ATLAS Upgrade ID Barrel: Services around ‘outer cylinder’ TJF 24.02.09 updated 12.03.09 According to the drawing ‘Preparation outer cylinder volume reservation’

Slides:



Advertisements
Similar presentations
Endcap assembly update C Buttar UK-SCT-MB RAL 2 nd Sept 04.
Advertisements

WP7 ATLAS ID Barrel End Services T.J.FRASER UCL Aim: Using experience gained from work on the current ATLAS SCT Barrel, attempt an improved design and.
ATLAS UPGRADE BARREL END SERVICES – Work on trying to reduce mass of cooling in R/PHI TJ Fraser UCL Assuming cooling pipes have to be directed.
Preparation for ATLAS SCT/ID Endcap Completion at CERN Jo Pater Manchester, 4 January 2006.
Barrel services minimum space allocation in Z ‘Strawman’ layout and Spider… layout WARM and COLD GAP versions Services envelope in Z: In order to reserve.
A.Nichols CLRC1 SCT HEX PRR ( ) Layout & Installation of Barrel off-detector HEX circuits From barrel cooling loop to PPB1 l Barrel Hex is a plain.
HFT Geometry Considerations F.Videbæk BNL. Introduction This presentation is meant to be a living document, updated as more and better information becomes.
Comparison of cooling services at barrel end Description SCT Barrel Upgrade ID barrel one end one end Total number of staves/rows 176 Staves/rows serviced.
SLHC - WP7 Barrel UPDATE on LAYOUT OF SERVICES AT THE BARREL ENDS OPTO PCBS: Sketches describe options after discussion with Tony Weidberg ( ) Preference.
CMS ECAL End Cap EDR Meeting CERN 28 Nov. to 29 Nov 2000 A.B.Lodge - RAL 1 ECAL End Cap CMS ECAL End Cap Engineering Design Review. EDR meeting held 28.
ATLAS SLHC UPGRADE ENGINEERING – LIST OF DECISIONS which will affect the design of auxiliary systems layout and routing BASIC LAYOUT FOR BARREL and WHEELS.
Update on alignment kit and stave 250 frame M.Gibson (RAL) 1.
SLHC Pixel Layout Studies S. Dardin, M. Garcia-Sciveres, M. Gilchriese, N. Hartman LBNL November 4, 2008.
26 April 2013 Immanuel Gfall (HEPHY Vienna) Belle II SVD Overview.
HEP GROUP MEETING work on the ATLAS UPGRADE T.J.Fraser.
M.Oriunno, SLAC Stave cable and module options. M.Oriunno, SLAC Background - module The IBL electrical unit for data output is a single chip The use of.
V. Cindro, Jožef Stefan Institute, Ljubljana, Slovenia DAQ, DCS, Power Supply and Cables Review CERN, March Electrical PP1 Basic features Electrical.
Aug/16/05 Su DongSiD Vertexing: Snowmass 05 SiD trk+vtx1 SiD VXD Geometry Update Su Dong SLAC.
ATLAS Tracker Upgrade - Services at Barrel Ends: Scenario where services are routed through existing services channels on cryostat shown on the next 3.
Phase 1 FPIX cooling tubes routing in HC Kirk Arndt - Purdue124 April 2012.
18 July 2006A.Ciocio -SCTSG1 SCT Services Installation ID week full report (July 4) SCT Cables Web page
Santa Cruz Meeting August 12 th 2008 Layout options & Schedule Issues David Lissauer 8/12/2008 1David Lissuaer, Santa Cruz Meeting.
ATLAS Pixel Detector September 2003 Services E. Anderssen LBNL Service Connectivity from Module to PP1b Eric Anderssen LBNL Pixel Services Meeting, CERN.
B-layer integration with beam-pipe and services ATLAS B-layer upgrade E. Anderssen A. Catinaccio.
Pixel Upgrade Phase I CMS Upgrade Week 27. April 2010 R. Horisberger, PSI.
Chiho Wang Duke University 1 TRT Barrel integration Status / Schedule Chiho Wang.
November 04 Jason Tarrant CCLRC1 SCT EC Interconnects l Progress of SCT EC Interconnects »Services (Required for Disc Insertion 2004 / Integration 2005)
PMG Meeting February 2000 A Split Central Silicon Tracker W. E. Cooper on Behalf of the D0 Silicon Group 3 February 2000.
SCT Barrel 6 Support Bearing A full-scale model of the barrel 6 support bearing has been machined at UCL (drawing G.Barbier ) It was tried out on both.
