To: E614 Collaboration From: Robert Henderson (TRIUMF) Re: Design concept of Cradle/track Date: 30 May 00 Hans Wattlitzer and I have been working on the Cradle/Track concept. In this report I will try to bring the collaboration up to date about the general concept without going into great detail. The concept is NOT finished, hopefully within 2-3 weeks it will be. There are eight postscript files included, they are as follows: W1.EPS - Three sections views of cradle/track/detector. These sections are at: Uptream cradle endcap (left) Central region of cradle and showing a detector (center) Downstream cradle endcap (right) W2.EPS - Section view of cradle/track at Upstream cradle endcap W3.EPS - Section view of cradle/track.detector at Central region of cradle W4.EPS - Zoom of W3.EPS showing region near right cable bundle W5.EPS - Section view of cradle/track at Downstream cradle endcap W6.EPS - Zoom of W5.EPS showing DS endcap near right cable bundle W7.EPS - Same view as W6.EPS but including `plug' and cable tray W8.EPS - Side View of cradle/track in solenoid. Figures W1.EPS thru W7.EPS are from my acad drawings and do NOT include all the details Hans has incorporated in his drawing. I made figure W8.EPS from two drawings Hans made, deleting many deatils. Current Cradle/Track Concept ===================== Going from Guys Stanford's initial concept, I modified it somewhat, the collaboration endorsed the new scheme and we dropped the cradle/track scheme based on arcs. Initially, I had the thick cradle endcaps filling the circular enclosure of the top half. In our meetings, the collaboration realised the thick Al need only be a smaller rectangle and the rest could be light-weight bolt-on extensions. In tals with the design office, they feel this just complicates the whole design, I agree. So the present concept has solid encaps with circular top half, if the weight increase is a problem, they can easily machine down some areas (I'd rather not). Going back to thick endcaps nread the cable trays started me re-thinking that interface, I'll discuss that below. Rolling and Landing -------------------- Hans has been working mainly on the Cradle-Track interface, i.e. how will the cradle roll. Guy's initial hurried concept had rollers to support the cradle, but none to prevent side-to-side motion and `rubbing' or even binding. Plus no details of cradle `landing'. Hans has added a second roller to control side-to-side motion, he's still working on landing scheme. Tension Rods -------------- We considered several ways of doing this, but soon came back to my initial concept. Each tension rod is inserted thru a hole in the DS endcap, passes close to the detectors modules, then screws into a tapped blind hole on the inside face of the US endcap (no gas leak). In principle, all that is required at the DS encap is to screw a nut onto each rod until it contacts the DS endcap, then lock it in pleace with another nut. Unfortunately, this is not failsafe. Someone unclear of the concept might keep tightening the first nut, putting huge forces on the cradle and modules. Therefore, in the present design, a machined `spacer' goes on before the first nut. This spacer has two surfaces, one that contacts the endcap face, the other a step on the tension rod. The spacer will have to be skimmed to the correct spacing when first assembled, but thereafter it prevents over tightening. To gas seal this DS end of the tension rods, a `cap' will cover both rods and o-ring seal to the DS face of the endcap. Vent holes to this capped volume ensure it's flushed. The cover also prevents people undoing the rods by mistake. Gas Outlets ------------ My inital concept had a flange on the encap extension, and a bellows inside connecting to the gas manifold. This has now been simplified. Each outlet will consist of a 0.5" dia, pipe glued into the DS endcap. A simple brass VCO fitting will connect to the manifold. This is simpler and required less space. Hans and I have started working on the manifold support/alignment scheme. Ouside the helium volume, the outputs connect to 0.5" polyflo. Gas Inlets ---------- It is clear to me that the two inlet hose bundles should NOT be incorporated in the cable bundle. If we move the cradle/detector stack to another location (cleanroom say), we do NOT want to have to disconnect all gas inlets and sample lines at the modules (75 hoses). Aslo if in aother location we want to flow gas, it is far more convenient if the inlet hoses are still attached. There are two possible locations for the gas inlet bundles, at the bottom of the cradle or near the cable bundles. After some thought, I decided that near the cable bundle is better. Why? If the hose bundles are at the cradle bottom, the only way to disconnect a chamber is to remove the large cradle bottom-plate, disconnect and cap, then lift out the module. Doing this while under the `track extension