ML18018A814
| ML18018A814 | |
| Person / Time | |
|---|---|
| Site: | Harris  |
| Issue date: | 06/11/1979 |
| From: | Esposito B, Gilfoy R, Tolf M ACTON ENVIRONMENTAL TESTING CORP. |
| To: | |
| Shared Package | |
| ML18018A805 | List: |
| References | |
| 14801-1, 14801-1-R01, 14801-1-R1, NUDOCS 8310130277 | |
| Download: ML18018A814 (63) | |
Text
~ra 6 t
Test Report. No.
148O1-1 Rev 1
No. of Pages Bepopt of Test on SEISMIC VIBRATION TESTING OF LIMITORQUE SMB-1/H3BC ACTUATORS FOR LIMITORQUE CORPORATION UNDER PURCHASE ORDER NO. TL516 6 N VI R 4 N hl KNTAL ACTQN CORPORATION Date June ll, 1979 Prepared By B. Esposf to ignea Date BE/hmf Checked R. Gk 1foy Approved M.L.Tolf 8310130277 830919 PDR ADQCK 05000400 E
0 P
SEISMIC TEST SMB-1-60/H3BC TEST REPORT f80048
SUBJECT:
Project 678037 - Pre Seismic Torque Switch Calibration and Monitoring performed during Seismic Testing.
REFERENCE:
Limitorque P/0 678037 Acton Report 814801-1 Unit Identification and Description SMB-1-60, I.D. 8678037-C mounted on an H3BC; I.D. 4678037-Cl.
Pre-Test Torque Switch Calibration Procedure:
Measured torque output of SMB-1-60/H3BC using 10,000'4 torque stand.
Result:
An actual torque of 5,740'f was obtained at a torque switch setting of 2 3/4.
Seismic Test Monitorin Procedure:
Both limit switch rotors and "open" torque switch were monitored for chatter by a 1 millisecond electronic chatter circuit.
The actuator was run from an open position (controlled by a limit switch), to a closed "torqued out" position (controlled by the torque switch) back to the open limit position during each of the seismic dwells and at the end of the seismic qual ification.
Result and Conclusion Refer to the general discussion of seismic tes ing for test reports B0047 and B0048 inserted in front of these reports.
V'cj I go~
Paul T. Young Assistant Chief Test Engineer
REV!SIC< RECORD DATE REV!S:Pj NUMBER PAGE NUMBER PP"-AGRAPH NUMBER CHANGES OR ADDITIONS APPROVED BY e
6/11/79
~mmF! RS
~
ISSUE 7/25/79 j
1 6
9 17 19-22 4.0 3.0 3:2 3.3 3.7 4.2 4.4 Figure 1
Changed 1/17/79 to 4/9/79 Reworded sentence Added word "Independently" Changed seismic aging test to "Plant Vibration Aging Test" in 4 places Added 6.0a sentence Changed seismic Aging Test to "Plant Vibration Aging Test" in 2 places Removed OBE curve o
(~
a 4I
~
e.
TZSTlpece r.exon <.
R N
14S01 -1 Report Ro.
ace ace Administrative Oats Limitorque Corporation Lynchburg, Virginia
~
SMB-1/H3BC
~
~
Limitorque Seismic Tes. of Limitorque SMB-3/H5BC and SMB-1/H3BC RED Project 678037 dated Aoril 9, 1979 Two (2) units marked g3 and 44 Unclassified Hay 10 197o C.Pilotte O.McLaughlin Returned to Limitorque Corporation.
4 ~
Refer to the results section herein.
Report No.
14801 Rev l 1
Page ACTON
nq,,
1.0 TEST rTEMS Two (2) Limitorque SMB-1/H3BC Actuators were submitted by Limitorque Corporation for seismic vibration testing at Acton Environmental Testing Corporation (AETC). The items were marked 43 and f4.
Report No.
14801 -1 ACTCIN Page 2
- The purpose of this test was to subject the actuators speci-fied in section 1.0 above to the seismic vibration tests specified in section 3.0 below to determine their ability to wi'thstand such vibration without evidence of mechanical damage, deterioration, loss of thei~ ability to operate properly, or contact chatter in excess of one (1) millisecond where applicable.
14801 Rcport No.
'CTCH 3.
Page
- 3. 0 TEST PROCEDURES This test was.performed under the direction of Mr. Pail Young of Limitorque Corporation fn accordance with Limitorque Seismic Test of Limitorque SMB-3/HSBC and SMB-1/H3BC, Research and Develop-ment Project 678037 dated April g,'lg7g.