S Temple CLRC1 End-cap Mechanics FDR Power Tapes and Optical Fibres Steve Temple, RAL 1 November 2001.
Tilt angles reloaded, and status of some other things.
1 Outer Barrel, Phase 2 Mech Review 26 Aug 2013, indico: Antti Onnela, CERN Tracker Phase 2 Mechanics Review, 26 August 2013 Status of the Outer.
DCS meeting27.Sep.2002 Serguei Zelepoukine (IHEP, Protvino) Contents: 1. Front-end electronics: problems & solutions. 2. DCS cabling outside the ECAL detector.
Stave 130 Geometry Peter Sutcliffe ATLAS Strips WP4 Meeting 26 th March 14 Liverpool.
G.Barber/Peter Cooke: Mechanical Design Update Imperial 22 July Mechanical Update for Tracker workshop Contents:- New Station Layout Light Guide.
End-of-stave region. 2 Space Z-dimension is critical –Keep gap small (might help getting rid of stubs) Edge of last barrel silicon (at corner) is 1277.
Alpine pixel layout Integration progress Teddy Todorov For the ATLAS-LAPP group AUW Integration meeting 20/11/2012.
G.Barber Mice Tracker Mechanical Progress Tracker Mechanical Progress Contents:- Station Space Frame Station Layout Light Guide Map Connectors Patch.
Stave 130 Envelope Peter Sutcliffe Strip Mechanics 20 th February Lancaster.
TC Straw man for ATLAS ID for SLHC This layout is a result of the discussions in the GENOA ID upgrade workshop. Aim is to evolve this to include list of.
EOS and type I Prototype Service Modules Mike Dawson (Oxford), Rob Gabrielczyk (RAL), John Noviss (RAL) 19 th January 2015 ATLAS Upgrade Activities, Oxford.
C.BAULT November 9 th  LAYOUT STRAWMAN 07V13 Vs STRAWMAN 07V14  SERVICES AND STRUCTURES INVENTORY  ENVELOPE SERVICES  BARREL SERVICES ROUTING.
D. Greenfield CLRC1 End-cap Mechanics FDR Baseline Design Overview Debbie Greenfield, RAL 1 November 2001.
Chiho Wang ATLAS TRT Duke University CERN, Sep Barrel integration status.
Comments on Engineering talk by A. Catinaccio at Inner Tracker Engineering Meeting CERN ) Fixed length barrel layout drawing by C. Bault (Strawman.
IBL CO 2 cooling flexible transfer integration into IDEP 24 July 2013 Jan Godlewski, Bart Verlaat, Siegfried Wenig, Nicolas Massol, Tomasz Blaszczyk 1.
1 PST Heater Panel Design The PST heater panels are internally redundant resistive circuits printed onto a Kapton sheet with an aluminum backing. They.
Baby MIND Scintillator modules 11 November 2015 Revision E. Noah.
ATLAS ID Services Mock Up - Proposal Presented by Ian Wilmut at DESY, update from John Hill 4th May, 20101ATLAS Upgrade - RAL.
EC: 7 DISK concept Preliminary considerations
Straw man layout for ATLAS ID for SLHC
ATLAS Internal ID Service Integration
Micro Vertex Detector of PANDA Status of Strip BARREL and DISC
Service channels between Tracker and PP1
Integration and Services RE3/1 and RE4/1
Service channels between Tracker and PP1
Update of MVD services and requests
- STT LAYOUT - SECTOR F SECTOR A SECTOR B SECTOR E SECTOR D SECTOR C
Services – First Considerations Sigi Wenig / Nicolas Massol ATLAS Tracker Upgrade Workshop Valencia December 2007 Existing services (in cryostat.
Micro Vertex Detector of PANDA Strip Detector
WP9 ITS Mechanics and Cooling
Additional muon stations for the Upgrade of the Elevator Regions in the ATLAS Muon Spectrometer. Integration issues Denis Diyakov, Alexander Seletskiy,
Services Layout – Update
Chamber Design and Integration RE3/1 and RE4/1
First of all we will remind some numbers:
BARREL 3 FIBRE ROUTE ORDER and HARNESS INSTALLATION ORDER]
Barrel stave allocation on the PP0 exhaust fitting
BCM Overview Placement such that system is sensitive to all types of beam accidents. => 2 independent subsystems Halo losses inside the Pixel volume ie.
Inner DET. Integration Inner detector envelope Radial clearances.
Presentation transcript:

