ML19340C409
| ML19340C409 | |
| Person / Time | |
|---|---|
| Site: | LaSalle  |
| Issue date: | 10/27/1980 |
| From: | SARGENT & LUNDY, INC. |
| To: | |
| Shared Package | |
| ML19340C408 | List: |
| References | |
| PROC-801027, NUDOCS 8011170211 | |
| Download: ML19340C409 (106) | |
Text
{{#Wiki_filter:;i il o !'s La Salle County 1 !I in Plant SRV Test Plan ! la lI is !I II am is , i ll LA SALLE COUNTY I STATION lI !I !I ll lI Tevision L !I B@l 7$g L Octoaer 27,'980 l il
! Revision 4 I TABLE OF CONTENTS l Page j I. Objectives I-l II. Schedule II-l i Figure II-l II-3 l
- III. Scope i
A. Test Conditions III-l B. Quencher Selection Criteria III-2
- C. Test Matrix III-d i
D. Sensor Requirements III-ll l E. Signal Conditioning System III-14 4 F. Data Acquisit:.or. and Monitoring System III-18 i j G. Processing and Reduction of Recorded Data III-22
- ! H. Test Dcouments III-27 i
I. Implementation III-28
- TABLES j No. of Pages General Nc tes to Tables 2 Table 1 - Accelerometer Data 4
- Table 2 - Pressure Sensor Data 5 i
Table 3 - Temperature Sensor Data 4 Table 4 - Strain Gauge Data 5 l
- SARGENT&LUNDY -
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Revision 4 1 1 j FIGURES .I ! l Figures 1 through 19 including lA 1B, 12A, 13A, 14A, 15A, and ISB f 1 i
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! Figure 1 - Accelerometer Locations ,I Figure lA - Accelerometer Locations Section A-A i l 1 s Figure 1B - Downcomer Accelerometer Locations l I Figure 2 - Sensor Locations in Wet Well and SRV Lines - Deleted j
- Figure 3 -
Strain Gauce on SRV Discharge Line i t Figure 4 - Sensors on SRV Brar.ch ' Connection - Deleted
- Figure 5 -
Downcomer Strain Gauge I 3 I Figure 6 - Strain Gauge on RHR Suction Line fi { Figure 7 - Strain Gauges on Quencher Assembly f a Figure 8 - Strain Gauges on Quencher Support f Figure 9 - Strain Gauges on Containment Liner I j- I. Figure 10 - Pressure Sensor Locations on Column ; i I j Figure 11 - Pressure Sensor Location on Downcomer k Figure 12 - Pressure Sensor Locations In Suppression Pool - Plan 4 i Figure 12A - Pressure Sensor Locations In Suppression Pool - I
- Section I l I Figure 13 -
Pressure Sensor Locations In SRV Discharge Lines Figure 13A - Pressure Sensors on SRV Discharqe Line , Figure 14 - Temperature Sensor Locations In Suppression Pool - Plan Fiqure 14A jl f Temperature Sensor Locations in Suppression Pool - B Section l Figure 15 - Temperature Sensor Locations in SRV Lines
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Revision 4 !I FIGURES 1 ll Figure 15A - Temperature Sensor Mounting on SRV Discharge
- s Lines Figure ISB -
SRV Downcomer Local Temperature Sensors Figure 16 - Identification of SRV Lines Figure 17 - Data Acquisition System l Figure 18 - Leaky Valve Test Setup l Figure 19 - Air Bleed System a APPENDICES l, l Appendix A - Test Matrix Appendix B - Specifications for Sensors
, Appendix C -
Specifications for Vishay System Appendix D - Specifications for Charge Amplifier Appendix E - Q.S.I. System Performance Characteristics E
- E Appendix F -
Specifications for RTD Signal Conditioner 4
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Revision 4 I. OBJECTIVES The objectives of the LaSalle County Unit 1 In-Plant SRV Test 1 are to provide test data that: (1) will be utilized to confirm that the containment can safely accommodate all hydrodynamic L loads and thermal effects associated with SRV actuation; and (2) will be utilized to demonstrate adequate plant design margins for these SRV loads. In addition to the In-Plant SRV Test results, it is intended that all appropriate information available from the generic Mark II Program, from the Karlstein Test Group (KTG), and from the Kraftwerk Union AG (KWU) information package also be used to support the LaSalle County plant licensing activities and schedule. It is intended that the In-Plant SRV Test results will be , used to address licensing issues relative to SRV actuation. The current issues are: A. Submerged structural loads resulting from SRV actuation. B. Containment boundary loads resulting from SRV actuation. C. Thermal mixing of the suppression pool water during an .I' extended SRV blowdown. D. SRV response spectra for mechanical components in reactor building.
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I Revision 4 These issues will be addressed for both first and subsequent SRV actuation conditions. I It is anticipated that the licensing issues identified above will be resolved by: (1) confirming that the actual measured L SRV induced mechanical / structural response of selected components in the reactor building can be accommodated; (2) confirming that the actual measured SRV hydrodynamic loads and thermal effects in the suppression pool can be accommodated; and (3) confirming that the SRV design basis loads provide an adequate safety margin by analytically extending the actual in-plant test results to the most severe design basis conditions. In order to accomplish the latter objective, the in-plant test data will be utilized to predict the most severe design basis SRV response postulated during plant operation. This experimental / analytical approach provides a method to compare the most severe actual SRV responses with the design basis responses and will demonstrate that plant safety margin. I 'I I I l SARGENT&LUNDY iENGINEE AS . 7 - _ _ I '-2
i I Uevision 4 I II. SCHEDULE Figure II-l is the schedule developed to address those activities associated with testing activities. These activities are concerned primarily with the SRV test prepara-tions and preliminary analysis and the subsequent acquisition of data from SRV actuations as described in Paragraph III.C, Test Matrix. I The schedule uses the LaSalle County - Unit 1 fuel load date as the primary reference date for activities associated with the In-Plant SRV Test. . 3 l The scheduled items on Figure II-l ' Jill encompass the following: j A. Pre-Test Activities - This will include the procurement of instrumentation, design, and installation of sensor mounting brackets, design of downcomer penetration and installation, issuance of revised test plan, final engineering evaluation and guidelines for testing parameters. B. Equipment Installation - This will involve the actual
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installation of sensors and data acquisition station. C. Test Procedure - This activity will include the preparation, review, and approval of a step-by-step method for performance in the In-Plant SRV Test. SARGENT&LUNDY lENGINEERS 7 - II-l
l Revision 4 D. Conduct of Test - The implementation of the test i procedure at LaSalle County Station. l I I $4 I I I I I I I I l SARGENT&LUNDY
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I Revision 4 III. SCOPE A. Test Conditions
- 1. During the performance of this test, the reactor temperature and pressure will be maintained within allowable operational and test limits. The prescribed reactor tolerances will be within 2% of the nominal operating values, with the reactor at or less than 60% power. These test tolerances have been established for statistical considerations and have been applied to all applicable initial plant conditions. To assure repeatability of data, the following initial conditions, in addition to those previously discussed, will be within allowable test tolerances prior to an SRV/ ADS valve actuation:
suppression pool water level, suppression pool water temperature, and discharge pipe temperature.
- 2. An air bleed system is included in each of the five SRV discharge lines in the test program. The bleed system consists of a double solenoid valve tapped into each line in the drywell. These valves
- are individually operated fron; remote controls.
Position indication lights give an indication of the solencid valves being energized open or deenergized closed. On loss of control power the i valves fail closed. SARGENT&LUNDY
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I Revision 4 I The purpose of the air bleed system is to return the suppressed discharge line water level to a level approximately that of the suppression pool. T', 2 air bleed system is used prior to each cold pipe discharge to provide a statistically constant parameter for data analysis. The air bleed system is not used prior to hot pipe or second pop SRV lifts. (See Figure 19. ) B. Quencher Selection Criteria I 1. Quenchers located at azimuths 210 , 230 , 252 , 264 , and 170 will be selected for testing. The selection is based on the following criteria (see Figure 16) :
- a. Maximum Structural Response - It is anticipated that the structural response of containment structures due to SRV discharges will be small.
Therefore, the location selected for monitoring accelerations should be on the containment wall rather that en the buttresses. There are three buttresses, located at azimuths 60', 180 , and 300*. Thus, the suppression pool is divided into three potential sectors, separated by these buttresses. SARGENT&LUNDY l
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Revision 4-I b. Representati're Structures - The sector selecte( for testing must represent a typical structural element with a minimum amount of discontinuities such as large penetrations, concentrated messes, etc. This would provide a favorable condition for comparing test data and analyti-cally-derived " expected values."
- c. Proper Mixes of SRV Line Volumes - The ideal combination of line seleccion is to include those lines with the largest and smallest volumes, and other lines with intermediate volumes. This would allow the evaluat. ion of effects of line volumes on pool pressure variations. If the above condition could not be met, the alternative is to include tne largest line volume in the test sector and to select the best available line combination, based on the existing SRV line arrangement.
- d. Close Proximity to Electrical Penetrations -
To minimize noise levels in the signal conductors, the shortest distance from the sensors to the available electrical penetration is preferred. 1 ; SARGENT&LUNDY
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Revision 4
- e. Submerged Structural Loads and Thermal Mixing -
The orientation of the tested quenchers should facilitate determination of multiple discharge load combinations, pool thermal mixing, and submerged stctcture loading characteristics.
- f. The SRV discharge line volume ranges from 3 3 80.05 ft (smallest) to 122.2 ft (largest) .
The arithmetic average of all line volumes is 3 100.2 ft , The five SRV discharge lines selected for this test have the volumes 91.2 ft , 103.5 ft , 3 107.0 ft , 114.5 ft , and 122.2 ft . Thus, the largest volume line is one of the test lines. The smallest volume test line deviates fror the smallest volume line in the plant by only 12.68%. C. Test Matrix The test matrix is based on actuations of SRV valves with quenchers located adjacent to each other (Az. 210 , 230 , 252 , and 264 ). In addition to these four valves, the SRV quencher at Az. 170 shall be tested in a single-valve-actuation mode. (Refer to Figure 16 and Appen-dix A.) Combinations of valve actuations shall be used I to cover a variety of loading conditions and consequent SARGENT&LUNDY i ENGINEEFIS _ 7 - - III-4
Revision 4 structural responses that will provide test data to confirm the methods used for summing dynamic SRV loads. A classification of the type of tests to be conducted is as follows:
- 1. One SRV Actuatior Test (SRV-1) l This test will be conducted by actuating a single SRV for a nominal 15 second duration of discharge time. This test is designated as SRV-1 in the The test will include both the cold I Test Matrix.
and hot initial pipe temperature in order to investigate first and subsequent SR" actuation conditions. The cold pipe actuation data is used to form the statistical basis for all other SRV Test actuations. I
- 2. Consecutive SRV Actuation Test (SRV-C)
This test will be conducted by actuating a single SRV consecutively for a given duration of discharge time for each actuation. This test is designated as SRV-C in the Test Matrix. The time interval between two consecutive actuations will be varied to determine the effects of the reficod transient on the maximum SRV loads resulting from subsequent actuation.
