Wall panels were put into place in the acoustic enclosure. Work is coming along pretty smoothly, no big issues so far.
In other news, the laser should be arriving on site early Monday.
- Gerbig working on clean room by H2 PSL - PSL delivery expected this afternoon is delayed until Monday as freight waits in Seattle - ICC in BSC8 continues - Farewell to RobertL, RolfM, RyanL - Stoneway delivery for EE people - Much mechanical and electrical activity in H2-ITMY test stand area - MichaelR transitioning LVEA to laser hazard at 1650
Betsy B., Andres R, Jeff B. We attached the lower wires to the FM in the Staging Building. All masses are now suspended with no apparent gross problems. There is a small amount of pitch in the Top Mass, which we will work on next week.
The remaining chamber floor and ring sections were brushed although tools remained problematic. As of 2:30 pm, 32 sections had been through first vacuum. The crew will stay in chamber today until the entire upper chamber has been vacuumed so that we can pull the bellows protection and get fibers off the support tubes on Monday.Zack and Randy were able to work on drills a little bit today which is good because the small replacement bearings arrived.
Moved SUS ITMY Sattelite Rack to southwest corner of ISI cleanroom. H2 ISI ITMY field cables were re-routed to move excessive wire bundles out of clean room area. Swapped out cabling for appropriate lengths (GS-13, T240, L4C, and CPS). Ran cabling inside clean room while staying clear of floor. H2 SUS ITMY sattelite amplifiers were swapped out. Modifications to units are: 1.Replace IC551 & IC552 AD797's with OP27's 2.Replace L101, L201, L301, & L401 with 100 ohm resistors 3.Remove C107, C207, C307, & C407 capacitors. 4.Replace R102, R202, R302, & R402 160k resistors with 121k resistors R. McCarthy, F. Clara, J. Garner, D. Stone
We have two failures modes of the interface box, the first is on the geophone channels that is characterised by having a DC offset (~4000 counts which i think is ~1volt) on the channel. The low frequency power spectra is also anomalous. This problem also might be intermittent, as in sometimes goes away when we power cycle. Richard has this board now and hopefully will come up with a diagnostic. the second is in the pressure sensor monitor, some channel slowly (a few seconds) ramp to full voltage, we will pull one of these boxes as soon as the first board gets repaired.
Summary: Magnetic fields from aLIGO electronics were measured in the LVEA test stand racks. Fields from the switching power supplies in the black IO boxes dominated, and were larger than fields from VME crate power supplies, that had produced lines in DARM during iLIGO. I measured magnetic coupling to some of the channels that were working and estimated that the switcher fields were within a factor of 6 of producing features in those particular channels. We may want more of a safety margin than this, so I suggest investigating different power supplies. I had a look at magnetic fields inside of the aLIGO electronics racks that were set up for the test stands holding the ITMY ISI and SUS, and compared the fields to those in iLIGO racks. I checked several sites but discuss 2 of the most important iLIGO magnetic field coupling sites below. The magnetometer was calibrated in-situ using a coil calibrator. Figure 1 compares the magnetic fields in the electronics rack near a test mass controller for aLIGO (ITMY coil driver in test stand racks in the +Y arm of the LVEA) and one for iLIGO (4k ITM controller measured during S6). The 60 Hz fields are significantly greater in the aLIGO setup than in iLIGO. However, this was not due to components in the racks: the fields outside of the test stand racks were about the same as inside and were more than an order of magnitude greater than at typical LVEA sites during science runs because the test stand racks are located near LVEA electrical panels and we are using a lot more current for clean rooms etc. than normal. Otherwise, the spectrum is dominated by broad features from wandering lines produced by the switching power supplies in the black IO expansion chassis discussed below. Figure 2 shows that the magnetic fields are greater around an aLIGO black box IO expansion chassis than they were near an iLIGO VME crate and are dominated by wandering lines. I opened up h2susb478 and used the magnetometer to search for the source. The fields were much greater right at the Synocean 24V input switching power supply. I confirmed that the fields and source were typical by also checking the TCS black IO box. I tried to determine if these fields were deleterious by estimating the coupling of the fields to a few of the channels that were working (OSEM channels). I set up a small coil on the Synocean power supply and generated large 55 Hz and harmonics fields with the coil. I checked that the fields from my dipole coil dropped off with distance about the same way the power supply fields did (ratio of switcher and diagnostic fields varied by less than 3 over a factor of about 5 in distance). Figure 3 shows that 2e-6 T/sqrt(Hz) from my injection coil produced about 1 count/sqrt(Hz) on the channels, and so the 2e-8 T/sqrt(Hz) signal from the power supply would be expected to produce 0.01 counts in the channel. While this value is too low to show up on this channel, it is only low by a factor of 6 or so. Considering that 1) other channels may be more susceptible to magnetic coupling, 2) other Synocean power supplies may be noisier, 3) this power supply was not drawing maximum current, and 4) we had line features in iLIGO DARM that were attributed to the quieter switchers in VME crates (here), we may want to consider other power supplies for the IO boxes. In a closer look at stationary lines, I saw 10 Hz and 0.5 Hz combs. In the analogous locations during iLIGO, 10 Hz and 1 Hz lines were present, not 0.5 Hz. Possibly something is happening every 2 seconds that happened every second in iLIGO electronics. Robert S., Richard M.
