ML20063E258

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Revision B to Anticipatory Reactor Trip Sys Seismic Qualification Test Plan
ML20063E258
Person / Time
Site: Davis Besse 
Issue date: 01/27/1982
From: Loczi V, Schuessler J
AUTOMATION INDUSTRIES, INC.
To:
Shared Package
ML20063E227 List:
References
3394.01, NUDOCS 8207130362
Download: ML20063E258 (14)


Text

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Rev.

Date Approved A

5/4/81 gig B

1/27/82 M[h ANTICIPATORY REACTOR TRIP SYSTDi

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SEISMIC QUALIFICATION TEST PLAN No. 3394.01 May 21, 1980 Prepared by:

Approved by:

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V. Loczi J. C. Schuessler g AUTOMATION INDUSTRIES,INC.

VITRO LA8 ORATORIES DIVISION I ?!$YEImunoano 8207130362 820708 PDR ADOCK 05000346 P

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i AUTOMATIONINDUSTRIES,INC Sheet 1 of 12 VITRO LABORATORIES DIVISION Revision A ANTICIPATORY REACTOR TRIP SYSTEM SEISMIC QUALIFICATION TEST PLAN 10 SCOPE 1.1 This test plan describes a program which will verify that the Anticipatory Reactor Trip System (ARTS) for the Davis-Besse Nuclear Power Station Unit No. 1 can withstand, without loss of safety function, the effects of seismic occurrences which cause a floor response as depicted in Attachments 9 through 14 to Specification No. 7749-E-241Q.

2.0 APPLICABLE DOCUMENTS 2.1 Bechtel Power Corporation Specification No. 7749-E-241Q, Revision 0F, dated September 26, 1980.

A 2.2 IEEE 344-1975, "IEEE Recommended Practices for Seismic Qualification of Class lE Equipment for Nuclear Power Generation Stations".

2.3 Vitro Laboratories, " Seismic Electrical Test Procedure" TP 3394-1032.

A 2.4 Wyle Laboratories, " Seismic Test Procedure" 541/4303/DK.

l 3.0 EQUIPMENT FOR SEISMIC TEST 3.1 The Anticipatory Reactor Trip System is contained in a Hof fman Engineering Company NEMA 12 wall-mounted cabinet enclosure approxi-mately 48 inches high, 36 inches wide, and 12 inches deep. A ccepletely assembled, operating, deliverable enclousre will be j

seismically tested.

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AUTOMATION INDUSTRIES,lNC.

Shest 2 of 12 VITRO LABORATORIES DIVISION Revision:

None 4.0 SEISMIC QUALIFICATION 4.1 The enclosure and devices will be qualified by tests in accordance with IEEE 344-1975.

Seismic tests of the ARTS enclosure will be random-mo tion, multiple-f requency, phase-independent tests with simul-taneous horizontal and vertical inputs.

The Test Response Spectra from the control accelerometers will envelop the Required Response Spectra at the required damping value. During qualification testing, the acceleration levels at specific device locations will be monitored.

The devices will be operational and electrically monitored to verify there is no degradation due to the seismic occurrence.

4.2 At least thirty days prior to testing, Bechtel/Gaithersburg, will be notified of the testing schedule and location to afford the opportun-icy to witness any or all parts of the test and subsequent inspection.

5.0 SEISMIC TESTS 5.1 The cabinet enclosure will be bolted to a vertical wall on the test table as shown in Figure 1.

Af ter the cabinet is bolted in place, accalerometers will be idstalled in the cabinet in accordance with Figure 1, and two control accelerometers will be attached to the test table.

The tested arrangement duplicates the actual plant installa-tion.

5.2 Exploratory Tests - Axis Y and Axis Z Exploratory Tests will consist of a single-axis continuous one octave l

GD AUTOMATION INDUSTRIES,1NC.

Shast 3 of 12 VITRO LABORATORIES DIVISION Revision:

None per minute sueep frequency search using a sinusoidal steady-state input of approximately 0.2 g from 0.5 Hz to 50 Hz to determine equipment resonances. The horizontal and vertical axes identified as Axis Y and Axis Z in Figure 1 will be tested first.

5.3 0.B.E. Proof Tests - Axis Y and Axis Z Five 0.B.E. proof tests will be conducted on the cabinet. The cab-inet will be subjected to simultaneous horizontal and vertical inputs of random-motion consisting of frequencies spaced one-third octave apart over the frequency range of 1.0 Hz to 33 Hz.

The amplitude of each one-third octave frequency will be independently adjusted in an iterative process in each axis until the Test Response Spectra (TRS) from the control accelerometers envelops the Required Response Spectra (RRS) at a damping of 2% by a spectrum analyzer.

The RRS is defined by Figure 2 for the Y Axis (horizontal) direction, and by Figure 3 for the Z Axis (vertical) direction. The cabinet will be excited by simultaneous horizontal and vertical input accelerations for a period of 30[ seconds.

Following the fif th 0.B.E. proof test, the equipment will be examined for damage and hardware will be retightened if necessary.

5.4 S.S.E. Proof Test - Axis Y and Axis Z One S.S.E. proof test will be conducted on the cabinet.

The cabinet will be subjected to simultaneous horizontal and vertical inputs of random-motion consisting of f requencies spaced one-third octave apart over the frequency range of 1.0 Hz to 33 Hz.

The amplitude of each L

<> AUTOMATION INDUSTRIES,INC.

Sh nt 4 of 12 VITRO LABORATORIES DIVISION Revisicn: None one-third octave frequency will be independently adjusted to an iterative process in each axis until the TRS from the control accel-erometers envelops the RRS at a damping of 2% by a spectrum analyzer.