14801 Report No.
Rev 1
ACTON Page 4
i
3.1 The actuator under test ~as bolted to a test fixture.
The test fixture was'hen secured to the appropriate vibration table.
Refer to the individual test description's for specifics.
Rqpo~ No 1 4801 1
. ACTON 5
PO3I ~
~ ~
~
~
e
~
3.2 Test Conditions All tests were performed at room temperature and pressure.
During the resonance survey specified in section 3.4 below, the actuator under test was not operated.
Ouring the qualification test specified in section 3.5, the actuator under test was cycled open and closed once/dwell.
Ouring the multiple frequency test specified in section 3.6 below, the actuator under tes., was cycled open and closed once/run.
Ouring the -aging tes. specified-in section 3;7.-below, the actuator under test was cycled at the beginning of each test and then once every fifteen (15) minutes during the test.
The actuator under test was subjected to some tests with the seismic support bracket and some tests without the bracket.
Refer to the individual test descriptions for specific details.
Rapo~ No 14801-1 Rev 1
ACTbN 6
Page
3.3 Test Monitorina The actuator under test was visually monitored or any evidence of mechanical
- damage, deter iorati on or loss 'of its ability to operate properly where applicable.
The actuator under test was monitored with accelerometers by AETC personnel to determipe its mechanical response.
Data from these accelerometers through appropriate signal condi-tioning was recorded on visicorder recording paper included with this report for all tests except the multiple frequency tests during which data was recorded onto magnetic tape.
Dur-ina the multiple frequency tests, the output of the control accelerometer was also analyzed on-line and the X-Y plots
.of the test response spectra are included as part of this test report.
The accelerometers were located as follows:
1 ~p "ii-1 Report Nn.
ENvwoNMcpcrAL ACT b8 P
COgg POR ATlON 7
Page
ACCELERO!STER NO.
AXIS SENSING OR:ENTATION LOCATION ~
1 2
Hl H2
. on H3BC Housing Hl H2 V
on top of H3BC housing or on bracket when used
?
8 9
10 ll 12 13 14 15 16 17 18 Hl H2 V
Hl H2 V
Hl H2 "V
Hl K2 V
on SHB housing on end cap of motor on top of handwheel on base of table Control is 418 For tests 1A-9A, 16A-18A, the triaxial group of accelerometers 16, 17 and 18 was reoriented as follows:
(818 remained the control accelercmeter).
0 H< ~
V "Re.4'e, bonzo~ axQ pa~eL Co De motor ceca Cha horn oaten ax& pePtpen&~
Co the, mc~v". ~
Che v~caL ~.
Rcport No.
<o mcZuded pho<oorwpha 148Ol -1 DfVlgKWMt7ETAL,
~ acTON Page 8
Test yoni toring cont> nueo )
AXIS SENSING ORIENTATION ACCELEROMETER NO.
H1 TESTS H~ TESTS V TESTS 16 17 18 V
H~
Hl V
Hl H~
Hl HZ V
During the tests specified in sections 3.5, 3.6, and 3.7
- below, one (1) closed set of contacts of the limit switch and one (1) c1osed set of contacts of the torque switch were indeoendently monitored for contact chatter in excess of one (1) mi11isecond.
H> is We ho~ octal m4 puaQ,cL Co the moto< r~
H< is Che ho~=on~
a+ca pezpenckcuZc~
-o the mo o.". a~
he ve~caL ~.
148ol -1 Report Na.
Rev 1
The r esonance sur vey consisted of a sinusoidal input with peak horizontal or vertical accelerations of 0.75g at fre-quencies from 5 through 60 Hz and back to 5 Hz.
The resonance survey was performed at a sweep rate of 1/2 octave/minute.
The resonance survey was performed both with and without the seismic support bracket using actuator f4.
The input was applied using the AETC Ling A249 electrodynamic exci er as fol 1 ows:
TEST NO.
AXIS OF EXCITATION SEISMIC SUPPORT BRACKET lA 2A 3A 4A 5A 6A V
V H2 H2 Hl Hl No Yes Yes No No Yes
'Re)err
<o Ae ~'ncQcded photographs H>.ia the hocizoMaZ a~ pummel, o ate moCoc a~
H< i.~ the houri on~ axles pMpeiiA~a:o ~he mole~ a~
V m Che ve.i'.cd. axe 14801 -1 Report No.