! SARGENT&LUNDY iENGINEERS _ ;
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- I Revision 4 This procedure will cover the range of time intervals during which peak reflood height would occur in the line. A review of the KTG test data was also made to determine the range of time intervals to be considered in this test. The test will be repeated at least five times at the maximum loading condition measured in this test.
- 3. Two SRV Actuation Test (SRV-2)
This test will be conducted by actuating two
- adjacent SRV's for a given duration discharge time. This test is designated as SRV-2 in the Test Matrix. The test will include both the cold and hot initial pipe conditions.
TB 7alves will be actuated manually and their lift times will be recorded automatically on the sequential recording annunciator typewriter in the Reactor Control Room. The Sargent & Lundy (S&L) analytical model will be used to evaluate the effects of differences in line length and volume, which in turn affect the
.I bubble entry times into the pool.
Since the time of valve actuation and the geometric characteristics of the line will be available from .I
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Revision 4 the test data, the analytical model can be used to , I determine the vent clearing time, and hence the bubble entry times into the pool. This information l l 1 can then be utilized to deterrine the appropriate pressure-time histories in the pool. An evaluatien would then be made with the measured pressures traces to demonstrate that the analytical model prediction bounds the measured test results. The same S&L analytical model will be used to conser-vatively predict the loading conditions at the LaSalle design conditions. This S&L analytical model predicts loading conditions at design conditions which are bounded by the LaSalle Design Basis.
- 4. Four SRV Actuation Test (SRV-4)
This test will be conducted by actuating four SRV's simultaneously for a given duration of discharge time. This test is designated as SRV-4 in the Test Matrix. The valves will be actuated manually and their lift times will be recorded automatically on the sequential recording annunciator typewriter in the I Reactor Control Room. I l SARGENT&LUNDY IENGINEERS _ e - _ _- - - -- III-7
l Revision 4 I 1 I The Sargent & Lundy (S&L) calytical model will be l I 1 used to evaluate the effects of differences in line length and volume, which in turn affect the bubble entry times into the pool. ' Since the time of valve actuation and the geometric characteristics of the line will be available from the test data, the analytical model can be used to determine the vent clearing time, and hence the bubble entry times into the pool. This information can then be utilized to determine the appropriate pressure-time histories in the pool. An evaluation would then be made with the measured pressures traces to demonstrate that the analytical model prediction bounds the measured test results. The same S&L analytical model will be used to conser-vatively predict the loading conditions at the LaSalle design conditions. This S&L analytical model predicts loading conditions at design conditions which are bounded by the LaSalle Design Basis.
- 5. Sequential SRV Actuation Test (SRV-S)
This test will be conducted by actuating four SRV's in sequence (rather than simultaneously as in the previous case) for a nominal 15 second duration of SARGENT&LUNDY iENGINE ERS , III-8
Revision 4 I discharge time and at a one second opening time interval. The sequencing for the sequential valve actuation case will be accomplished manually with time interval equal to the time period of the first cycle of the lowest set-point air bubble in the Resonant Sequential Symmetric Discharge load case. This test is designated as SRV-S in the Test Matrix. The purpose of this test is to provide data which can be used to verify the conservatism of the loads due to bubble phasing. Analyses of bubble phasing and its effects will be examined by using the S&L analytical models already available. Since the valve opening time and the associated geometric characteristics for each line are known, the analytical models can be used to predict the line clearing transient and determine the time at which individual bubbles arrive in the pool. The analytical model then can predict the wall pressure histories at any location in the suppression pool for the test condition. The same . I analytical model is also used to predict loads at the design conditions which are bounded by the LaSalle Design 3 asis. With this type of analyses, in conjunction with the measured data, an evaluation l SARGENT&LUNDY l ..~o,~...4- _ III-9
I Revision 4 il of the effects of phasing can be obtained for both test and design conditions.
- 6. Extended SRV Blowdown Test (SRV-E)
This test will be conducted to simulate the initial phases of the suppression pool temperature transient resulting from a postulated stuck-open safety relief valve (SORV) . This test is designated as SRV-E in the Test Matrix. The purpose of this test is to demonstrate: (1) adequate normal thermal mixing of the suppression pool water; and (2) adequate performance of the installed temperature monitoring system during an extended SRV blowdown due to SORV.
- 7. Leaky Valve Test (SRV-L)
This test will be conducted to simulate a leaky relief valve seat preceding an SRV actuation. The discharge pipe will be hot but unlike SRV-1
. Hot Pipe, will not necessarily be purged of air.
Leaky valve test will be simulated by introducing steam into the SRV discharge line before actuation of the valve. Provision has been made to introduce steam into the line over any desired time period. This test is designated as SRV-L in the Test Matrix. SARGENT&LUNDY
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Revision 4 Appendix A shows the Test Matrix for this program. The reactor will be maintained at normal operating temperature and pressure. The entire test will be performed with the reactor at or less than 60% power. It is anticipated that after a series of tests, the hot SRV/ ADS line will require about three or four hours to restore pipe temperature to within allowable test tolerances for a " Cold Pipe" test. ll The re fore , during the actual testing program, sequencing of the tests shall be optimized to reduce the total time required for completion of the entire test program. Tests which will be used to evaluate thermal effects, hydrodynamic loading and responsc shall be repeated at least five times to ensure that a statistically signi-ficant result is obtained, and to demonstrate repeat-ability of the results. The tests used to evaluate relative responses shall be performed a maximum of three times. The Test Matrix (Appendix A) details the types of various tests to be performed. D. Sensor Requirements i l SARGENT&LUNDY l
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Revision 4
- 1. General Four basic types of instruments were selected to measure the test data: Acceleromaters, Pressure Sensors, Temperature Sensors, and Strain Gaugen.
These instruments are further divided by monitoring ranges and environmental conditions as described below.
- 2. Accelerometers Thirty-eight (38) accelerometers will be used in the tests. The accelerometers are divided into three categories by environment: Containment Drywell, Containment Wetwell, and Outside Containment.
The Endevco 7717-200 will be used in the Containment Drywell; the Endevco 7717-M2A will be used in the
- Containment Wetwell; and the Endevco 7704-100 will be used at all locations outside of the contain-ment. Technical data on these accelerometers is provided in Appendix B.
il Accelerometer locations are listed in Table 1 and shown on Figures 1, lA, and 1B.
- 3. Pressure Sensors Fifty-two (52) pressure sensors will be used in the l SARGENT&LUNDY IENGINEERS 7 - --
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Revision 4 tests. The pressure sensors are divided into four groups based on pressure range to be monitored. The high pressure sensors are used to monitor SRV discharge line pressures at several locations. The medium and low pressure sensors are used in the suppression pool to measure the pressure transient caused by the SRV discharge. One low pressure sensor capable of withstanding a high overpressure will be used to monitor reflood transient pressure. Four ranges of the CEC 1000 were selected to fur-nish all but one of the required pressure signals. A Val 1 dyne AP-78 will be used to measure low pressure fluctuations in discharge piping after an SRV list. Pressure sensor locations are listed in Table 2 and ! shown on Figures 10, 11, 12, 12A, 13, and 13A.
- 4. Temperature Sensors Fo rty-ei ght (4 8 ) temperature sensors will be used in the tests. Two categories of RTD's are used due to the differences in mounting methods required.
I The Medtherm PTF-XXX-10356 will be used in all loca-tions listed in Table 3 and shown on Figures 14, 14A, 15, and 15A except for T42, T43, T46, and T47. These sensors are Medtherm PRT-XXX-10387 surface mounted RTD's. (XXX is the sheath length in feet.) SARGENT&LUNDY
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l Revision 4 l
- 5. Strain Gages l
i ! Fifty (50) uniaxial strain gages will be used in the l tests. Although all the strain gages are of the weldable type, three different categories of strain gages are used due to diffdrent temperature compen-sation requirements of the metal on which they are j mounted (Table 4 notes). The Ailtec MG-125/20-OlHG-150-6S uniaxial strain gage was selected to be installed in bridgc, bridge, il and rosette configurations. iE E Strain gage locations are listed in Table 4 and shown - Figures 3, 5, 6, 7, 8, and 9. !I E. Signal Conditioning System
- 1. General II A 208-channel signal conditioning system will be required for the SRV test program. Strain gages and pressure sensors will be conditioned with the Vishay 2100 signal conditioning / amplifier system.
. The temperature sensors will be conditioned with the AGM Electronic, Inc. Model EIA-4003 RTD Signal Conditioner. The Endevco accelerometers will be conditioned by the charge amplifier, Endevco 2721AM4 or by Endevco 4479.lM3/2652Mll. j l SARGENT&LUNDY , iENGINEERS p - - _ - III-14
1 t 1 1 l Revision 4 l
- 2. Vishay System The Vishay 2100 will be used to condition strain gages and pressure sensors. (See Appendix C for system specifications.) This system features inde-pendently variable excitation for each channel (1-12V DC) and will accept quarter , half , and full-bridge inputs as well as DC signals from other than bridge sources. Internal to each amplifier channel are 120-ohm and 350-ohm bridge completion components for quarter- and half-bridge gages, as well as internal shunt calibration resistors to simulate 11000 microstrain. Each channel has a bridge balance network that will offset a 13000 microstrain imbalance, and an always active LED null indicator and balance resistors to compensate for line resistance.
The 2100 system has a signal output from 0 to 10V DC up to 100 ma with a frequency response of 5 KHz. All signal and power outputs are current-limited for short circuit protection. After transducer hook-up, normal setup procedure for the Vishay 2100 system involves only offset balancing and output gain adjustment. This system will accommodate any common data collection or monitoring equipment. SARGENT&LUNDY ENGINE E AB _ p - - III-15
Reyision 4
- 3. Endevco 2721AM4 AC Charge Amplifier The Endevco 2721AM4 amplifier (See Appendix D) will '
l be used to condition Endevco accelerometer sensors. This amplifier is an all solid state, wideband instrument designed for use with piezo-electric transducers. The output voltage of the charge ampli-fier is proportional to the electric charge generated by the connected transducer. As a result, changes I in cable lenoth between transducer and amplifier will not affect system sensitivity, system low frequency response, or the temperature response of the transducer. A ten-turn potentiometer on the front panel allows insertion of specific transducer sensitivity. The five-orsition rotary switch provides five steps of calibrated gain resulting in system sensitivity (transducer plus amplifier).
- 4. Endevco 4479.lM3/2652M11 Charge Converter Signal Ccnditioner The Model 2652Mll is a charge-to-voltage converter designed for use with piezo-electric transducers.