The split crew continued. Randy and Zack replaced the conflat on the dome according to M1000355. Kyle, please note for the record that the conflat has been tagged for later inspection. Later in the day, they worked on tooling (aka air drills). Mark, Chris, Scott H. worked in/around chamber with Carolyn as recorder. Thirty sections were brushed which means that only half of the lower chamber body remains "dirty". Air drills again failed at a rate of ~50%. Bubba and I spent some time looking at a couple drills that had the crew worried because of black residue on the teeth of the chuck (although the metal shroud was clean). Zack disassembled the two drills in question so that we could look at the guts and see what was going on. After examination, Bubba and I agreed that the residue was not likely to have come from the interior of the drill. (The most likely source seems to be particulate that is pulled past the chuck by the vacuum. There is also some possibility that the chuck key could be leaving residue behind when it is used to tighten the brush in place.) I asked Zack to use chuck replacements on any drills that are rebuilt from here on out so that we can keep an eye on the situation.
Today while paging through some transfer functions we noticed that the low frequency transfer function from stage 1 actuators to Stage 2 CPS does not go to zero, but goes flat below ~100mHz. This seems like a very strange thing. Last night we took a TF with all of the lockers engaged, 45kgs of extra weight in each corner of the stage 2 keel plate (45*3kgs total extra weight) and with the corner 3 CPS to AA chassis unplugged and shorted. The attached figure shows the these transfer functions below 0.1Hz and above 0.1Hz transfer functions from the night before when the system was free and fully running some things to notice in the plot 1) locking the system down reduces the low frequency signal (~20X) but there is still alot of signal there (coherence is still 1) 2) Disconnecting the CPS controllers reduces the signal much more, reducing the coherence to ~0 3) We tried disconnecting various CPS sensors in both the locked and unlocked state to see if there was any sensor cross talk, with null results Very tentative conclusions, either there is pick up from the actuator or actuator drive cable directly to the cps sensor or electronics or the sensors are actually picking up signal, flexing or motion we aren't sure. Celine, Hugo and Rich
Andres R. Jeff K. & Jeff B.
This morning we released H2 SUS ITMY Quad-2 from its stops. All chains and masses are hanging freely and no gross alignment or general problems from the move were observed. The Reaction chain looked good for pitch and roll. The Main chain required 2 turns of fine pitch adjustment to bring it to rough (bubble level and ruler) level.
I have restored the dust monitor alarm level settings and added directions on how to do so to the h0dustlab, h0dustlvea, h0dustmx, h0dustex, h0dustmy and h0dustey wiki pages. I suspect they were not restored after the power outage.
[Vincent L, Hugo P, Rich M, Celine R]
On Monday, we noticed the following weird reading from the seismometers pods (pressure signals):
Checking at the pods, we were able to check:
At this point, that means that we need 2 T240 and 1 horiz L4C pod replacements.
Randy replaced a conflat on the BSC 8 dome. It will be tagged as such, but it's being noted here for Kyle and future leak testing.
K. Arai, J. Bartlett, B. Bland, J. Garcia, G. Grabeel, D. Ingram, J. Kissel, R. Lane, R. Mittleman, H. Radkins, A. Ramirez, N. Robertson, J. Warner, and a large crowd of spectators We have successfully mated H2 SUS ITMY [[QUAD 02]] (still in its metal configuration) with the H2 ISI ITMY [[BSC-ISI Unit #1]]. A slide show of the afternoon's activity (105 photos -- thanks Koji, Dale, and Norna!!) can be found in the DCC under G1100893. I attach a few highlights here. Excellent work team! Important take-aways: - We've successfully imployed the lifting bars + genie lift system such that we were able to move the QUAD as a whole, without separating the two chains. While rolling under the Mechanical test stand cross beams there was millimeters of clearance, but we did manage to clear it. - We've weighed the QUAD in its current state to be 774 lbs. Note that there are lots of things still missing from that mass budget, including (but not limited to) the stiffening sleeve, upper structure cross braces, and vibration absorbers. - We've successfully employed the "cookie cutters" as designed, and layed out in D1101259, HOWEVER this resulted in the only major hitch in the move. - In our initial pick of the QUAD, we did not pre-assess how little room we'd have once we got under the BSC-ISI. It took a good amount of finagling to allow the genie lift's feet to give us enough play to shove the QUAD as far into the corner as it needed to go given the cookie cutter arrangement. - As we lifted the QUAD up to the BSC-ISI's optical table, we discovered that the genie lift was not holding the QUAD level. This meant the top of the QUAD did not mate flush with the optical table, and made dog-clamping difficult at best. The solution was to dog it as best we could (over 18 clamps -- plenty enough to hold the QUAD in place), but still with a gap on one side, then lower the genie, wedge wrenched on the lower side, and raise the genie again to support the weight of the QUAD. This worked out great, and yielded a flush mate with the optical table such that we could finish up dog clamping. - We've installed all dog clamps as per D0900363, using assorted lengths of 3/8-16 bolts into the optical table. Some of these proved extremely difficult to install given that (unlike in the drawing) there's the gigantic donut of the BSC-ISI's Stage 0 in the way. In some cases, it required a two-man job where one held the clamp by reaching between the gap between Stage 0 and the Optical Table, which the other squeezed as best he could between the QUAD and the inner diameter of Stage 0 with the hex driver (eg. pg 99 of G1100893). Still to-be-done (in roughly chronological order): - Suspend the QUAD, ensure visually that nothing's crazy, lock it back up - Finish QUAD contruction, including (but not limited to) the stiffening sleeve, upper structure cross braces, and vibration absorbers - Remove appropriate ballast mass from BSC-ISI - Float & Balance the BSC-ISI, ensure level is retained, lock it back up - Swap out satellite amplifiers, replace / swap field cables - Re-Cable up the QUAD and BSC-ISI - Turn ON QUAD and BSC-ISI - Ensure / Develop / Test Watchdog interaction between BSC-ISI - Unlock both, B&K hammer everything, test vibration absorber functionality - Start playing again! OH YEAH AND THEN THE FOLD MIRROR.