PAlRONMCNTAL I
ACTOR 'j PQgd 10
3,g uglification Test with Seismic Support Bracket The qualification test with the seismic support bracket consisted of a continuous steady state sinusoidal dwell input with peak horizontal or vertical accelerations of 6.0g ex-cept ~here limited by AETC shaker table capabilities as specified below.
The sinusoidal dwell test was performed at 1/3 octave intervals of frequency from 5.0 through 32 Hz (5.0, 6.3, 8.0, 10.0, 12.5, 16.0, 20.0, 25.0, 32.0) as well as at 35 Hz.
Each dwell was for a duration of fif.een (15) seconds.
This qualification test was performed with the seismic support bracket using actuators 83 and 44.
The input was applied asing the AETC Ling A249 electro-dynamic exciter as follows:
TEST NO.
7A 8A 9A AXIS OF EXC'.TATION*
Hl H2 V
ACTUATOR NO.
The level of input applied was as follows:
'Re.fee Co Ae ~elude pho<ognaph4 H> m the honizo~ axQ panaLZeL W See, mo~ort ~
H< m Che hollo~ axQ penpendicuLa:.
Co Ne mo~ce ~
V ~
4<@ veau at!~
14801-1 aepOrt NO.
ACTCM ll Page
ualification Test with Seismic Suooort Bracket (continued)
FREQUENCY Hz 5.0 6.3 8.0
- 10. 0
- 12. 5
- 16. 0
- 20. 0
- 25. 0
- 32. 0 35.0 INPUT 'LEVEL 1.0 1.5 3.0 5.0 5.5 6.0 6.0 6.0 6.0 6.0 Ropo~ No.
14301-1 ACTCK 12 Page
3.6 Hulti le Fr eouenc Test A biaxial multiple frequency excitation was applied.'he test input was recorded on a 14-channel tape recorder, each track having discrete frequency sine beats recorded at a diff-erent frequency and delay between beats. All frequencies were recorded at maximum levels.
The input was played back through a 14-channel tape recorder.
The outputs of the 14-channels were then combined in a 14-channel mixer which resulted in a multiple frequency output.
The individual mixer channels had gain controls so that the level of each output tape channel passing through the mixer could be controlled.
In this manner, the required test spec-trum was shaped by controlling the level of individual fre-quencies.
Qualification tests, consisting of biaxial periodic pseudo-random excitation were performed.
The test duration for each input was thirty (30) seconds.
The level was such that the Test Response Spec.ra (TRS) from the control acceleraneter computed at Q=10 (5% damping) would envelop the SSE Required
Response
Spectra (RRS) shown in Figure l.
The test response spectra were also analyzed at Q=20 (2.5" damping) and Q~50 (1.0" damping).
Report No.
14801 -1 ACTON
'LROPgMCHYAL 13 Page
Multi le Fre uenc Tes. (continued)
The multiple frequency test was performed with the seismic support bracket using actuator 83.
The input was ap-plied using the AETC hydraulic seismic simulator as follows:
TEST NO.
BIAXIAL DIRECTION OF EXCITATION*
lOA-11A~
12A 13A 14A 15A Hl 5 V
-H2 5 V
H2 5 Y
~ca~< ~o he ~clouded pho ogcapiv H
~s
~he ho'.i-on~ axis pa.",~M Zo the monroe axe H< is Zhc hof~"oi~ ax& pe~pendic~
zo De. mo~oc axi.s V
i.s 4Am v~maL a~
"Shai.c.i. ZubCc ~quasi a4ion ~o.
po~~ No.
14B ENVIAONMCHTAL
-'ACTOR QOR POAATlON 14 Poge
0
3.7 Plant Vibration Aqinq Test The plant vibration aging test consisted of a sinusoidal inout with peak horizont>> nr vertical acceleration of'.75q at fre-quencies from 10 thru 100 Hz and back to 10 Hz.
The olant vibration aging test was performed at a sweep rate of two (2) octaves/minute.
The input was applied for 90 minutes/axis.
The plant vibration aging test was performed with the seismic support bracket using actuator 43.
The input was applied using the AETC Linq. A249 electrodynamic exciter as follows:
TEST NO.
AXIS OF EXCITATION*
16A 17A 18A Hl H2 V
Rejig@
Hi M Hi V
<o We ~~eluded phoCoo~fu.
the ho~oMal'. ~ pancZEeL Co Ae mome exch 4ie hortizoetaL ~ pmpenA~ W the, mo<on. ~
Ae v~cal! axe Report No.