The Model 4479.1M3 Plug-In Mode Card is a signal conditioner for use with the Model 4470 Signal l l l I SARGENT&LUNDY
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Revision 4 Conditioner module and provides power to, and conditions the signal fram the Model 2652Mll. (See Appendix D and Figure 17.) The charge converter, located near the transducer, i converts the electrical charge generated by the transducer to a low impedance voltage signal. The { output is essentially unaffected by the length of the cable on changes in cable capacitance between transducer and driver. i i A calibrated dial is provided to set in transducer f sensitivity. Full scale output +2.5 volts peak is I obtained for input measurements of 0.1, 0.3, 1.0,
; 3. and 30g,
!6 j 5. AGM Electronic, Inc., Model EIA-4003, RTD Signal Conditioner i The Medtherm EIA-4003 RTD Signal Conditioner provides a filtered, regulated, rectified power supply to individual RTDs. $ The EIA-4003 amplifies, linearizes, and isolates the output signal from the RTD and provides an I output signal to the Q.S.I. 721 or Oscillograph Recorders. ! For conditioner specifications, see Appendix E. SARGENT&LUNDY iENGINEERS _ 7 - - - __ III-17
Revision 4 F. Data Acquisition and Monitoring System
- 1. Data Acquisition System The digital data acquisition and recording system is the Q.S.I. Model 721. A block diagram of the Q.S.I. 721 along with the other Data Acquisition System and Playback (DARPS) equipment is shown in
- I Figure 17.
All signal inputs to the system are processed, formatted, and written in IBM compatible form on digital magnetic tape. The tapes so generated may then be processed on any computer system (supporting industry standard magnetic tapes) for data reduction, analysis, and reformatting to any desired standard. See Appendix E for System Performance Characteristics. Internally, the System consists of four main sub-systems: (1) an analog multiplexcr; (2) precision analog-to-digital converter; (3) high speed digital magnetic tape recorder; and '4) electronic control logic. Several factors contribute to the unusually high accuracy and throughput of this system. The analog-to-digital converter is a precision, 12-bit (11 bits plus sign) unit, with crystal referenced I sampling rate. The resulting low sample interval 1 jitter eliminates the wow and flutter problems of l analog recorders. The digital magnetic tape unit
- l SARGENT&LUNDY IENGINEERS _ p - __--- - __ --
III-18
t_ r Revision 4 is a high-speed (125 ips), very high density l (6250 BPI Group Code Recording [GCR]) device. This enables an extremely high data throughput for the system. The GCR technique provides for a very low f error rate by correcting many recording errors on-the-' fly. Finally, semiconductor memory is used to buffer l data flow through the system. This allows data acquisition and recording functions to proceed inde-pendently, for the highest possible system throughput (up to \ million samples /sec.). The system provides for on-the-spot playback of recorded data, with reconversion to analog form. It is also possible to speed up or slow down the playback over a 1000:1 range, with no loss of accu-racy. Time data retrieved from the tape are locked to the signal data and thus track and speed up or slow down.
- 2. Data Monitoring System
- a. General The analog monitoring system will consist of a number of conventional analog instruments (oscillographs, X-Y recorders, spectrum analyzers, FM magnetic tape, etc.). The monitoring system has four functions:
l SARGENT&LUNDY 1aumusman-7-- _ _ - _ _ _ _ _ - _ III-19 l
Revision 4 (1) real-time monitoring of signals; l l (2) display medium for after-the-run quick-look replay of digitally-recorded signals; (3) redun-i dant recording of any specially selected critical j signals; and (4) system operational check / calibration. i is jg One FM magnetic tape recorder will be provided j for analog recording of dynamic data from seven j selected accelerometer channels. In addition, up to 47 selected channels will be recorded l on escillograph recorders for real-time veri-j fication of data. J l This " quick-look" data will be provided as j follows: !I ] Sensor No. of Time Resp. Freq. j Type Sensors History Spec. Spec. 4g ju Accelerometer 7 X X X 1 Pressure Sensor 14 X X i j Temp. Sensor , 11 X Strain Gage 8 X X i
- b. FM Recorder j The FM magnetic tape recorder will be a Bell and Howell Model 4010. During recording of the test data, a trassport speed of 3-3/4 ips will be used so that a response of 0-1250 Hz will be l SARGENT&LUNDY l . . ~ . , ~ . . . . -
1 III-20
I i Revision 4 l obtained. This recorder will be calibrated for 1 full scale equal to +40% deviation of the center frequency. Data fror accelerometer channels will tTen be played back into a spectrum analyzer witP. an X-Y plotter in order to obtain response spec- f trum plots.
- c. Oscillograph Recorder l
Up to 47 selected channels of test data will be i presented in real-time through the use of light ' i ! beam oscillograph recorders. Honeywell Model 1508 recorders, with M-1000, M-1600, or M-400-350 galvanometers are used for this application. This equipment will provide for the recording of data over the frequency range of DC to 200 Hz and will allow test personnel to validate incoming data before proceeding onto the next test phase.
- d. Response Spectrum Analyzer An MRAD Model 282S or equivalent spectrum analyzer will be used to present the " quick-look" llE accelerometer data required. The data will be analyzed at one-sixth octave intervals over a i
frequency range of 1 Hz to 100 Hz. l l l l I i SARGENT&LUNDY ) , . ~ . , ~ . . . . --- - III-21 i h
lI , Revision 4 j G. Processing and Reduction of Recorded Data
- l. General I
The following processing and reduction tasks will be a ! performed on the recorded, digitized data, and will , be written in IBM EBCDIC format. The digitized data will ce converted to engineering 4 1 l units and recorded in IBM EBCDIC format with
, appropriate header information on 1600 BPI magnetich Microfiche records will be prepared of the digi-
! tized engineering unit data. i j All digital tapes used will be certified to be i j free from parity errors. i The data will be reduced and plotted and will be recorded on digital tape in IBM EDCDIC format, i I
- 2. Data Reduction l To perform the required data processing and reduction, we are presently considering the existing general 1
j purpose Wyle computer program ADARE (Advanced Data i i Analysis and Reduction Software). ADARS provides i j the framework for coordinating various data files t l on disc. ADARS has an operator interface which i I SARGENT&LUNDY j ..~.,~.... ------- - III-22
Revision 4 1, o
- allows the user to select a wide variety of
)g processing and display options to meet his analysis iE I requirements. ADARS will perform all the necessary steps to process the raw digitized data tape and produce the required plots of reduced data. The .ujor tasks involved in l l this process include: building a data base of pertinent channel information, demultiplexing the lI digitized data, conversion of the data to the proper engineering units and producing the analysis plots. > j 3. Basic Analysis Parameters , The data, which is to be acquired at 1000 samples ) 4 j per second, per channel, will be filtered at 200 Hz and then decimated to 500 samples per second. The f. list below summarizes the major parameters of the acquired data:
?
Acquisition rate of 1000 samples per second i per channel. i Frequency components of data up to 200 Hz. L j
- Typical test time will be a nominal 15 seconds for most tests.
i
- l Data recorded in multiplexed 16-bit integer A/D counts.
SARGENT&LUNDY ! i
- III-23 l 1
-- w=r -w
5 Revision 4 'I All data from each test run will be recorded on one magnetic tape. i
- 4. Computer System Description i
The ADARS computer program is operational on Wyle l Interdata 8/32 system. The Interdata 8/32 is a i 32-bit computer with 256 Kilobytes of 300 nanosecond
- main memory. The system includes a high performance single and double precision floating point processor to speed calculations.
The primary peripherals of the Interdata 8/32 l system include: l 16-channel, 12-bit analog-to-digital converter 1 i 8-channel, 12-bit digital-to-analog converter i 67 Megabyte disc memory t
- 300 Megabyte disc memory Two, 000/1600 BPI, 75 ips tape drives l *
! 400 cpm card reader I j
- l
- 600 1pm line printer Two interactive terminals
! Tektronix 4014 Graphic Terminal I l SARGENT&LUNDY
' ENGINE E A S -
7_- j 111-24 4
. Revision 4
] Versatec 1200A printer / plotter /hardcopy unit The interdata is supplied with a full complement of l j i software, including a real-time multiprogramming } ) operating system, time sharing, an optimizing FORTRAN l i compiler, and full disc file management facilities. j These capabilities provide full support for all the ADARS activities. 1
- 5. Data Processing and Reduction Approach i
The data processing and reduction that will be performed are described in a step-by-step manner. Descriptions of steps that are not directly related l to final requirements are included to show the logical j proccss of the steps performed. The processing i { steps are: I i 1 (1) Build a data base on disc containing the perti-I i nent channel information, including gage ] sensitivity, gage type, engineering units and plot labels. 1 i t (2) Demultiplex the data to tape and copy it to ' disc for processing. (3) Remove any unwanted transducer bias or drift - I j from the data. t
- SARGEIIT&LUNDY
..~m~....-- - - - - --
l III-25
i I Revision 4 i i i j (4) Convert the data to its proper engineering unit form. (5) Low pass digitally filter the data to remove j any unwanted noise. The cutoff point and rate are user selectable. i l (6) Decimate the data down from 1000 samples per I i second. l I (7) Copy the filtered and decimated data as 1 I described in (5) and (6) above to magnetic l tape in IBM EBCDIC format in 4000 character
)
records (fifty 80-character card images) in the tape format and file structure. 1 (8) Prepare min ofiche records of the data described i 1 in (7) above. 42 power 4" x 6" microfiche cards with 208 pages per sheet will be prepared j using computer output to microfiche (COM) techniques. 4 I (9) Plot the following time history data in l ! engineering units: l l Accelerometer data Pressure sensor data i - Temperature data
! SARGENT&LUNDY iENGINEE AS 7-III-26 i
i -_. _ _ _ _ _ _ _ _ _ . _ _ , . _ _ _ . _ _ , _ . _ _ _ _ _ _ _ _ . . .
I Revision 4 Uniaxial stress data (computed from strain gage data) ! (10) Plot the Fourier spectrum magnitude and phase for the following: Pressure Sensor Data Accelerometer Data Uniaxial Strain Gage Data (11) Plot the response spectra for the following: Accelerometer Data (12) Copy the reduced data Items (9), (10), and (11) above to magnetic tape in IBM EBCDIC I format. All digital magnetic tapes used on this project will be new and certified by the manufacturers to be free from parity errors. H. Test Documents The In-Plant SRV Test procedure provides a methodical I approach which will ensure repeatability of data, plant safety and optimize the time spent performing this test. l f The step-by-step format of the procedure addresses the critical plant conditions applicable to this test.
- SARGENT&LUNDY I 1ENGINEEf38. 7 - ---
III-27 l l
i l Revision 4 The precautions and induced conditions are within 1 allowable operating tolerances as specified in the ! 1 LaSalle Jounty Technical Specification. ( l As an added precaution, " Quick-Look" data will be
- evaluated at the cr7pletion of each uniquely different test section, to ensure response levels are within design limitations. This evaluation will be completed prior to proceeding with the next test section.
Implementation I I. 4 Implementation of the In-Plant SRV Test program requires
- a multi-organization, multi-discipline effort.
i Commonwealth Edison Company (CECO), as the licensee, provides overal.1 program direction. Ceco operations and technical / engineering staffs will provide input to test document preparation and assist in conduct of the test (test performance and data collection). Sargent & Lundy, as the plant designer, will provide program definition and requirements, testing requirements and acceptance criteria for the test. Sargent & Lundy will also prepare all necessary testing documents, provide
- test administration, specify sensor types and locetions, and conduct any associated analysis.