cart'. If the hose bundle is near the cable bundle, we have TWO options. The first is the same as discussed above, the second is to lift the module vertically (usual removal technique), but with the inlet hoses still attached. W3.EPS shows, a set of four gas fitting and a 1/4" hose `floating' above the in-situ module. These are a copy of the module gas inlets positioned 820 mm above in-situ location. The hose is same length as the the in-situ, but obviously follows a different path to the gas bundle. The idea is to illustrate that, with the hose bundle near the cable bunbdle, the module can be lifted clear WITH the those hoses attached. Then it is trivial to undo and cap them, without removing the bottom-plate at all. I beleive we should retain the bottom cover plate, this just enhances our options. This scheme would NOT work with the hose bundles at the bottom of the cradle, since where and how would we store the 1 meter of extra hose in the in-situ position. On the subject of gas inlet and sample lines. Robert Opensahw and I have discussed it at length. The sample lines were origionally my idea, but if is unclear if they do anything for us except use up valuable space. If there, we have to figure some way of flushing those sample lines (not trivial). All a smaple line could do is possibly confirm that a helium is leaking into a module, something we should know from perfomance far sooner. Cradle and Track ------------------ For some reason, Willy's drawing to Hans showed the cradle extending beyond the track at both US and DS ends!? I don't understand this! Making the cadle overly long just uses up valuable space during removal and makes it more unwieldy to transport. Also, unless other concerns arise, the DS end of the track should entend almost to the steel. This shortens the length of the `track extension cart' and requires less distance to roll the cart before it can be lifted via crane. The present concept has the cradle 8.4" shorter than the tack on the US end, the track end 4.7" from the steel. At the DS end, the track is only 1" from the steel, so the cradle is 12.1" shorter. The cradle is simply supported from teh rail with pairs of rollers are each `corner' of the cradle. The `landings' would be in the same area. This means the cradle is resting on the rails 7" from the point where the rails are attached to the external supports. I think this is definately close enough. The latest scheme for Z-axis alignment fo the cradle is to view targets from the side of the magnet, getting a direct measure of Z locations. With the cradle the present length, target extensions would need to be attached to the cradle corners, holding targets 4.5" beyond the ends. These extensions could be dowelled and bolted so they can be removed and re-installed easily. The US cradle endcap has two braces (gussets) to the top surface of the longitudional beams. These braces are 10" long, 19.5" high and 1.5" thick. There are no such braces on the DS endcap of the cradle, since we care only about the stiffness of the US endcap and also because they would interfere with the cable bundles. Upstream Cradle Endcap ------------------------- Shown in W2.EPS. Very simple. Has bumpers that will screw in to touch the G10 endcap during initial alignment. They are then locked with lock nuts and hopefully never touched again. On the US face, these four locations will have screw-on covers with an o-ring seal and vent holes to the covered volume. On the Inside face there will be blind holes for manifold US support/alignments etc. There will be a helium inlet pipe glued into this endcap. At the central circular cutout, there will be a `lip' with blind tapped holes and an o-ring groove. The input window assembly will be screwed onto this lip. The lower half of the endcap will be bolted and glued to the longitudional beam and to a 0.5" permanent baseplate. The 3.16" shell comes into contact with the upper circular half of the endcap. Gas seal will be by gasket compressed to say 2 mm final thickness. Downstream Cradle Endcap ---------------------------- Shown in W5.EPS, W6.EPS and W7.EPS. Has four bumpers that will slid thru holes in the endcap and contact the DS G10 ring. On the DS side of the encap, each of the bumpers will attach to a brass pneumatic cylinder (about 2.75" dia bore). These cylinders will be attached and supported from the endcap. Flanges with o-rings will ensure Gas seal and there will be vent holes to these volumes. There will be a helium outlet pipe glued into this endcap. At the central circular cutout, there will be a `lip' with blind tapped holes and an o-ring groove. The output window assembly will be screwed onto this lip. The lower half of the endcap will be bolted and glued to the longitudional beam and to a 0.5" permanent baseplate. The 3.16" shell comes into contact with the upper circular half of the endcap. Gas seal will be by