236 G285 Gsame evaluation methodDeformation47 mm54 mmused for an actual packaging.(2) Horizontal dropAcceleration231 G237 GDeformation63 mm75 mmAcceleration160 G161 GDeformation104 mm107 mm24 mm26 nun93 mm86 mm(3) Comer dropDrop test II(1) Vertical dropDrop on the center of the shockabsorber (Fir-plywood part)Drop on the end part of the shock**Distance between thecenter of gravity and theabsorber (Balsa wood part)impact point of the packaging350 x 1/2 position It is presumed that the(2) Horizontal dropDeformation at the center of the8.5 mmNot penetrated.value has been reducedbecause the target portionouter containerstrikes twice during aDrop on the shock absorber21.5 mm 29 mm88 mm88 mm(3) Comer dropDeformation of the shock absorber(1)-A.App-62drop.
Table (II)-A-App.8 lists the experimental results and the analytical results of the shockabsorber deformation when both drop test I and II are conducted. The 1/2-scale modelevaluation results are higher than the experimental results. They can therefore be assumed tobe on the safe side in terms of the evaluation of deformation. Table (11)-A-App. 8 also lists theanalytical results of the actual packaging. Therefore, the method used to calculate shockabsorber deformation and the impact deceleration of the actual packaging is assumed to beproper.Table (M-A-App.8 Comparison of the 1/2-Scale Model Test, 1/2-Scale Model Evaluation, and Actual PackaginMEvaluation ResultsShock absorber deformationduring drop tests I II(1) Vertical drop(2) Horizontal drop(3) Comer drop1/2-scale modeltest result140 mm85 mm192 mmActual packagingevaluation results1/2-scale modelevaluation results294 mm236 mm410 mm140 mm104 mm195 mmIRemarks* Obtained using thesame evaluation methodused for an actual packaging.A leakage test is conducted before and after 1/2-scale model specimen drop test to indicatethat the engineering criterion is satisfied. (See section C.4 of Chapter II.)Moreover, the outer container, rotating plug fixing part, and penetration hole lid unit arevisually inspected after the drop test is completed to confirm that the outer container is notpenetrated (during drop test II), and that no deformation occurs. Therefore, the structuralevaluation method used for the actual packaging is judged to be proper.(1)-A.App-63
(10)-B THERMAL ANALYSISB.1 OutlineThis section and its appendix describe how to calculate the temperature of every major sectionof this package under both normal and accident test conditions, and also determines thetemperature data required to calculate the thermal stress in Chapter (II), "Structural Evaluation."B.1.1 Features of this Package(1)This packaging is a dry-type packaging basically consisting of an outer container, front andrear shock absorbers, and an inner container as shown in Fig. (I)-1.(2)As shown in Fig. (I)-2, the outer container is made up of a double-cylindrical body shellconsisting of outer and inner shells, and front and rear lid units connected to both ends ofthe shell part. The decay heat generated by the contents stored in the inner container istransferred through the inner container to the inner shell of the outer container, rotatingplug, and shielding plug via radiation and thermal conduction, and is further transferredto the lead shield via thermal conduction. Most of the heat on the lead shield istransferred through the cement layer and heat dispersion fins to the outer shell via thermalconduction, and is finally released into the open air from the outer shell surface of theouter container via natural convection and radiation. Some of the heat from the lead shieldis transferred through the front and rear lid units to the shock absorbers via thermalconduction, and is finally released into the open air through the surface cover steel plateof the shock absorbers via natural convection and radiation.(3)The quantity of heat generated from the contents of this package ranges between 0 and 260W.(4)The pivoting trunnion and rear base plate are fixed to the transport skid as shown in Fig.(I)-3 so that this package remains in a horizontal position during transport.(5)In case of fire, heat will enter this package via the outer shell part of the outer containerand the front and rear shock absorbers. The outer shell part of the outer container isequipped with eight fusible bismuth plugs that release gas generated from the cement layerand resin layer to prevent pressure from increasing in the
(i) Halogen leak detector a) Suzuki Kosakusho Co., Ltd. Leak detection sensitivity b) Toshiba Corporation Leak detection sensitivity SK AZ-2 1 x 106 atm-cc/sec HAL 6 I X 10-6 atm -cc/sec Standard leak a) G.E (USA) Full scale LS-20 3 x 10-6 atm
WIRING DIAGRAM DIRECTORY WARNING: Wiring direct to battery not recommended. Install actuator after ignition switch, or master power switch. Diagram 1 Diagram 2 Diagram 3 Diagram 4 Diagram 5 Diagram 6 Diagram 7 Diagram 8 Diagram 9 Diagram 10 Diagram 11 Diagram 12 Diagram 13 Diagram 14 Diagram 15 On/Off, 12VDC, 3-wire/3-pin, SPST On/Off, 12VDC, 3 .
Snatch Block, Shackle 6:24 Snatch Block, Hook 6:24 Snatch Block, others (page 6:29) 6:25 Tilt Wall Block 6:26 Oilfield Blocks 6:27 - 6:30 Tubing Block 6:27 Manhandler Block 6:28 Derrick Block 6:28 Laydown Block 6:29 Tong Line Block 6:30 Hay Fork Pulley 6:30 Guyline Block 6:30 J-Latches 6:31 T
Consequently, the approximate deceleration based on the static front axle load is: a/g) static (2528)/6300 0.401g Using a deceleration of 0.401g produces a load transfer upon the front axle to further increase the front braking force. MARC1-E4 was developed to make the first and second calculation.
Chapter 6 Geometric Design Page 6 of 12 Figure 5: Parallel type right-turn deceleration lane—for major or minor right-turn lanes. Figure: Taper type right-turn deceleration lane—for major right-turn lanes. Minor Right-Turn Lane Design A minor right-turn lane provides for deceleration from 30 mph on the mainline to the speed
Structured analysis Object-oriented analysis System boundary Context diagram Use case diagram Functionality Data flow diagram Activity diagram Interaction diagrams Data Entity-relationship diagram Class diagram Object diagram Control State diagram State diagram Structured methods System as a set of nested processes accessing system data.
Note: The diagram shown above is for reference only. Use the instructions beginning on the next page to draw your Package diagram. Creating a Package Diagram from the Use Case Diagram The package diagram is a type of class diagram and can be created from a use case diagram. 1. Make sure the Use Case diagram c
Figure 2: A sequence diagram that has incoming and outgoing messages Notice that in Figure 2 the diagram's label begins with the letters "sd," for Sequence Diagram. When using a frame element to enclose a diagram, the diagram's label needs to follow the format of: Diagram Type Diagram Name UML basics: The sequence diagram Page 3 of 24 http .
Spring 2018 :: CSE 502 Simple Interleaved Main Memory Divide memory into n banks, “interleave” addresses across them so that cache-block A is –in bank “A mod n” –at block “A div n” Can access one bank while another one is busy Bank 0 Bank 1 Bank 2 Bank n Block in bank Bank Block 0 Block n Block 2n Block 1 Block n 1 Block .