I Wyle Laboratories, as the contractor, will install test a SARGENT&LUNDY 1 ENGINEERS _ p - --- --- - -I III-28 l
-1
Revision 4 equipment and sensors. The field installation and test team will operate the data acquisition station. I I They are experienced with this type of testing and have perforated similar tests in the past. I I i O i I I I I I l l l SARGENT&LUNDY
- r ENGINEERS J 7_-
l I III-29
I _ I s P i l TAB L ES l e i I I I I I I .I I l ! SARGENT&LUNDY I l
1 Revision 4 { TABLES j General Notes to Tables 1-4 l, { Tables 1 through 4 refer to six environmental conditions that are defined as follows: 4 1 Environment El Wetwell 1 i Fluid Water Pressure 100 psia ) Temperature 50 F-150 F j Relative Humidity NA j Radiation 4 50R/hr.Y i Environment E2 Drywell 15 Fluid Air }g Pressure 15.4 psig i Temperature 135 F Relative Humidity 90% ] Radiation 50R/Hr. y ; 1.4 x 105 n/cm 2 sec. t' Environment E3 SRV Discharge Line
- Fluid Air / Water / Steam ig Pressure 650 psia
- E Temperature 500 F Relative Humidity NA Radiation
- 50 R/Hr . Y It Environment 24 I
j Fluid Sensor will be in the SRV dis-Pressure charge line (E3) and the "out-m ,I emperature Relative Humidity side" of the sensor and its cabling will be exposed to Radiation conditions in wetwell (El).
- Note Discharge Line in the drywell experiences 50 R/Hr. y ; 1.4 x 105 n/cm2 see.
SARGENT&LUNDY
..~.,~..... r -- -
1 of 2 l l
Revision 4 l Environment E5 Fluid Pressure Sensor will be in the SRV discharge line (E3) and the Tempera <..re Relative Ilumidity "outside" of the sensor and the cabling will be exposed to condi-Radiation tions in the drywell (E2). Environment E6 Fluid Air Pressure 15.4 p3ig Temperature 120 F L Relative ilumidity 60% Radiation l Negligible { i I I L c ll SARGENT&LUNDY 1ENGINEE AG p r _ - _ -_ 2 of 2
LA SALLC COUNTY - 1 4 C0tH0 WEALTH E0150N COMPANY l TABLE 1 PAF.E _I_ O d PROJECT NO. 5835-00 i i' I ACCELEROMETER DATA REV 4 SE N 57. LOCATION z j SEN50F DPECTED *O
; N'JMBE 5 RESPON5E EXPECTED ACCURACY ENVIRON . g NOTE 5 FREQUENCY wtNT v i
I AZIMUTH (CEG) ELEV. (FT-IN) RA)fUS (PT-IN) (G) DA%E (H2) (t % F.S.) g y A1 46 804'-0 22'-7 0.005-1.0 1-50 1 E2 R 1 l A2 46 804*-0 22'-7 0,005-1.0 1-50 i 1 E2 ? 1 A3 106 804'-0 22'-7 0.005-1.0 1-50 1 E2 R 1 A4 100 804'-0 22'-7 0.005-1.0 1-50 I E2 T I 1 A5 226 304'-0 22'-7 0.005-1.0 1-50 1 E2 R 1 A6 226 804*-0 22'-7 0.005-1.0 1-50 E2 1 T 1 A7 46 755'-3 14'-11% 0.005-1.0 1-50 1 E2 R 1 I AB A9 46 106 755'-3 755'-3 14'-11$ 14'-11b 0.005-1.0 0.005-1.0 1-50 1-50 1 1 E2 E2 V R A10 106 755'-3 14'-11 0.005-1.0 1-50 1 E2 V ' l _ All 226 755'-3 14'-11% 0.005-1.0 1-51 1 E2 k M A12 226 755'-3 14'-114 0.005-1.0 1-50 i E2 V l 4 I A13 l 46 736'-7 14'-115 0.005-1.0 1-50 1 E2 R 2 A14 46 736'-7 14'-11\ 0.005-1.0 1-50 1 E2 V 2 i A l ', 10e 736*-7 14'-115 0.005-1.0 1-50 1 E2 k 2 i A16 106 736'-7 14'-11$ 0.005-1.0 1-50 1 E2 V 2 A17 226 736'-7 14'-11 0.005-1.0 1-50 1 E7 R 2 i A18 226 736'-7 14'-115 0.005-1.0 1-50 1 .2 V 2 A19 226 764'-6 41'-0 0.005-1.0 1-50 1 E6 R 6 o A20 'I A21 226 236 764'-6 740'-0 41'-0 43'-0 0.005-1.C 1-50 1 E6 V 6 0.005-1.0 1-50 1 E6 R 3.6 A22 236 740'-0 48'-0 0.005-1.0 1-50 1 E6 V 3,6 l A23 226 649'-10 47'-4 0.005-1.0 1-50 1 E6 I R 6 A24 226 699'-10 47'-4 0.005-1.0 1-50 1 E6 V 6 I A25 226 673'-4 47'-4 0.005-1.0 1-50 1 E6 R 4,6 A26 226 673'-4 47'-4 0.005-1.0 1-50 i
*1 E6 V 4,6 '
I i i } LA SALLE COUNTY - 1 COPNONWAtlH EDISON COMPANY TA M 1 "^r,t .2_ cr 4 i PROJECT N0. 5835 00 ACCELEROMETER DATA yg , i. l SENSCR LOCATION ' z SENSOP o NUMBES EXPECTED DrECTED ACCURACY ENV[p0N. ;- NOTES RESPONSE TPEQUE' ICY ufNT u RA%E E AZI%TH ELEY. E/DIUS (G) (H2) (t % g i (CEG) (FT-IN) (FT-IN) F S.) See A27 Notes 740'-0 104'-0 0.005-1.0 1-50 E6 1 V 3,5,6 3 __ I See A28 Notes 673'-4 1n4'-0 0.005-1.0 1-50 E6 1 V 3,5,6 A29 226 673'-4 14*-11% 0.005-1.0 1-50 1
; - El R 4 l
A30 226 673'-4 14'-115 0.005-1 0 1-50 1 1:1 V 4 A31 230 699'-10 29' 9 0.1-30 p 1-100 1 el 1..._. A32 230 693'-10 29'-9 0.1-30 1-100 1 El T e. j A33 230 736'-7$ 29'-9 0.005-1.0 1-100 1 U2 P
}
A34 230 688'-4 24'-9 0.1-30 1-]OO 1 1 El R I I A35 230 j 688'-4 29'-9 0.1-30 1-100 1 El T A36 226 804'-0 22'-5 0.005-1.0 1-100 1 E2 V
~
^ A37 1/4 6 8 b '-l ti 32'-9 0.10 ';u 1-1'O c1 a
!I 1 A38 174 688*-10 32'-9 0.10-50 J 1-100 1 El T 3 __ w- e-ww 4 1 - il I JI i _ j 4 1 - 1 i 3 4 1 4
g Revision 4
.E TABLE 1 ACCELEROMETER DATA l NOTES (1) Sensors are to be located on the Gusset Plate connecting the legs of the Stabilizer Truss.
(2) Sensors are to be located on the Drywell Floor near the Reactor Support. (3) Sensors are to be located on the slab. (4) Sensors are to be located on the Basemat. (5) Sensors are to be located near the Intersection of Column Rows 8.9 and A. (6) Sensor has no Conductors passing through the Containment. GENERAL NOTES E Location Sensor No. Function
,g Stabilizer Truss Al through A6 To record the horizontal responses at the interface point with G.E.
j Reactor Support A7 through A12 These sensors are coordinated,
; with sensors Al through A6 to record both the horizontal and vertical responses at the top of the reactor support.
Drywell Floor / A13 through A18 These sensors are coordinated , Pedestal Inter- with sensors Al through A6 to face record both the horizontal and vertical responses at the , top of the reactor support. Containment Wall A19 through A26 To record the containment I responses at important loca-tions. They are also required? to determine the vertical attenuation through the containment. SARGEN1NhLUNDY
' ENGINE E A B _ ,
3 vf 4
W Revision 4 l ~ TABLE 1 ACCFLEROMETER DATA
-~
GENERAL NOTES ~ Location Sensor No. Function I Corner of Reactor A27 and A28 To determine the attenuation of the horizontal responses Building across the reactor building slabs when compared to sensors A21 and A25, respectively. Bottom of Reactor A29 and A30 To record the reactor support Support horizottal and vertical responses at the basemat. When A23 and A30 are com-pared with sensors All, Al2, A17 and A18, the amplifica-tion of the responses can be determined. Column (Az. 230 , A31 through A35 To record the horizontal and Radius 29'-9") vertical acceleratien res-ponses of the suppression pool column. These sensors are needed to correlate the acceleration response with the pressure measured by I sensors P18 through P21 and P27 through P30. Top of Support A36 To record the vertical res-Column ponses at the top of the l sacrificial shield. This sensor is provided to show , the vertical amplification ' of the acceleration response in the sacrificial shield when compared to sensor AB. ] , l lg Downcomer A37 and A38 To record the horizontal l acceleration responses of the ( g (Az. 174 , instrumented downcomer. These I Radius 32'-9") sensors are needed to corre- I late the acceleration response : with the pressure measured by sensors P37 through P44. SARGENT&LUNDY innamaans _ 7-4 of 4
I LA 5ALLE COUNTY - 1 C0m0wtAttu Eo!50n ComrAN' FAAE _L F .5,, ( PROJECT h0. 5835-00 T/R E 2 PRESSURE SENSOR DATA ,g 4 i SEN%q LOCATION SEN50s EXPECTED EXPECTED ACCURACY ENVIRON. NCIES N'JMSEE RESPONSE FRE']UENCY MENT R AY,E A71%TH ELEV. RADIUS (PSIA) (NZ) (i % (CEG) (FT-IN) (pr-IN) I'S') P1 260.90 673'-5 36*-115 3-46 0-100 0.5 El P2 246.40 673'-8 36'-10% 3-46 0-100 0.5 El P3 233.14 673'-5 36'-6 3-46 0-100 0.5 El P4 220 673'-3 37'-1\ 3-46 0-100 0.5 F1 P5 200 673'-8 35'-7 3-46 0-100 0.5 El P6 173.14 673'-S 36'-Sh 3-46 0-100 0.5 El P7 166.86 673'-5 36'-55 3-46 0-100 0.5 El P9 258.90 673'-S 20'-8 1/2 3-46 0-100 0.5 E1 P9 246.41 673'-5 21'-0 3-46 0-100 0.5 El P10 214.57 673'-5 20'-75 3-46 0-100 0.5 El 1 _ P11 201.21 673'-5 20*-10 3-46 0-100 0.5 El P12 264 681*-2 43'-4 3-46 0-100 0.5 El P13 246.46 676'-10 43'-4 3-46 0-100 0.5 El P14 229 f 511 ' - 2 43'-4 3-46 0-100 0.5 El P15 161.67 676'-10 43'-4 3-46 0-100 0.5 El P16 250 676'-10 14'-11 3-46 0-100 0.5 El Pl? 210 676-10 14'-115 3-46 0-100 0.5 El 4
. P18 230 676'-10 29' '. 3-46 0-100 0.5 El I P19 226.42 676'-10 28'-0 3-46 0-100 0.5 El P20 230 676'-10 26'-3 3-46 0-100 0.5 El 1
- P21 233.58 676'-10 28'-0 3-46 0-100 0.5 El l P22 268.67 684'-3 43'-4 3-46 0-100 0.5 El j i
3 P23 258.90 685'-5' 4 43'-4 3-46 0-100 0.5 El P24 234.67 694'-3 43'-4 3-46 0-100 0.5 E1 P25 250 691'-0 14'-11h 3-46 0-100 0.5 El 4 P26 210 688'-1 14'-115 3-46 0-100 0.5 E1
i ) LA SALLE COUNTY - 1
}W COPNONWEALTH E0!$0N COMPAN)