K. Arai, J. Kissel
We found that all of three processes on H2SUSB478 showed DAQ status of 0x4000 when we came back to the control room after the awesome work of the SUS and SEI team.
This IOP showed the CRC error counts.
- Hitting "DAQ Reload" and restarting H2DC0 did not help the situation.
- We decided to restart the realtime process on the host and this just restored all of the DAQ status back to green.
We don't see any obvious reason other than there was bunch of disconnection of the cables from the QUAD this afternoon.
The chamber cleaning crew was split again today. Thirty-seven sections were brushed in the chamber body. The upper chamber has all been cleaned except for one nozzle. The air drills are experiencing a failure rate of about 50% but since so many drills are prepared work continues apace. (We plan on running all the prepared drills so that we can look for patterns when we do autopsies.)The large replacement bearings arrived from McMaster-Carr. The work on the dome was completed and, after being re-covered with C-3, was moved off the pedestals which are needed at Y-end. The cleanroom was moved to cover the dome in its new location. (We tried to avoid the survey lines.)
Framing of the anteroom and laser room went up today
K. Arai
MEDM screens for SUS AUX have been made. They are available from the sitemap as well as the individual suspension screens.
Details:
1) the master screen for the quad aux screen has been made. This is located as
/opt/rtcds/lho/h2/userapps/release/sus/common/medm/quad/SUS_AUX_QUAD_OVERVIEW.adl
Similarly, the master screen for the triple aux screen has been made.
/opt/rtcds/lho/h2/userapps/release/sus/common/medm/bsfm/SUS_AUX_BSFM_OVERVIEW.adl
These utilize the "macro" technique to let the suspensions share the unified MEDM screen files.
(i.e. $(VAR_NAME) is used in the MEDM, then give VAR_NAME=ACTUAL_NAME as an argument of MEDM)
2) Made "SUS AUX" Overview screen and added to sitemap.adl
This screen is located at
/opt/rtcds/lho/h2/medm/h2susauxb478/master/H2SUSAUXB478_OVERVIEW.adl
3) Added "SUS AUX" button to the QUAD/TRIPLE master screens
/opt/rtcds/lho/h2/userapps/release/sus/common/medm/quad/SUS_CUST_QUAD_OVERVIEW.adl
/opt/rtcds/lho/h2/userapps/release/sus/common/medm/bsfm/SUS_CUST_BSFM_OVERVIEW.adl
Particularly, the BSFM master screen had many broken links to the other screens that had been induced
by the transition from the static screen to the macro-compatible screen. They have been fixed.
First thing this morning, John had a look at the rusty water being blown out of the compressors and agreed that it was the result of condensation due to the heat. He gave the go-ahead for work to begin in-chamber but encouraged the crew to continue to be aware of similar circumstances. Particle counts were taken in chamber (chamber with 2 people standing still, drill with metal shroud with no vacuum, drill with metal shroud with vacuum, drill with metal shroud and vacuum while brushing chamber-right side of operator, left side of operator, drill with metal and Teflon shroud and vacuum while brushing chamber-right side of operator, left side of operator). Then, serious work commenced. The crew split today and spelled each other for breaks and lunch. Twenty-six sections were brushed in the chamber and the work on the dome was started.
[Responding to request during morning INS meeting...] Dust monitor #3 is in the ISI stand cleanroom, #4 is in the SUS stand cleanroom within the LVEA. The scale of the axes in each plot are different. Notes: - At no point did these dust monitors alarm this morning, indicating unacceptable levels. - Dust peaks in ISI and SUS areas do not seem to be correlated, indicating dirty activity particular to that room, not somewhere else in the LVEA. - H0:PEM-LVEA_DST_3_5 has been 0 since yesterday afternoon...should probably be inspected.
I suspect that the alarm level settings for the dust monitors were not restored after the power outage and so they would not have alarmed at any value. I have restored them today.