ATLAS Upgrade ID Barrel: Services around ‘outer cylinder’ TJF updated According to the drawing ‘Preparation outer cylinder volume reservation’ (C.Bault ), the inner surface of the outer cylinder is at R1033. Given this radius, it is possible to accommodate a continuous layer of cooling pipes from the SCT barrel with unmanifolded alternating exhaust and input pipes or grouped exhaust/input pipes in a single layer IF the number of staves is still no more than the ‘original’ 28, 36, 44, 56 and 72 ie 236 (total for one side, with each stave having one input and one output pipe. Although cooling pipes in this layout would not occupy more than 10mm in R, the structure/s that support them and protect them from being bashed during Installation (eg a SERVICES MODULE) would have to be substantial and probably take up an additional 20mm in R without including possible insulation. If power cables are used (rather than power tapes), it is possible that they could fit into another 10mm envelope in R, if evenly spaced and not bunched. The space envelope allowed for on the drawing between the inner surface of the ‘outer cylinder’ is 63mm (R1033 – R970). This is insufficient for the combination of services from barrel, pixel discs 1-3 and end-cap discs 4-8. IF SERVICES MODULES WERE USED, HOW WOULD THEY BE INSTALLED? 1

SERVICES MODULES containing cooling pipes, power and opto cables or Optofibres and DCS cables – how are they installed? Step A REAL ID BARREL with staves Outer cylinder Services jig: Barrel end + outer cylinder section. Services modules separate ends of services with connectors TJF ID (IT) barrel in cleanroom ID Barrel JIG in same cleanroom or adjacent, visible area 2

SERVICES MODULES – how are they installed? Step B REAL BARREL with staves Outer cylinder Services jig: Barrel end + outer cylinder section. Services modules After fitting on jig (pipe bending etc) and securing in services module shell, remove first module from jig……. 3

SERVICES MODULES – how are they installed? Step C REAL BARREL with staves Outer cylinder Services jig: Barrel end + outer cylinder section. Services modules then fit to outer cylinder and connect up cables and pipes, except for cables which may overlap those of the adjacent services module. 4

SERVICES MODULES – how are they installed? Step D REAL BARREL with staves Outer cylinder Services jig: Barrel end + outer cylinder section. new services module Next, fit a new services module adjacent to the second services module to be fitted on the real barrel….. 5

SERVICES MODULES – how are they installed? Step E REAL BARREL with staves Outer cylinder Services jig: Barrel end + outer cylinder section. new services module Make sure the services from adjacent modules fit, then remove the module to be installed on the real barrel and fit. 6