PROJECT NO. 5835-00 TM 2 "* I ' #' PRESSURE SENSOR DATA
' gy 4 i
I 1 1
$EN500 LOCATION SEN50s i EXPECTED EXPECTED ACCURACY
. NUMB E s
RESPONSE
twlRON. NOTES l FREQUE'iC Y MENT ! R W.E AZIMUTH ELEV. RADIUS (PSIA) (HII (1 % (DEG) (FT.!N) (py-IN) i I'S* ) 1 I P27 230 688'-4 l 29'-9 3-46 0-100 0.5 __E l_ , i 3 P28 226.42 688*-4 ! 28'-0 3-46 0-100 0.5 El ' 4 ! I P29 P33 230 233.58 688'-4 688*-4 26'-3 28'-0 3-46 0-100 0.5 El i 3-46 0-100 0.5 El i - - P31 ~ 14-650 0-200 0.5 ES 1
~ ~
P32 ~ 14-650 I P13
~ ~ ~
14-650 0-200 0-200
') . 5 0.5 E5 E4 2 1
~ ~
P34 ~ 14-650 0-200 0.5 E4 2 f P35 170 700*-10 36'-6 13-660 0-200 0.5 E4 P36 170 700'-10 ,36'-6 13-660 0-200 0.5 E4 P37 174 674'-10 32'-9 3-46 0-200 0.5 El . P38 174 (94'-10 32'-9 3 46 0-200 0.5 El P39 174 694'-10 32'-9 3-46 0-200 0.5 El P40 174 694'-10 32'-9 3-46 0-200 0.5 El I P41 042 174 174 689'-10 689'-10 32'-9 32*-9 3-46 3-46 0-200 0.5 El 0-200 0.5 El P43 174 689'-10 32'-9 3-46 0-200 0.5 El P44 174 689'-10 32'-9 3-46 I P45 14-650 0-200 0-200 0.5 0.5 El E5 1
~ i P46 '
14-650 0-200 0.5 E5 1 1
~
~
P47 ~ 14-650 0-200 0.5 E4 2
- ~ ~
P48 14-650 0-200 0.5 E4 2 P49 228.66 682*-7 43'-4 3-46 0-200 0.5 El P50 228.33 699'-6\ 43'-4 3-46 0-200 0. 5 El P51 350 673*-5 33'-10 I 3-20 0-200 0.5 El PS2 170 - 36*-6 3-15 0-200 0.5 ES 3
, - ~
Revision 4 TABLE 2 i 1 PRESSURE SENSOR DATA NOTES I (1) Sensors P31, P45, and P32, P46 are located downstream of Safety / Relief Valve and inside Pipes 1MS04BR-12 and 1MS04BM-12, respectively (see Figure 13). (2) Sensors P33, P47, and P34, P48 are mounted in the center I of the Quencher Device for Pipes IMSO4BR-12 and IMS04BM-12, respectively (see Figure 13) (3) Sensor P52 shall have, as a minimum, a sensitivity of I +1 in, of H2 O at 90 F and be capable of withstanding the conditions of Environment E5. GENERAL NOTES O, Location Sensor No. Function Basemat Pl through Pll Measurement of pressure-time history on the basemat surfacej I for the determination of load on basemat. P1 and P6 are also used to obtain circum-ferential pressure attenuationj I along with P51. Outer Pool P12, P13, P14, Measurement of pressure-time l I Boundary Wall P15, P22, P23, P24 history on the outer wall surface for the determination of pool boundary loads. P14 I and P24 are also used to obtain vertical pressure attenuation along with P49 and P50. I Inner Pool PlC, Pl7, P25 Measurement of pressure-time L Boundary Wall P26 history on the inner wall sur-I face for the determination of pool boundary loads. l i SARGENT&LUNDY I . ~.,~... 4 - - _-_ 3 of 5
I Revision 4 TABLE 2 PRESSURE SENSOR DATA GENERAL NOTES Location Sensor No. Function Column P18, P19, P20, Measurement of pressure-time (Az. 230 , P21, P27, P28, history on the column for the Radius 29'-9") P29, P30 determination of submerged I structures load. These sen-sors will be worked in con-junction with sensors A31, A32 and A33 to correlate between the pressure measured and the acceleration response on the column. T-Quencher P33 and P47 Measurement of pressure-time (lMS04BR-12) history inside the T-quencher 4 sphere for the determination l i of quencher load and the l condition of steam during the blowdown transient. T-Quencher P34 and P48 Measurement of pressure-time ig (lMSO4BM-12) history inside the T-quencher E sphere for the determination of quencher load and the l condition of steam during the I blowdown transient. ( Downcomer P37, P38, P39, Measurement of pressure-time
- (Az. 174 , P40, P41, P42, history in the downcomer sur-
! Radius 32'-9") P43, P44 face for the determination of : submerged structures load. i These sensors will be worked in with sensors A34, A35, A37 and A38 and sensors S31 through S34 to correlate between the pressure measured and the acceleration response i on the downcomer. SRV Discharge P31 and P45 Measurement of pressure-time Line (IMSO4BR-12) history inside the SRV dis-charge line for the deter-mination of back-pressure , downstream of the safety l relief valve. SARGEN11hLUNDY IENGINEERS 7_- 4 of 5
l Revision 4 TABLE 2 PRESSURE SENSOR DATA ) GENERAL NOTES socation Sensor No. Function l SRV Discharge P32 and P46 Measurement of pressure-time Line (lMSO4BM-12) history inside the SRV dis-charge line for the determina-I tion of back-pressure down-stream of the safety relief valve. I SRV Discharge Line (IMS04BM-12) P35 and P36 Measurement of pressure-time history inside the SRV dis-charge line above the norma I water level for comparison with analytic model predic-tions and for accurate calculation of discharge linef rigid restraint loads. Suppression Pool P49 through P51 Measure pressure attenuation within the suppression pool. Si1V Discharge PS2 Measurement of low pressure Line (lMS04BM-12) transient of the discharge line. I I I I SARGENT&LUNDY IENGINEE AS _ , 5 of 5
i I LA SAttE County - 1 l ComowtAtis E0150n CoMPAw '* 'E 1 d TABLE 3 l PROJECT NJ. 5835 00 jB TEPPERATURE SENSOR DATA g, 4 } 1 i j SEN500 LOCATION
$EN505 EXPECTED EXPECTED A;CLE ACY E N v p>0h . NniE5 l
i NUMEEE RESPONSE FREQUENCY whT
- RA %E
{ AZ I'fJT H ELEV. RA0!t5 (*[) (kZ) g , ,,) j (DEG) (FT-IN) (FT-lN) a l { T1 266.83 673'-5 37'-0 50-200 J-100 0.5 El - - . I f T2 '~6.66 673'-5 36'-7 50-200 0-100 0.5 El i T3 246.45 673'-8 22'-25 50-200 0-100 0.5 E1 i T4 205.58 673'-5 21'-75 50-200 0-100 0.5 El ~ T5 263.33 631'-2 43'-4 50-200 0-100 0.5 El i T6 241.67 677'-4 43'-4 50-200 0-100 0.5 El T7 228.67 c31'-2 43'-4 50-200 0-100 0.5 El TB 201.67 676'-10 43'-4 50-200 0-100 0.5 El 4 ! T9 161.67 677'-4 43'-4 50-200 0-100 0.5 El T10 250 6 7 7 ' -4 .14 '-11$ 50-200 0-100 0.5 El 4 Til 210 677'-4 I 14 '-11% 50-200 u-200 0.5 E1 T12 81.67 676'-10 43'-4 50-200 0-100 0.5 El jl . - _ __ i
! T13 0 681'-2 43'-4 50-200 0-100 0.5 El j -__
i J T14 90 676'-10 14'-115 50-200 0-100 0.5 E1 ! T15 0 676'-10 14'-11h 50-200 0-100 0.5 E1 } ] T16 266.42 676*-10 28'-0 SC-200 0-100 0.5 El l 717 246.42 687'-4 28'-0 50-200 0-100 0.5 El i T18 226.42 676'-10 28'-0 50-200 0-100 0.5 El I' i T19 206.42 6S7'-4 28'-0 50-200 0-100 0.5 El i T20 186.42 687'-4 28*-0 50-200 0-100 0.5 El T21 270 684'-9 43'-4 50-200 0-100 0.5 El i 3 T22 260.33 685'11'g 43'-4 50-200 0-100 0.5 El i l T23 234.67 684'-9 43'-4 50-200 0-100 0.5 El
- I j T24 199.C 684'-3 43'-4 50-200 0-100 0.5 El i
T25 16i.33 685'5 3/4 43'-4 50-200 0-100 0.5 E) i j T26 250 690'-6 14-11 50-200 0-100 0.5 El e J
e c lI LA SALLE COUNTV - 1 C0mC% EALTH E0!$0tl COMPANY TABLE 3 par,E 1. cr_4 lg PROJECT NO. 5835-00 !g TEMPERATijRE SENSOR DATA
,EV 4 j
l i 4 SENSCR LOCATION sggsc; EXPECTED EXTECTED ACCURACY E N / I R0t! . SOTES RESPONSE FRE%ENCY wtNT 7.Npag R WiE AZIMUTH ELEV. RADIUS (*F) N) (t *r> (CEG) (FT-lN) (FT-IN) T27 210 687'-15 14 -11 50-200 0-100 0.5 El , T28 90 684'-0 14'-115 50-200 0-100 0.5 El i 4 I T29 0 684'-0 14'-115 50-200 0-100 0.5 El l _- j T30 0 635'-6 43'-4 50-200 0-100 0.5 El 4 } T31 87.66 685'-5 /4 43'-4 50-200 0-100 0.5 El l T32 252 21 50-200 0-100 0.5 El i . _ _ . k j T33 230 37 50-200 0-100 0.5 E.1 l I T34 - - - 60-500 0-200 0.5 E5 1 1 1 1
. T35 - -
60-500 0-200 0.5 E5 1 T36 - - - 60-500 0-200 0.5 E4 2 ( - 1 4 j T37 - - -- 60-500 0-200 '1. 5 E4 / f - - . T38 - - 60-500 0-200 0.5 E5 1 T39 - - - 60-500 0-200 0.5 E5 1 1 j T40 - - - 60-500 0-200 0.5 E4 2 T41 - - - 60-500 0-200 0.5 E4 2 j T42 _ _ _ 60-500 0-200 0.5 E2 3 i T43 60-500 0-20t, 0.5 E2 3 f - - - i T44 726'-6 60-500 0-200 0.5 E4 4 T45 728'-3 60-500 0-200 0.5 E4 _ _ 4 T46 -- 726'-6 60-500 0-200 0.5 El 5 T47 - 728'-3 60-500 0-200 0.5 El 5 l I T49 228.33 699'-0 43'-4 50-200 0-100 0.5 El
Ravicion 4 TABLE 3 TEMPERATURE SENSUR DATA NOTES (1) Sensors T34, T38, and T35, T39 are located downstream on Safety / Relief Valve and inside Pipes 1MSO4BR-12 and 1MS04BM-12, respectively and measure fluid temperature (see Figure 15) . (2) Sensors T36, T40, and T37, T41 are mounted in the center of the Quencher Device for Pipes 1MS04BR-12 and 1MS04BM-12, respectively and measure fluid temperature (see Figure 15) . GENERAL NOTES
- . I Location Sensor No. Function Suppression Pool Tl through T33 Measurement of temperature-and T48 time history at various loca-
- ] tions in the suppression pool
-E to determine the degree of thermal mixing during an SRV , ~g blowdown. T2, T6, T7 and T23 l E are used in conjunction with l permanent sensor ITE-CM057G to measure therm stratifica-tion in the suppression pool.