14801 -1 Rev 1
ACTON
]C P096
0
4.0 TEST RESULTS 4.1 Resonance Surve Test Resu1ts The fo11owing resonances were detected during the resonance survey specified in section 3.4 above:
TEST NO.
AXIS OF EXCITATION>>
SEISMIC SUPPORT RESONANCES BRACKET Hz 1A 2A 3A 4A 5A 6A V
HZ H~
H1 H1 No Yes Yes No No Yes None detected None detected 49.0, 58.0 41.0,. 46.0, 58.0 34.0, 41.0, 47.0 56.0
'Ra)m W Ne, ~eluded phoWg~ha H m 4e, hom=o~ pcnaQ,eL 6 6e monroe axis 1
N< M We hcnico~ axQ penpencti~
Co &e. motto.x ~
V ~ Ae vocal ax@
Report No. 14801-1 ACTON
~NO 16 Page
4.2 uglification Test Results with Seismic Support Bracket Ouring the 35 Hz portion of test 7A, {6.0g), the interface gas-ket between the clutch housing and the main housing vibrated out and the three
{3) 3/4" bolts of the seismic support bracket loosened up.
At this time, actuator 84 was replaced with actuator P3.
There was no evidence of mechanical
- damage, deteriora-tion or contact chatter as a result of the qualification test specified in section 3.5 above other than that specified above.
Report No.
14801-1 Rev 1
ACTOH 17 Page
1
4.3 Multi le Fr uenc Test Results There was no evidence of mechanical damage, deterioration or contact chatter as a result of the multiple frequency test specified in section 3e6 above.
14801-1 Report No.
TESTOvO ACT4N 18 Page
4.4 Plant Vibration A in Test Results There was no evidence of mechanical damage, deterioration, or contact chatter as a result of the plant vibration aging test specified in section 3.7 above.
Report No.
Rev 1
19 Page
5.0 TEST EOUlNENT LlST NAHE tlFGR.
HOOEL Si R. tlG.
RhtlGE ACCURACY INV.P CAL.FRY.
I Accelerometer PCB 4343
'302 302A 472607 4726ll0 344770 344703 344781 450710 4729/6 472909 473010 2034 2043 2044 666 667 670 671 672 673 2045 694 2051 2053 2054 2l355 1-8000 llz 1 llz - 5 Kllz 0.25 - 5 KHz 1 llz - 5 Kllz 0 25 llz - 5 Kllz 1 llz - 5 Kllz
+5%
AC307 AC309 AC310 AC318 AC322 AC323 AC329 AC336 AC338 AC367 AC371 AC374 AC375 AC376 AC379 AC380 AC301 AC302 AC383 AC384 AC392 AC395 AC396 AC410 3 months
TEST CQUIPMFtJT LlST
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Accelerometer II Timer Seconds Scope, Storage N
Filter-Dual VTVH.
Sweep Oscillator Audio Generator Vis ic order N
Recorder Tape Recorder X-Y Visicorder SE Tektronix lthaco Dallintine SDY.
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j16, 17, 18 ACCELEROHETER LOCATIONS VERTICAL AXIS ACTUATOR 44 TESTS lA 5 2A ACTUATOR f3 SIHILAR FOR TESTS 9A 5 18A ae
~No
'48O'-'RC~
ACTdS 31 P090
10, 11, 12 1
).a ACCELEROMETER LOCATIONS H2 AXIS ACTUATOR 44 TESTS 3A 5 4A 14801-1 Report No.
ACTON 32 Page
+
Hl AXIS ACTUATOR g4 TESTS 5A, 6A, 7A (ACTUATOR f3 SIMILAR FOR TEST 16A) 14801-1 Report No.
KHVAOHMCNTA3 ACT4Q
~rr3t43 Page 33
-H 5V 1
BIAXIALDIRECTION OF EXCITATION ACTUATOR 03 TESTS 10A>>12A 14801-1 Report Ne.
Pago 34
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-H) 5 VERTICAL BIAXIALDIRECTION OF EXCITATION ACTUATOR g3 TEST.13A 14801-1 Roport No.
acyaa 1
CCATS'CggATCX4 35 Page
H 5 V BIAXIALDIRECTION OF EXCITATIOH ACTUATOR f3 TEST 14A Report No.
14801-l ACTOR 36 Poge
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AC%ON 38 Pago