IS THIS PROCESS USING SERVICES MODULES FEASIBLE? Each services module contains a few of each type of services, some rigid and formed such as cooling pipes and some very fragile such as readout micro cables or fibres. The filled services module would be an unwieldy and heavy object to move about with metal edges a hazard to thin cables. It could also bend and twist over its length. There would be services sets with ends of different lengths – very difficult to handle, first when assembling on a jig and then when installing and connecting, even if only transporting from one part of the cleanroom to another. Some services would have to be embedded under others when packing the services module so that inspection would be difficult if such a cable or pipe failed during testing in situ after connection. Long pipe lengths inside the Services Module and extending to end barrel connections would certainly place stress on the barrel staves and would thus require substantial bracketry on the barrel end to take the stress off the stave structure. Power cables inside sleeving would place even more stress on barrel end connectors and the stave. How strong does the stave with integral connectors have to be at the barrel end? Very! As we observed on the SCT barrel, a ‘spider’ of 5 or 6 cooling exhaust pipes, even with bellows to allow flexibility, was difficult to connect up to the barrel. In the end bellows could not be used and each exhaust pipe was connected up separately as were the input pipes. A 32 way layout in phi would mean that Services Modules would take up more space if they are in the form of channels or boxes with ‘lids’. 7

WHAT TO DO NEXT? Assume all new services from ID out to PP2 but probably best to also assume same or very similar position in phi to old services ie based around 45 degs for cooling with readout either side of this and power cables spaced approx. evenly in quadrants allowing space for cooling and (im)possibly big opto boards. Assume a SINGLE baseline LAYOUT for ID which may well change many times! A 32 way layout still means there would be more than 7 staves served by one Services Module which is a lot, probably 6 too many! POSSIBLE SOLUTIONS: Connect up each type of service separately, finishing and testing one type before starting another. Bunch small sets of the same type which could be packed in a small ‘module’ or channel with others. Cooling could be bunched but not packed and could occupy dedicated space envelopes without intertwining with cables. CONCLUSION: Probably unfeasible as an ‘all services module’ given only limited access: handling and connecting a bunch of services all of one type is difficult enough without combining several types. Cooling pipes with connectors would be very difficult to control when in a mixed bunch and would obstruct access to other connectors. The ID barrel would have to be rotated for each SM installation. 8

MAPPING for BARREL services based on the following layout for ONE end: ACTIVE TOTAL COOLING COOLING POWER READOUT DCS LAYER R STAVES OUTPUT INPUT CABLES ORDER R x 2 28 x 2 bunch 5th R x 2 36 x2 bunch 4th R 600 R x 2 56 x 2 bunch 2nd R x 2 72 x 2 bunch 1st x 2 44 x 2 bunch 3rd Using the only known ‘baseline’ dimensions and stave numbers 9

MAPPING for BARREL services based on the following layout for ONE end: ONE QUADRANT eg side A, QUADRANT A1 with cooling centred on 45 degs. POWER CABLES: one stave, (half length of barrel) in one sleeved bunch. 59 sleeved bunches from one quadrant, going to 20 ‘power services modules’ arranged in 4 sets of 5 either side of COOLING centred on 45 degs and READOUT centred on 22.5 degs READOUT CABLES or FIBRES: one stave, (half length of barrel) in one sleeved bunch. 59 sleeved bunches from one quadrant, going to 4 ‘R/O services modules’ arranged in 2 sets of 30 either side of COOLING centres on 22.5 degs. NB this is assuming ‘opto’ board is mounted somewhere on the stave, rather than being remote from the detector. IF remote then distribution of cables will need to be spaced out rather than bunched. OUTPUT COOLING: one stave, (half length of barrel), one pipe with no manifolding. ie 59 pipes directed to 2 layered bunch centred at 45 degs INPUT COOLING: one stave, (half length of barrel), one pipe with no manifolding. ie 59 pipes directed to 2 layered bunch centred at 45 degs either side of output cooling 10

POWER and DCS cables READOUT cables or fibres COOLING output COOLING input spare space reserved for rails etc Services fan-in to main pathways from area of octant, all layers via the shortest possible route BARREL MAPPING 11