SRV Discharge T35 and T39 Measurement of fluid tempera , Line (lMSO4BM-12) ture-time history inside the SRV discharge line downstream of the safety relief valve. SRV Discharge T35 and T39 Measurement of fluid tempera-Line (lMSO4BM-12) ture-time history inside the SRV discharge line downstream , I of the safety relief valve. T-Quencher T36 and T40 Measurement of fluid tempera-4 I (lMS04BR-12) ture-time history inside the T-Quencher sphere for deter-mination of quencher load and l I the condition of steam during the blowdown transient. ! SARGENT&LHDY
-~.....v 3 of 4
I Revision 4 I I TABLE 3
)
TEMPERATURE SENSOR DATA GENERAL NOTES Location Sensor No. Function T-Quencher T37 and T41 Measurement of temperature-(1MS04BM-12) time history inside the i T-quencher sphere for the I determination of quencher . i load and the condition of steam during the blowdown I SRV Discharge T42, T46 transient. Measure pipe external sur- l 1 Line (lMSO4BR-12) face temperature. T44 Measure pipe internal surface temperature. SRV Discharge T43, T47 Measure pipe external sur-Line (lMSO4BM-12) face temperature. T45 Measure pipe internal surface i temperature. I i 1 l l !I 2 SARGENT&LUNDY IENGINEERS _ 7 -_ _ 4 of 4
LA SALLE COUNTY - 1 j C0m0NWEALTH EDISON C0&ANY TM 4 PAGE 3 OF 3_ PROJECT NO. 5835-00 .I ? STPAIN GAUGE DATA
,ty 4 d
SEN50f' LOCATION l SENSOF EXPECTED EXPECTED ACC' J RACY ENVIRON 'GTf 5 NUMBES RESPONSE FREQUENCY MENT RANGE -I j AZIMUTH (DEG) El.E Y. (FT-IN) RADIUS (FT-IN) (IN/IN) (HZ) (% F.S.) 4 I S1 170 692' 9/10 36'-6 .0001 .002 0-100 3 El 1,7,8 S2 170 692' 9/16 36'-6 .0001 .002 0-100 3 :.1 1,7,8 S3 170 692' 9/16 36'-6 .0001 .002 0-100 3 El 1,7,8 ' S4 170 692' 9/16 36'-6 .0001 .002 0-100 3 El 1,7,8 55 170 716'-10 36'-6 .0001 .002 0-100 3 El 1,7,8 1 f 56 170 716'-10 36'-6 .0001 .002 0-100 3 t.1 1,7,8 l 57 170 716'-10 36'-6 .0001 .002 0-100 3 El 1,7,8
]
l 58 170 716'-10 36'-6 .0001 .002 0-100 3 El 1,8 1 53 170 676'-9/4 36'-6 .0001 .002 0-100 3 El 1,9 1 1 ! S10 170 676'-9/4 36'-6 .0001 .002 0-100 3 El 1,9
- S;' 170 676 ' 9h4 36'-5 .0001 .002 0-130 1,9 3 El 3 ._
.i l 1 S12 170 676'-9/4 36'-6 .0001 .002 0-100 3 El 1,9 l 1 j S13 170 6 7 6 '-Y/4 36*-6 .0001 .002 0-100 3 El 1,9 1 514 170 676'-9/4 36'-6 .0001 .002 0-100 3 El 1,9 } S15 170 I 676'-9,'4 36'-6 .0001 .002 0-100 1 El 1, 9 i 1 sit 170 676*-9/4 36'-6 .0001 .002 0-100 3 El 1,9 j _ S17 170 0-100
- -676
_' 9- /4 36'-6 .0001 .002 3 El 1, 9 1 ! Slr 170 676'-9 /4 36'-6 .0001 .002 0-100 3 El 1,9 i 1 S19 170 676'-9/4 36'-6 .0001 .002 0-100 3 El 1,9 S20 170 676'-9/4 36'-6 .0001 .002 0-100 3 El 1,9 i f S21 170 676'-9/4 36'-6 .0001 .002 0-100 3 El 1,9 S22 170 6 7 6 '-9h4 36'-6 .0001 .002 0-100 3 El 1,9 1 } S23 170 674'-7 36'-6 .0001 .002 0-100 3 El 1 i s. ! E24 170 674'-7 36'-6 i
.0001 .002 0-100 3 El 2,9 e
! S23 170 674'-7 36'-6 .0001 .002 0-100 3 El 2,9 ] S26 170 674'-7 36*-6 .0001 .002 0-100 3 El l 9 1 _ _ _ _ _ _ _ _ .- . -~ .-
l LA SALLE COUNTY - 1 C0 m0NWEALTH EDISON COMPANY TABLE 4 "A"'E 2_ Or 2._
)
{ PROJECT NO. 5835-00 1
!E STRAIN GAUGE DATA ,g 4 l
f SENSOR LOCATION 4 SENSOR EXPECTED EXPECTEC ACCURACY ENVIRON. NOTE 5
! NUMBEE RESPON5E FREQUENCf MENT j RA vie j AZIMUTH ELEV. RADIUS (IN/IN) (H2) (1 %
l (DEG) (FT-IN) (FT-IN) F.S.) 1 i S27 170 674'-7 36*-6 .0001 .001 0-100 3 El 2,9
.h
{ S28 170 674'-7 36'-6 .0001 .001 0-100 3 El 2,9 S29 170 674'-7 36'-6 .0001 .001 0-100 3 El 2,9 i S30 170 674'-7 36'-6 .0001 .001 0-10C 3 El 2,9 l S31 174 - 32'-9 .0001 .001 0-10E 3 El 6,7,10 S32 174 - 32'-9 .0001 .001 0-100 3 El 6,7,10 S33 174 - 32'-9 .0001 .001 ')- 10 ) 3 El 6,7,10 S34 174 - 32'-9 .0001 .001 0-103 3 El 6,7,10
; S35 246 -
23'-3 .0001 .001 0-103 3 El 6,7,10 3 t S36 2 4 t. - 23'-3 .0001 .001 0-100 3 1:1 6,7,10 I S ri 246 -- 23'-3 .0001 .001 0-100 3 El 6,7,10 J S38 246 - 23'-3 .0001 .001 0-1E0 3 El 6,7,10 S39 250 681*-2 43'-4 .0001 .001 0-100 3 El 2,9 j S40 250 681'-2 43'-4 .0001 .001 0-100 3 El 2,9 S41 250 681'-2 43'-4 .0001 .001 6-130 3 El 2,7,9 l S42 250 681'-2 43'-4 .0001 .001 0-130 I 3 El 2,7,9 S43 250 681'-2 43'-4 .0001 .001 0-130 3 El 9 S44 250 681*-2 43'-4 .0001 .001 0-100 3 El 9 S45 230 681'-2 43'-4 <* 0001
. 1-50 3 El 10
, S46 230 681'-2 43'-4 " .0001 1-Y0 3 10 El 1 S47 230 681'-2 43'-4 '".0001 1-50 3,10 3 El 849 230 681'-2 43'-4 ~ .0001 1-50 3 3,10 El l l S49 230 681'-2 43'-4 ~.0001 i 1'O 4,10
- I El 3
J S50 : j 230 681*-2 43*-4 ".0001 1-50 3 El 5,10 t l l l l
Revision 4 TABLE 4 STRAIN GAUGE DATA NOTES !Il (1) Gauges on SRV Discharge Pipe / Quencher may experience temperature up to 500 F. (2) The following sets of Strain Gauges should be arranged in a Rectangular Rosette Pattern: (S25, S27, S28), (S24, S29, S30) and (S39, S43, S44). (3) These are redundant sensors to S45 and S46. (4) Sensor is centered between stiffeners and oriented along the short direction. (5) Sensor is centered on the stiffener opposite sensor S49 and aligned with the long direction. (6) Sensor elevation is shown in Figure 5. (7) The followie. sets of Strain Gauges should be wired in I a half-bridge fashion in order that their signals add on a bending moment and subtract on elongation. (S1, S2); (S3, S4); (SS, S6); (S7, S8); (S31, S32); (S33, S34); (S35, S36); (S37, S38); (S41, S42). (8) Strain gauge mounted on SA-106 - Grade B steel. (9) Strain gauge mounted on SA-358 - Grade 316L steel. Strain gauges mounted on SA-240-TP-304 stainless steel. I (10) GENERAL NOTES Location Sensor No. Function SRV Discharge S1, S2, S3, S4, Measurement of bending strains; I Line IMS04BM-12 (Discharge line having largest SS, S6, S7, S8 in radial and tangential planes. For determining bending stresses resulting I air volume) from self-imposed SRV dis-charge loads. Placement of strain gauges is based on exoected locations of maximum , s' tress. SARGENT&LUNDY
..~ .~...._ e - -- --
ll 3 ef 5
Revision 4 TABLE 4 STRAIN GAUGE DATA GENERAL NOTES Location Sensor No. Function Quencher Assembly S9, S10, Sll, Measurement of quencher arm and Support S12, S15, S16, bending strains in two (Quencher corres- S17, S18 mutually perpendicular planes,L ponding to SRV parallel'to the arms longitu-; discharge line dinal axis. For determining 1MS04BM-12) bending stresses resulting from self-imposed SRV dis-charge loads. I Quencher Assembly and Support (Quencher corres-S13, S14, S19, S20, S21, S22 Measurement of hoop strains in quencher arms and sphere for determining approxima-ponding to SRV tions of thermal transient discharge line and pressure stresses. 1MS04BM-12) Quencher Assembly S23, S24, S25, Measurement of bending strainsj and Support S26 in the quencher support in thea (Quencher corres- radial and tangential planes. ponding to SRV For determining bending discharge line stresses resulting from self- l 1MSO4BM-12) imposed SRV discharge loads. Quencher Assembly S27, S28, S29, To be combined with S24 and and Support S30 S25 to form two rectangular (Quencher corres- rosettes. The strain rosette ponding to SRV will be used to calculate discharge line support torsional stresses 1MS04BM-12) resulting from self-imposed discharge loads. Downcomer S31, S32, S33, Measurement of bending strains (Az. 147 , S34 in radial and tangential Radius 32'-9", planea. For comparison with L Az. 246 , S35, S36, S37, stresses calculated from Radius 23'-3") S38 analytically predicted sub-merged structure loadings. Placement of strain gauges is based on expected locations of maximum stress. SARGENT&LUNDY 1 ENGINEERS _ r - _ - _ _ -
^
4 of 5
l Revision 4 1 TABLE 4 STRAIN GAUGE DATA GENERAL NOTES Location Sensor No. Function RHR Suction Line S39, S40, S41, Measurement of bending strains (Az. 250 , S42 in and out of the plane of Radius 4 3 '-4 ") the elbow. For comparison with stresses calculated from analytically predicted sub-merged structure loadings. RHR Suction Line S43 and S44 To be combined with S39 to c (Az. 250 , form a rectangular rosette Radius 4 3 '-4 ") for calculating torsional stresses. For comparison with stresses calculated from analytically predicted submerged structure loadings. Containment S45 and S46 To record the strain responsesL Wall Liner in the containment wall most likely to experience a net suction pressure loading, if any. Containment S47 and S48 Backup sensors to S45 and Wall Liner S46. Basemat Liner S49 and S50 To record the strain responses in the basemat liner and liner stiffeners. They are located in an area most likely to experience a net uplift pressure loading, if any. I SARGENT&LUNDY
..~.~.... - - - - -
5 of 5
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I Revision 4 i 1 i
- s I
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- ,i in APPENDICIES .
