ML18018A812
| ML18018A812 | |
| Person / Time | |
|---|---|
| Site: | Harris  |
| Issue date: | 03/13/1979 |
| From: | Casaubon M, Esposito B, Tolf M ACTON ENVIRONMENTAL TESTING CORP. |
| To: | |
| Shared Package | |
| ML18018A805 | List: |
| References | |
| 14331-3, 14331-3-R01, 14331-3-R1, NUDOCS 8310130271 | |
| Download: ML18018A812 (17) | |
Text
Tes Report No. 14331-3 REVISION 1 - 3/13/79 No. of Pages Hepopt of Test on SEISMIC VIBRATION TESTING OF ONE (1) LINITORQUE SMB-000/HOBC ACTUATOR MITH SEISMIC ADAPTOR FOR LIHITOROUE CORPORATION UNDER PURCHASE, ORDER NO. TL-413 ENVlRONMENTAL ACTQN TEST1NG CORfssORATtON January 31, 1979 Date By igrec Date BE/hmf Prepared B.Esposito Checked
) Approved M.Casaoboo
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N.L.Tolf 830',9 83foisoav, 0500040o I
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6
REVISION RECORD DATE 1/31/79 REVISION NUMBER PAGE PARAGRAPH NUMBER NUMBER
>>>>>>>>>>>>>>>>>>FIRST ISSUE>>
'CHANGES OR ADDITIONS APPROVED BY 3/13/79 1.0 3.2 3.4 Footnote 3.5 Footnote Footnote 4.2(4B) 4.2(78) 4.2(12B) 4.3(138)
Changed
~Ada tor to Bracket Added last sentence Changed above to below Change 440 to 460 Added last column to table Typographical correction Added second foot-note Added last column to table.
Typographical cor-rections Added second foot-note Added footnote Changed valve to actvator Added last sentence Changed valve to anteater Reworded next to las last sentence.
Added last sentence Added word "cover" ACTaN Report No; Page 1 of 2
REVISION RECORD DATE
'REVISION NUMBER PAGE PARAGRAPH NUMBER NUMBER CHANGES OR ADDITIONS APPROVED BY 0
m~wmuwmwmFIRST ISSUEwm n
a 3/13/79 4.3(14B) 4.3(15B)
Added word "switch" Added word "switch" Added last sentence ACTON Report No; 1'4331-3 Page 2
Administrative Gata T
vibration testing.
Limitorque Corporation Lynchburg, Virginia SHB-000/HOBC Limitorque P. 0.
No. TL-413 One (1)
Unclassified September Il, 1978 C.Pilotte Returned to Limitorque Corporation.
Refer to result section herein.
14331-3 Re part Na.
Page 1
ACTdN
1.0 TEST ITEM One (1) Limitorque SMB-000/HOBC Actuator with a Seismic Bracket was submitted bv Limitorque Corporation for seismic vibration testing at Acton Environmental Testing Corporation (AETC).
Note:
Actuator was'lso subjected to additional seismic excitation as documented in Acton Report'f14331-2.
The purpose of this test was to subject the actuator speci-fied in section 1.0 above to the seismic vibration test specified in section 3.0 below to determine its ability to withstand such vibration without evidence of mechanical damage, deterioration, loss of its ability to operate properly, or contact chatter in excess. of one (1) millisecond.
3.0 TEST PROCEDURES This test was performed under the direction of Mr. Paul Young of Limitorque Corporation.
The actuator was bolted to a test fixture supplied by Limitorque.
The test fixture was then securely attached to the single-axis table of the AETC seismic test facility.
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 was not operated.
Du~ing the sinusoidal dwell test specified in section 3.5 below, the actuator was cycled open and closed at least once per dwell.
460 VAC 3g power was supplied to the actuator.
3.3 Test Monitorina The actuator was visually monitored for any evidence of 14331-3 Report No.
Rev 1
ACToN Page 2
mechanical damage, deterioration or loss of its ability to operate properly.
The actuator was monitored with triaxial groups of accel-erometers by AETC personnel to determine its mechanical response during the resonance survey and sinusoidal dwell test specified in sections 3.4 and 3.5 below.
Data from these accelerometers through appropriate signal condition-ing was recorded on visicorder recording paper included with this report.
The eighteen (18) monitoring accelero-meters and one (1) control accelerometer were mounted as
. follows:
ACCELEROMETER AXIS SENSING NO.
ORI ENTATION*
LOCATION Hl H2 V
Triaxial on end of motor Hl Triaxial on SMB-000 Housing H2
~
at mounting flange V
10ll 12 13 14 15 16 17 18 Hl H2 V
Hl H2 V
Hl H2 V
Hl H2 V
Triaxial on HOBC mounting adaptor Triaxial on base of test fixture, control is il2 Triaxial on top corner of actuator housing Triaxial on gear frame of geared switch Hl is the horizontal axis parallel to the motor axis.