The RRS is defined by Figure 4 for the Y Axis (horizontal) direction, and by Figure 5 for the Z Axis (vertical) direction. The cabinet will be excited by horizontal and vertical input accelerations for 3

a period of 30+0

- seconds. Following the test, the equipment will be examined for damage and hardware will be retightened if necessary.

5.5 Exploratory Test - Axis X An Exploratory Test will consist of a single-axis continuous one octave per minute sweep frequency search using a sinusoidal steady-state input of approximately 0.2 g from 0.5 Hz to 50 Hz to determine equipment resonances.

The horizontal axis identified as Axis X in Figure I will be tested.

5.6 0.B.E. Proof Tests - Axis X and Axis Z Five 0.B.E. proof tests will be conducted on the cabinet. The cabi-net will be subjected to simultaneous horizontal and vertical inputs of random-motion consisting of frequencies spaced one-third octave apart over the frequency range of 1.0 Hz to 33 Hz.

The amplitude of each one-third octave frequency will be independently adjusted in an iterative process in each axis until the TRS from the control accelerometers envelops the RRS at a damping of 2% by a spectrum analyzer.

The RRS is defined by Figure 2 for the X Axis (horizontal) <

AUTOMATION INDUSTRIES,INC.

Sheet 5 of 12 VITRO LABORATORIES DIVISION Revision: None direction, and by Figure 3 for the Z Axis (vertical) direction.

The cabinet will be excited by horizontal and vertical input accel-erations for a period of 30[3 seconds.

Following the fifth 0.B.E.

0 proof test, the equipment will be examined for damage and hardware will be retightened if necessary.

5.7 S.S.E. Proof Test - Axis X and Axis Z One S.S.E. proof test will be conducted on the cabinet. The cabinet will be subjected to simultaneous horizontal and vertical inputs of random-motion consisting of frequencies spaced one-third octave apart over the frequency range of 1.0 Hz t,o 33 Hz.

The amplitude of each one-third octave frequency will be independently adjusted in an iter-ative process in each axis until the TRS from the control accelerom-eters envelops the RRS at a damping of 2% by a spectrum analyzer.

The RRS is defined by Figure 4 for the X Axis (horizontal) direction, and by Figure 5 for the Z Axis (vertical) direction.

The cabinet will be excited by horizontal and vertical input accelerations for a period of 30[ seconds. Following the test, the equipment will be examined for damage and hardware will be retightened if necessary.

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5.8 Photographs will be taken of the test setup, accelerometer locations, and any noticeable physical damage.

5.9 Following the test, the equipment will be crated and shipped to Vitro Laboratories.

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7 AUTOMATION INDUSTRIES,1NC.

Sh ut 6 of 12 VITRO LABORATORIES DIVISION Revision:

None 6.0 ACCEPTANCE C hTERIA 6.1 The criteria for acceptance or failure of the cabinet enclosure will include the following:

(a) The direction of cabinet testing shall comply with Figure 1.

(b)

Sufficient accelerometers shall be attached to the cabinet in order to provide a profile of g levels, both horizontally and vertically, at all points of interest in the cabinet.

(c)

The cabinet shall be tested to the seismic level of the accel-eration response spectra of Figures 2 through 5 when analyzed at the required damping value.

(d) The cabinet shall demonstrate sufficient structural integrity so proper functioning of Class 1E devices is not compromised.

6.2 The criteria for acceptance or failure of devices will include the following characteristics as applicable during and af ter testing:

(a)

No loss of output signal, short or open circuit.

(b) No closing of an open, or opening of a closed output relay contact greater than 2.0 milliseconds.

(c) No structural failure, broken or loosened parts, or deflection which could cause interference with the safety related functions.

II AUTOMATION INDUSTRIES,lNC.

Sheet 7 of 12 VITRO LABORATORIES DIVISION Revision A (d) No loss of required function, ability to change state or position.

7.0 DOCUMENTATION 7.1 The electrical tests conducted during the seismic tests are described in TP 3394-1032, Seismic Eeletrical Test Procedure. The seismic tests A

are conducted in accordance with Wyle Laboratories Test Procedure No.

541/4303/DK.

7.2 A report will be prepared which documents the results of the test program and provides verification that the Anticipatory Reactor Trip System can withstand the specified seismic occurrences at the Davis-Besse Nuclear Power Station without loss of safety function.

The test report will be prepared in accordance with the outline presented in paragraph 8.4 of IEEE Standard 344-1975, and 'will contain:

(a)

Equipment Identification (b)

Equipment Specification (c) Test Facility (d) Test Equipment and Calibration Due Dates (e) Test Methods and Procedures (f)

Test Data (g)

Results and Conclusions (h)

Signature and date by a registered professional engineer.

(1) Approval signature and date by a knowledgeable of ficer of the company.

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O AUTOMATION INDUSTRIES,1NC.

Shest 8 of 12 VITRO LABORATORIES DIVISION Revision:

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-13UNC, SAE Grade 5 Mounting Bolts 8 @ ft-lbs 4 places 3

50h Accelerometer Locations No.

Direction Device 1

Vertical Maximum Cabinet Response, All Devices 2

Horizontal Power Supply 3

Horizontal Digital Isolator 4

Horizontal Control Panel / Card File 5

Horizontal Relay and Terminal Block 48

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Y Axis Figure 1 y X Axis ANTICIPATORY REACTOR TRIP SYSTDi CABINET AND ACCELEROMETER MOUNTING (Job 03394)

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VITRO LABORATORIES DIVISION APPENDIX B WLE LABORATORIES SEISMIC SIMULATION TEST REPORT NO. 45183 -1 FEBRUARY 11, 1982 i

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