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Revision 4 ^ APPENDIX A ~ TEST MATRIX w ~ Nominal ** /" Initial Discharge Type of Valve (s) Initial Initial Test Actuated Water Leg Pipe Temp. Pool Temp. Duration (sec) r - SRV-1 C NWL+ CP, HP NT 15 SRV-1 G NWL+ CP, HP NT 15 m SRV-1 H NWL+ CP, HP NT 15 SRV-1 M NWL+ CP, HP NT 15 SRV-1 R NWL+ CP, HP NT 15 E " SRV-C C NWL* CP* NT 15 SRV-C G NWL* CP* NT 15 - SRV-C M NWL* CP* NT 15 u SRV-2 C,H NNL+ CP, HP NT 15 SRV-2 C,R NWL+ CP, HP NT 15 SRV-2 C,R NWL+ CP/HP NT 15 SRV-2 C,G NNL+ CP, HP NT 15 m l SRV-4 C,G,H,R NWL CP NT 15 " SRV-S C,G,H,R NWL CP NT 15 SRV-E C NWL CP NT 600 SRV-E H NWL CP NT , 600 m SRV-L M --- HP NT 15 NOTES: The number of times each type of test should be repeated is to be determined from statistical considerations.
* = After first actuation temperature and water level change.
- ** = 15-second nominal time can be 5 to 20 seconds actual; extended blowdown may be limited by plant limits. - + = Cold pipe only i The SRV Discharge Ouenchers of valves M, G, C, f! , and R are located at 170*, 210 , 230 , 252*, and 264*, respectively. - SRV-1 = One valve actuation CP = Cold Pipe SRV-C = Consecutive valve actuations HP = Hot Pipe SRV-2 = Two valve actuation CP/HP = One Hot & One Cold Pipe ~ SRV-4 = Four valve actuation NWL = Normal Water Level - SRV-S = Sequential valve actuation NT = Normal Pool Temperature SRV-E = Extended valve blowdown _; SRV-L = Leaky valve simulation 1 of 1
Revision 4 APPENDIX B Specifications for Sensors Accelerometer Specifications: (Endevco 7704-100 Accelerometer) (used outside containment) Charge Sensitivity Nominal: pC/g 100 I Minimum: pC/g 90 Frequency Response (15% charge deviation); Hz 1 to 5000 Mounted Resonant Frequency Nominal: Hz 20,000 Transverse Sensitivity Maximum: % 3 Temperature Response (15% charge deviation): F -65 to 500 Amplitude Linearity % Sensitivity
'E increases 1%
- n per 250 g's.
Accelerometer Specifications: (Endevco 7717-200 Accelerometer) (used in Containment Drywell) Charge Sensitivity Nominal: pC/g 200 Minimum: pC/g 180 i~ - Frequency Response (15% charge deviation): Hz 1 to 4000 Mounted Resonance l 4 Frequency Hz 17,000 l 1 of 9
Appendix B Continued Revision 4 l I Transverse Sensitivity 9 Approx. 15 liz: % 3 max. i l Temperature Response l (+5% charge deviation): r -65 to 572 Amplitude Linearity: Sensitivity increase i approx. 1% per 250 g. I i l Accelerometer Specifications: (Endevco 7717-M2A Accelerometer) l (used in Containment Wetwell) Charge Sensitivity Nominal: pC/g 200 Minimum: pC/g 180 Frequency Response l (+5% charge deviation): Hz I - 1 to 3000 1 i Mounted Resonance Frequency: liz 17,000 Transverse Sensitivity @ j I Approx. 15 Hz: % 3 max. Temperature Response (+5% charge deviation): r -65 to 572 l Amplitude Linearity: Sensitivity increase approx. 1% per 250 g. l RTD Specifications: (Medtherm PTF-XXX-10356) (used in all applications except pipe outside surface temperature measurement) l l Type: Platinum thin resistance I thermometer on ceramic substrate. l 2 of 9 i ^
i i i I Appendix B Continued Revision 4 I I Resistance: 100 ohms at 0 C, 138.50 ohms at 100*C. i Temperature Range: 50 - 600 F f Presnure Range: 0 - 1500 psig i' Reference Time: 5 milliseconds I - Accuracy: 1 0.5 F I RTD Specifications: (Medtherr. PRT-XXX-10387) l I (used for pipe outside surface temperature measure ment) Type: Platinum Resistance Thermometer i .i I - Resistance: 100 ohms at 0 C, 138.5 ohms at 100 C Temperature Range: 50 F to 500 F } Pressure Range: 0 - 700 psig Response Time: 1 second typical (Ailtech MG125) ) Strain Gauge Specifications: I - Element Type: A Resistance: 120 + 5 ohms Gauge Factor: 1.7 1 3% i Gauge Factor Change with , Temperature: -l%/100 F Pressure Rating: 0 - 2500 psig 3 of 9
1 Appendix B Continued Revision 4 Pressure Sensor Specifications: (CEC 1000) !
- (used for ranges 0-100, 0-300, 0-50 psig) i
- PRESSURE RATING
Proof Pressure: 200% of rated pressure, not to exceed 7,500 psi, will not cause changes in per-formance beyond the specified tolerances. Burst Pressure: 300% of rated pressure, not to exceed 10,000 psi, will not cause rupture of the sensing element or case.
- ELECTRICAL CHARACTERISTICS
Excitation: 10 Vdc rated; 15 Vdc maximum Full range output: 30 mV minimum Residual unbalance: within +2%, FRO Bridge Resistance: 300 to 500 ohms Combined Linearity, Hysteresis and non-repeatability: +0.25% FRO, BSL I - Insulation kesistance: 500 megohms or greater at 45 Vdc. Breakdown Voltage: 100 Vdc or pk ac between case and any terminal without damage. I I Connections: 6-pin Bendix PTIH-10-6P, or equivalent. 4 of 9
I Appendix B Continued Revision 4 Shunt Calibration: Provisions for single-arm, oxternal shunt calibration. MECHANICAL CHARACTERISTICS: Mounting Isolation: Double case isolation provides assurance that the sensing element will be unaffected by external stresses. Sensing Element: 4 active arm bridge using sputtered elements. ENVIRONMENTAL PERFORMANCE: Temperature: Operating Range: -65 to F300 F Compensated Range: -65* to +250*F Thermal Zero Shift: +0.005 FRO / F over the compensated temp. range. Thermal Sens. Shift: +0.005/ F over the compen-sated temp. range. Thermal Zero Stability: 0.15% FRO over the compen-sated temp. range. Thermal Sensitivity Stability: 0.10% FRO over the compen-sated temp. range. Vibration: Qualification Level of 35 g. pk; 5-2000 Hz Max. 1/2" D.A. Less than 0.003% FRO /g 5 of 9
Appendix B Continued Revision 4 Shock: Qualification level of 100 g. 11 msec, half sine wave without damage. lI - Humidity: Per MIL-E-5272C Proc. 1. Altitude: Insensitive to external case pressure variations within the range of 0 to 25 psia.
- Performance Stability: +0.1% FRO for a minimum of 4 hours when subjected g to any combination of constant temperature and g pressure within the speci-fied limits.
Pressure Sensor Specifications: (CEC 1000-04 Sputtered Thin Film High Temperature Pressure Transducer) (used for 0-1000 psig range) PRESSURE RATING: Proof Pressure: 0 to 100 psi and above are available in psis. 200% of rated pressure or
- g 15,000 psi (whi.chever is 3 less) will not ,ause changes in performance beyond specified tolerances.
Burst Pressure: 300% of rated pressure or 20,000 psi (whichever is j less) will not cause rupture ; of the sensing element or ;
;g .g case.
ELECTRICAL CHARACTERISTICS: Excitation: 10 Vdc rated; 15 Vdc maximum 6 of 9
j Appendix B Continued Revision 4 I Full Range Output: 30 mV nominal. l Residual Unbalance: within +5%, FRO. i 1 Bridge Resistance: 300 to 500 chms. l / - Combined Linearity, Hysteresis and non-repeatability: +0.25% FRO, BSL. l Insulation Resistance: 100 megohms or greater at 45 Vdc. i Connections: 6-pin Bendix PCIH-10-6P (101), or equivalent. 1 Shunt Calibration: Provisions for single-arm, j external shunt calibration. : 11 i j MECHANICAL CHARACTERISTICS: Mounting Isolation: Double case isolation
, provides assurance that the sensing element will be unaffected by external j stresses.
i Sensing Clement: 4 active-arm bridge using sputtered elements. ENVIRONMENTAL PERFORMANCE: l i Temperature: l l-1 l Operating Range: -65 to +450 F. I Compensated Range: +75 to +400 F. i
- g lE Thernal Zero Shif t
- 10.01% FRO /*F over the i compensated temp. range.
l 7 of 9
I Appendix B Continued Revision 4
+0.01% F"O/ F over the I Thermal Sens. Shif t:
compensated temp. range. Thermal Zero Stability: 0.25% FRO ,:ver the compen-sated temp. range. Thermal Sens. Stability: 0.15% FRO over the compen-sated temp. range. I - Vibration: At 35g peak from 10 to 2000 Hz (1/2" D.A. max.) the out-put shall not exceed 0.04% FRO /g for 15 psi units decreasing logarithmically to .003% FRO /g for 1000 psi units and above. Natural Fregua my: 50 kHz at 5000 psi, decreasing logarithmically to Skliz. at 15 psi. Shock: 100g, 11 msec, half sine wave without damage. Humidity: Per MIL-E-5272C, Procedure 1.