H2 is the horizontal axis perpendicular to the motor axis V
is the vertical axis Report No.
143313 Rev 1
ACT O N Page 3
One (1) normally closed (N/C) set o.f contacts..of the limit s~~tch and one 0 ). N/C set of contacts of the torque switch were monitored for contact chatter in excess of one (1) millisecond.
.4
~R The resonance survey consisted of a sinusoidal input with peak horizontal or vertical accelerations of 0.5g.
The resonance survey was conducted at a
sweep rate of 6 seconds/
Hz (1 octave/minute for Tests 58, 6B 5 BB).
The resonance surveys were performed as follows:
TEST TEST NO.
AXIS OF EXCITATION FRE UENCY RANGE Hz TABLE~*
1B V
1-60-1 1
2B 3B 1-50-1 1-50-1 5B V
5-36 2
6B H
1 5-36 2
H2 5-36 3.5 Sinusoidal Owell Test The sinusoidal dwell test consisted of a continuous steady state sinusoidal input.
The sinusoidal dwell test was to be performed at the resonant frequencies found during the resonance survey (only those below 33 Hz) specified in section 3.4 above.
If no resonances were detected, then testing was to be performed at 33 Hz.
Each input at each test level was for a duration of thirty (30} seconds.
The input was applied as follows:
14331-3 Report No.
Rev 1
Hl is the horizontal axis parallel to the motor axis H2 is the horizontal axis perpendicular to the motor axis V
is the vertical axis.
1 Single Axis Hydraulic 2
Ling A-249 Magnetic ACTON Page 4
/
~
I ~
TEST NO.
AXIS OF TEST EXCITATION>>
LEVEL G TEST TEST FRE
. Hz TABLE">>
4B 7B 9B 10B llB 12B V
3 4 5,6 33 Hl 3,4,5,6 33 1
3,4,5,6 33 1
V 7 8 9 10 11 12 33 2
Hl 7,8,9,10,11,12 33 2
H2 7,8,9 33 2
3.6 Sine C clin Test The sine cycling test consisted of a sinusoidal input cycling from 10 to 100 Hz and back to 10 Hz, at a sweep rate of two (2) octaves/minute.
The sine cycling test was performed for a period of ninety (90) minutes/axis.
The vertical or horizontal input was 0.025" DA from 10-24 Hz and 0.75g peak from 24-100 Hz.
The input was ap-plied as fo11ows:
TEST NO.
AXIS OF EXCITATION*
13B H2 14B 15B Rcport No. 1 Rev 1
Hl is the horizontal axis parallel to the moto~ axis H2 is the horizontaI axis perpendicular to the motor axis V
is the vertical axis Single Axis Hydraulic 2
Ling A-249 Magnetic ACTQN 5
Page
~wi Zlh4 4
m>>l
~
~ e
- 4. 0 TEST RESULTS 4.1 Resonance Surve Test Results TEST 18 - Resonance was detected on the motor end cap at 104>> Hz.
TEST 2B - Resonance was detected at 70>> Hz on motor end cap
%B 000 actuator housing and SHB-000 housing at mounting flange.
TEST 3B - Resonance was detected at 46 Hz on gear frame of
~gear imit switch at 74>>
Hz at motor end cap and actuator housing.
TEST 58 - No resonances were detected.
TEST 68 - No resonances were detected TEST 88 - No resonances were detected 4.2 Sinusoidal Dwell Test Results TEST 4B - The actuator operated correctly.
The torque switch chattered at each test level.
Torque switch was defective be-fore testing.
Between TEST 6B and 7B, the housing of the limit gear switch was found to be loose and was retightened.
TEST 7B - The actuator was operated at each level and the torque switch chattered at each test level.
At the 6g level, a shift in response was detected at the motor end housing and actuator housing.
The mounting bolts between the motor and actuator were found to be loose and it seemed as if local yielding had occured.
The bolts were removed.
The holes in the actuator were recapped and new bolts, were installed.
TEST 9B - The actuator was operated at each level.
The torque switch chattered at 4g's, 59's and 6g's.
Mhen trying to re-move the unit from the test fixture, the bolt threads holding the test item to the fixture were found to have yielded.
The bolts were removed and replaced with new ones.
Harmonics not within frequency range of interest.
Report No.
14331 3
Rev 1
E?CVlRONNBIBNTAL ACTOR Page 6
a
~
Ce ~
e 7 4.3 TEST 108 - The a'ctuator-was operated at'each teYt level.