gasket compressed to say 2 mm final thickness. The big difference between the US and DS endcaps is the need to bring the cable and hose bundles out the DS end. I have spent considerable time designing a scheme I hope will be as convenient as possible. Instead of glueing (RTV) the cable bundle into notches in the DS endcap, I have deigned a `pug' that will allow a gasket seal to be used. When trying to seal with a gasket, corners must be avoided. Also, all parts of the gasket need to be compressed at the same time. To accomplish this, I make a curved cutout in the DS encaps (see figure W6.EPS). The bottom edge of the cutout is horizontal, the left edge vertical and of course the corners are rounded. The upper suface surls around the hose bundle area and goes to the outer rim again. The upper sufaces are at 10 degrees from the horizontal. Why? The idea is that the `plug' piece will hav a matching contour, but seperated by 2 mm, the final compression thickness. If the plug is inserted into the notch along a 5 degree line, then all surfaces come into contact and are compressed at the same time. The plug has a large machined cutout into which the cable bundle is permantently glued. Thus the plug becomes part of the cable bundle. The thinnest part of this aluminium plug at the outer wall, here it is 0.25" thick. The figure shows three brackets attached to the plug, two for bolts and one for a pin. There will probably actually be five, the two bolts being replicated on the iside face of the plug to avoid `twisting'. There are three (or five) matching brackets attached to the endcap, two (or four) threaded and one with a hole for the pin. This scheme should allow relatively easy removal and re-installation of the cable bundle without the need for RTV. The plug would be as thick as the endcap (2-3 inches), it's outer surface would be similar to that of the endcap, with tapped holes for the outer shell and its gasket. In principle the only leak point (except for within the cable bundle) is the point where shell gasket and plug gasket meet. If the plug gasket protrudes a little at that point, I believe a seal will occur. If not, this one location may need a bead of RTV which would be easy to remove. Hans is studying the notch/plug concept, but doesn't see a problem. Central region -------------- This region is shown in figures W3.EPS and W4.EPS. I have used just about all the available sapce for the hose bundle and cable bundle. The hose bundle has 3.2 mm thick wall and is shown with thirty-two 0.25" dia. hoses. If we have sample lines, we need: 56 + 19 + 4(spare) = 79 lines. This is 40 for each hose bundle. If we drop the sample lines, we need (56+4)/2=30 for each hose bundle. I could make the hose bundle bigger at the expense of the cable bundle. It is fine if we drop the sample lines. The cable bunbdle is shown with fifty-one 8.34 mm cables, that represent SHV and LV cables. We need 56+4(spare)=60 SHV and 38+4(spere)=42 LV cables. Thats 102 total, 51 for each cable bundle. Grant and I considered the idea of having our mini-coax cables put in a weave similar to that on the VTX chamber. This greatly reduces the chance of dmaaging the coax and makes it far easier to attach the connectors to the ends. I did some measurements and found for the 17-way ribbon of the VTX chamber, this weave increases the cable area by a factor of 2.26. For out larger coax and bundles of eight, I estiamte the same weve would cause an area increase of 1.6 for us. In talking to the company, Grant found that they can also bond the mini-coax together, this option causes little or no increase in area. Each ribbon effectievely becomes a 10 mm wide by 1.25 mm thick rectangle, with an area of 12.5 mm2. In the figures I show 321 bonded 8-way cable ribbons, each occupying an area of 15.6 mm2, 25% more than true cross section. Each fully instrumented detector layer requires 10 ribbons. If only the central 48 channels are instrumented, 6 ribbons are required. If we fully instrument all the layers in the dense stacks and only the central regions of the target, we need 568/2=283 ribbons in each cable bundle, So the 321 shown represents 13% spares. There is still some space in the cable tray, but we also need pulser cables (10 per tray) and 8-signal temperature readout cables (10 per tray). My view is that the cable tray should be no smaller than shown. Clearly, the alternative of a weave on the mini-coax would be a risky choise. Between cradle encaps, I show a bar extension to the beam `lips'. Hans had the same idea, except he `hogged out' a groove for the attachment screws. These extensions would be permanently bolted and glued to the beams. The outer edge of the extension is angled and has blind tapped holes for the shell and its gasket. This provides the helium seal. Hans and I are considering the possibility of making the shell in two pieces, but I won't report on that yet