~
Pressure Sensor Specifications: (Validyne AP-78-44-1590) I (used for low pressure measurement after high pressure spike) Pressure Range: 20-32 PSIA Linearity: +0.5% FS best straight line Hysteresis: 0.5% pressure excursion Overpressure: 3 Differential: 200% FS up to 6000 psi maximum 8 of 9
L Appendix B Continued Revision 4 m L_ Absolute: 20 PSIA or 200% FS whiche.er is greater, up to 6000 PS2 r maximum i I l Differential Line Pressure: 5000 ps.ig operating l Line Pressure Effect: Less than 1% FS Zero shift / 1000 psig 1 Output: 40mV/V full-scale (typical) i - Inductance: 20mH nominal, each coil I Zero Calance: Within SmV/V Excitation: Rated: SV RMS, 3 kHz I Corrosive liquids and gases ; Pressure Media: compatible with 410 CRES and : l. Inconel j Tempe ratu re Operating: -65 F to +250 F ^ Compensated: 0 F to +160 F , 1 psi and above, 0.02%, l l Thermal Zero shift: (typ) FS/ F l Below 1 psi, 0.04% (typical) i FS/ F i
- Thermal Sensitivity Shift: 0.04%/ F (typical) i
\ Pressure Connection: 0.125" O.D. by 1" stainless ,I steel tubing l l - Electrical Connection: 8-inch wire leads I ll e er e .
{ Revision 4 J l ' APPENDIX C Specifications for Vishay System Brid 3 e Completion: 1/4 bridge completio- . network per channel 'I - Bridge Balance Range: 3000 micro-inches / inch I I - Calibration: Internal calibration of
+1%
Amp Gain: 100 to 2000 continuous or j s tcps o f 100, 500, 1000, l and 2000 I i Input: Differential 4 Input Impedance: 25 megohms differential or j common mode Output: +10V maximum j Linearity:
+0.05% to DC e
i Stability II 0.5% after 15 minutes 1 1 l 1 l ) i l 1 of 1 i
Revisien 4 APPENDIX D Specifications for Charge Amplifier ENDEVCO Model 2721AM4 and Charge Converter Signal Conditioner Endevco l Model 4479.lM3/2652M11 ( 2721AM4 INPUT INPUT CONNECTION Single-ended with one sida connected to circuit common; restricted for use with capacitive devices. SOURCE IMPED 7d'CE 1 k ' minimum shunt resistance; 30 000 pF maximum shunt capacitance. MAXIMUM INPUT 30,000 pC pk without overload SLEW RATE 1,000 pC/us maximum j OUTPUT 1 OUTPUT CONNECTION Single-ended with one side connected to circuit conunon , l LINEAR OUTPUT VOLTAGE +10 V, maximum LINEAR OUTPUT CURRENT +2 mA, maximum OUTPUT IMPEDANCE 100 +10% l RESIDUAL NOISE Ne <0.03 pC rms +00.008 pC rms per 1,000 pF of source capacitance, referred to input. Nr = pC ras (typical)
/liS where Rs $100 kn Noise = /NO2 + Nr2 1 of 4
i ) i' Appendix D Continued Revision 4 i TRANSFER SYSTEM SENSITIVITY Amplifier gain is continuously adjust-able to allow for indicated calibrated l system sensitivity for transducers l l with sensitivities of 1 to 100 pC/g. i I l INDICATED RANGES 1, 3, 10, 30, 100 mV/g for 1 to 11 pC/g: 10, 30, 100, 300, 1,000 mV/g for 10 to 110 pC/g. GAIN ACCURACY 11% of actual gain for source impedance i
>10 kn and/or <10,000 pF t
s GAIN STABILITY 1200 ppm / F, maximum I FREQUENCY RESPONSE 15%, lHz, with source, impedance l 2721AM4 >300 kn } I i ENVIRONMEl?TAL TEMPERATURL 0 C to 75 C (3 2 *F to 167
- F) j HUMIDITY 95% relative humidity, maximum 4479.lM3/2652Mll j ELECTRICAL 1
l INPUT CHARACTERISTICS j (2652M11) { Input Connection Single-Ended i Source Impedance Capacitive devices only. j Shunt resistance 25 M.7 minimum. j Source Capacitance 10,000 pF, maximum . OUTPUT CHARACTERISTICS l (2652Mll) l Output Connection Single-Ended l Output Impedance 5 ohms nominal, when used with 4479.1. I 2 of 4 i
l i Appendix D Continued Revision 4 I ). I Maximum Capacitance between 2652Mll and To meet all specifications, C = K/fuF, )j 4479.lM3 where f is maximum frequency of j l interest and K = 330,000 tor 1 pc full , j scale, K = 3,000 for 100 pc full scale, ' i K= 85 for 3,000 pC full scale. l Worst case: 8500 pF maximum at 10,000 Hz j and 3,000 pC pk input signal. INPUT CHARACTERISTICS (4479.193) Input Connection Single-Ended l Input Resistance 1000 ohms in series with 390 pF l OUTPUT CllARACTERISTICS i (4479.lM3 Card) ) I i Output Connection Single-Ended Linear Output Volt 2.5 V pk, Full Scale lg j Linear Output Current 2.5 mA pk, maximum ig Output Impedance 50 ohms, maximum, in series ! with 200 pF. l ! POWER (R40) +30 V dc from 4470 set by program i resistor on mode card. i TRANSFER CHARACTERISTICS (2652M11 and 4479.lM3) Full Scale Ranges for Sensitivities: 1 10 to 100 pC/g 0.1, 0.3, 1.3, 10, 30g Actual Gain 0.8 to 2500 mV/pC System Accuracy 3% of F.S., any range at +24 C f (+75 F) and source capacitance of 1000 pF, maximum. Gain Stability Better than 0.5% per 1000 pF 4 source capacitance. I Better than 2%, -10 C to +65 C J t (+15 F to +150 F). Gain decreases ! approximately 1% for every 10 ohms cable resistance. Frequency Response 5%,lHz to 10,000 Hz { Linearity !0.5% of reading from best straight line. Total Harmonic Distortion 0.2%, maximum ! Residual Noise Less than the total of 0.0075 pC rms j plus 0.0025 pC rms per 1000 pF source i capacitance referred to input plus ! 0.5mV rms referred to output. i ! PHYSICAL ! MODE CARD (4479.Ul3) Designed for plugging into from panel ' of 4470 Module. l l l ! ) 1 3 of 4 J-- , _ _ .
I Revision 4
} , Appendix D Continued 4
1 I
- l. CONNECTORS (2652Mll)
Input (J1) Coaxial, 10-32 thread, Microdot { S-50 Series or equivalent. j 1 Output Solder terminals. l MOUNTING (2652M11) Converter mounts in 13/16" hole. l W sher and 11/16" x 28" nut supplied. l E 1E mONTROLS (on Mode Card) Sensitivity (R30) Ten turn potentiometer, with calibrated l turns dial. t Six position rotary switch. j j F"ll : scale (S1) ' i j ENVIRONMENTAL OPERATINC TEMPERATURE i 3 -54 C to +85 C (-6 5 l' to +18 5 F) (2652Mll) 1 l l I J 1
)
1 l i 6
- I l
ll 4 4 of 4 i,- - . ... _ - . _, . _ - _ _ _ - . . . . _ - - . _ _ _ _ . _ - - . . --- , - . _ _ _ _ . - - . - .
Revision 4 APPENDIX E Q.S.I. System Performance Characteristics Record Electronics Analog Input Channels: Expandable to 256 channels in 16 channel blocks. I Digital Input Channels: Expandable to 32 channels up to 16-bit parallel with handshake transfer. Frequency Response Range: 200 Hz Throughput Rate: 1000 samples /sec/ channel Recording Capacity: Up to 145 Megabytes per reel. Analog input Impedance: 10 Megohms Conversion Method: Successive approximation with S/H input amplifier. Conversion Code: 2's complement binary Conversion Resolution: 12 bits including sign Dynamic Range: 66 dB l Conversion Accuracy: 0.01% F.S., + 1/2 LSB Input Level-Analcg: 15 FS, 115V FS maximum overvoltage protected. Digital: Standard TTL Logic Levels Time Code Data: Days, hours, minutes, and seconds may be entered into tape records as required. Header Data: Manual.ly entered by operator via front panel keyboard. Power: 1800 W, 110V AC, 110%, 50-60 Hz. Playback Electronics 3 - Number of Output Channels: One (expandable up to eight I channels) 1 of 2
) Appendix E Continued Revision 4 i I) - Throughput Rate: Up to 250,000 samples per second. Speed-Up Factor: Up to 1000:1 and beyond 's limited only by throughput I rate. Conversion Code: 2's complement binary Conversions Resolution: 12 bits including sign Setting Time: 3 microsec to 1/2 LSB j' Slew Rate Output Voltage: 20V/second standard for iSV FS; other ranges optional Output Current: 1 5 ma Output Filter: 4-pole active Bessel, l ' Butterwortl or Tschebychev optional Conversion Accuracy: 10.05% FS i LSB at 25 C Temperature Coefficient: 20 ppm / C ! 1 - 1 Time Code Data: Days, hours, minutes, and ; seconds may be read from ' , tape records and displayed. l l Tape Transport Characteristics i Format: IBM compatible ; i Number of Tracks: 9-track i l . Density: 6250 BPI, GCR I Record Length: 4096 bytes Tape Speed: 125 ips l t a . _ _ _ - . - - . - . _ . _ . - - . - - . _ _ . _ . _ . - _ . -
L r L Revision 4 m L APPENDIX F Specification for RTD Signal Conditioner f~ L r i Analog / digital integrated circuit design. l e g - ll7V AC 60 Hz or 24V DC 1201 regulation. Nominal ambient temperature range -20 F/120'r. E - Calibration accuracy 10.101. l r - Linearity/ repeatability 10.10%.
- 1 Temperature sensitivity 10.0025%/ F. l Line voltage sensitivity 10.0001%/17 line change.
Signal isolation from de power source is standard. Optional input to output signal isolation is lkVp-p. Extremely high common / normal mode rejection. Digital circuit resolution, J0 bit minimum. Zero droop sample-hold and ramp generator circuits. Output circuits. Current (automatic AR loop correction) 1/5mADC into 0-2400 astd., 0-5000 copt., 4/20mADC into 0-600 astd., 0-1500 copt., 10/50mADC into C-300 nstd., 0-600 nopt. Voltage (nominally zero source impedance). O to 10 mADC into load. Control Relay, 10 Amp contacts, resistive. ! Pulse, any V or I, source or sink. Input impedances. I n 1/SmA is 2000 , 4/20mA is 50 . , 10/50mA is 20n. E v and mv is greater than 10 megohm. h f 1 of 1
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