The torque switch chattered at 7g's, gg's, gg's, 10g's, llg's and 12g's.
TEST 118 - The actuator was operated at each test level.
The torque switch chattered at 7g's, gg's, gg's..10g's, llg's and 12g's.
Following ccmpletion of the 12g run, the coupling adaptor was found to be fractured in the same manner that previous couplings had fractured.
The coupling adaptor was replaced.
TEST 128 - The actuator was operated at each test level.
Xfter fsrst'attelapt at gg's, one of the finger basis of the gear limit switch fractured shorting input power.
The finger base was replaced and the test continued.
This necessitated moving accelerometers 17, 18 and 19 from the previous loca-tion to the thin metallic gear limit frame cover.
The actuator was operated manually by the representative from Limitorque after testing in each axis was completed.
Sine c clin Tes Results TEST 138-The actuator was cycled every 15 minutes and resonances were found as follows:
Resonances were detected on the gear frame cover of the gear limit switch between 48 and 90 Hz.
The SHB-000 housing at the mounting flange and the motor end cap and actuator housing resonanted at 75 Hz.
No chatter occured during the cycling.
TEST 148 - Resonance was detected at 65 Hz of the motor end cap, actuato~
housing and SMB-000 housing at the mounting flange.
Handwheel recorded at 65 Mz.
No switch chatter occured during the cycling.
TEST 158 - No resonance below 100 Hz was detected.
No switch chatter occured.
The actuator was operated manually by the representative from Limitorque after testing in each axis was completed.
Relgort No.
14331-3 Rev 1
ACTOk Page 7
TEST EOIjiPl'lEtlT LIST NAIIE Exc i ter A)))pl i fier llydraulic Actuator Con tro1 Ier Cha tt r Honi tor Power Supply Rack HFGR Ling L ing HTS tla trix PCB 202D 3IO 299 HOOEL SER.rlo.
A249 70 PP I20/150 56 204. 63S 443. I15 RAtlGE ACCURACY lNV 9 CAL.FREIL
'E317 1 month.
PE367 6 months Detection:10
& 100 usec 22 VDC 12 HAOC 12 channel y2r tl/A PE370 6 months I
PE379 6 months 30,000:-'orce 1" P/P disp.
t5%
5 - 5 Kllz
+2%
OC - 300 llz, 25K force lbs.
+2.
F 25" DA max.
~5" A OC - 2000 Ilz
~lX Power S<<pply Amp 1 iiier PCB 483H23 289 12 channel Xl
& X5 gain filter freq.
50 Ilz N/A PE385 6 months Power S<<pply VIsco) )Ier Visicorder Visicorder Tin)er Secnnds Strobotac Sweep Oscillator Scope,Storage Power Supply Power Sullply Deca)IU Ampl.
PCO lloneywell Iloneywell Iioney))e 1 1 SE GRC SDY Tektronix Trygnn Bubr Glen 483A02 9060 36I 8687 906 1508 560 153 IA 9-5235 I6'I715R 105 F408 624 SO-104-5 21n 564-11582 IIR60-5A 27979 506/16 322
<22VOC current 4 HA 6 channel DC-2 Kllz 12 channel DC-2 KNz 12 channel 12 channel-metric 0-60 seconds l.rpm 0-25K rpm 0.005 llz -50 Kllz OC to 10 tlllz 60 volts 5 amps
<15 VOC, 1
ADC 3 to 100 Kllz 40db/x100 tl/A PE397 6 months ildb RE301 3 months ildb RE332
~1db RE347
+0. 1 sec FH3II1
+li PP322 3 months 3 months 6 months 6 months tlat 50315 6 months
+3%
OS309
.OIL PD328 3 months 6 months 0.5X PD372 6 months
+I'I AH315 6 months
0
IIAHE HFC) R.
NOBEL TEST E()UIPllENT LIST SER. HO.
RANCiE ACCURACY INV.S CAL.FREO.
Acce1 erome ter PCO BK 302A 4344 302A 667 668 671 673 2845 694 696 697 2851 2852 447575 2856 1772 1774 1780 178I 1805 18 I I 0.25 Hz - 5 KHz 1
Hz - 5 KHz 0.25 Hz - 5 KHz 1
Hz - 5 KHz 0.25 - 5 KHz I Hz -
5 KHz
+5%
AC376 3
AC377 "
AC380 "
AC382 "
AC383 "
AC384 "
AC386 "
AC387 "
AC392 "
AC394 "
AC395 "
'AC41,4 "
l AC415 "
AC417 "
AC423 "
AC424 "
AC425 "
AC428 "
months
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