DOE/NSF Review of U.S. ATLAS /March 2001 WBS 1.1.1 Pixel Overview and WBS 1.1.1.1 Pixel Mechanics M. G. D. Gilchriese Lawrence Berkeley Laboratory.

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Presentation transcript:

DOE/NSF Review of U.S. ATLAS /March 2001 WBS Pixel Overview and WBS Pixel Mechanics M. G. D. Gilchriese Lawrence Berkeley Laboratory

DOE/NSF Review of U.S. ATLAS /March ATLAS Pixel System Semiconductor Tracker(SCT) Transition Radiation Tracker(TRT) Pixel Tracker(PIX)

DOE/NSF Review of U.S. ATLAS /March Overview  Pixel system in ATLAS  Provides critical pattern recognition  Determines ability to find secondary vertices eg. for identifying b-quarks  Part of Level 2 trigger  Countries involved are Canada, Czech Republic, France, Germany, Italy and US.  The US is roughly 20% of the project.

DOE/NSF Review of U.S. ATLAS /March ATLAS Pixel Baseline Three barrel layers Three disk layers Provides  3 his for |  |  2.5 Pixel size is 50x400 , except for innermost barrel layer that is 50x300 

DOE/NSF Review of U.S. ATLAS /March US Pixel Baseline Scope  The US baseline scope corresponds to a 2-hit system.  The innermost(B-layer) and outermost barrel layers are retained.  2x2 disks are retained.  This corresponds to the current concept for the ATLAS initial detector  Upgrade path to full 3-hit system

DOE/NSF Review of U.S. ATLAS /March Pixel Parameters

DOE/NSF Review of U.S. ATLAS /March US Institutions and Management ALB LBL UNM UOK OSU Pixels(Gilchriese) Mechanics(Gilchriese, Anderssen) x x Sensors(Seidel, Hoeferkamp) x x Electronics(Einsweiler, Denes) x x Hybrids(Skubic, Boyd, Gan) x x x x Modules(Garcia-Sciveres, Goozen) x x x x Test Support(Gilchriese) x (Physicist, Engineer ) SUNY Albany, LBL, New Mexico, Oklahoma, Ohio State In addition, off-detector electronics(ReadOut Drivers for both pixels and SCT) are separate project(Wisconsin, Iowa State and LBL).

DOE/NSF Review of U.S. ATLAS /March Hit System - US Deliverables 1  Mechanics( )  Support tube and plugs at end of support tube  Overall pixel support structure(frame)  Disks  Coolant pipes(shared with Europe)  Power and other cables(shared with Europe)  Tooling for final assembly of system(shared with Europe)  Sensors( )  About 20% of production procurement and testing  Electronics( )  About 20% production procurement, 50% of testing of front-end ICs  About 50% production procurement and testing of optical ICs  Common test systems for all collaboration for front-end ICs, modules  Hybrids( )  All flex hybrids  Optical components and hybrids for disk region  Modules( )  Thinning, dicing of FE and die sort  Assemble and test about 25% of modules  Test Support( )  About 20% of support for system tests and beam tests at CERN 1 Assumes release of 600K of management contingency

DOE/NSF Review of U.S. ATLAS /March US Baseline Cost

DOE/NSF Review of U.S. ATLAS /March Management Contingency  Management contingency for pixels in two parts.  High priority(600K)to complete 2-hit system. See below.  Lower priority - to complete 3 hit system.  Note all structural mechanics in baseline, so if more. money found(even from outside US) chance to complete 3-hit system.

DOE/NSF Review of U.S. ATLAS /March US Baseline - Critical Path 4/06 US Baseline schedule established before recent change to LHC/ATLAS schedule. More float?

DOE/NSF Review of U.S. ATLAS /March Mechanics( ) Support Tube Support Frame Disks Services Barrel supporting./cooling structures are European responsibilities. Services and final assembly/installation are shared with US.

DOE/NSF Review of U.S. ATLAS /March Disk Structures  Disks are composed of sectors(8 per disk) that provide mechanical support and cooling and support rings.  Six modules are mounted on each sector.  Sectors are attached to disk support ring at outer radius.  Disk support ring is mounted in support frame.

DOE/NSF Review of U.S. ATLAS /March Baseline Sector Concept  Combined structural support with cooling.  Carbon-carbon faceplates. Front and back faceplates offset in phi to provide full coverage(minimal gaps).  Aluminum coolant tube between faceplates.  Three precision support points to disk ring.  Modules mounted on both sides.

DOE/NSF Review of U.S. ATLAS /March Disks - Status  Two complete mechanical/thermal disks have been made and tested.  In addition, about one dozen prototypes of sectors along baseline design have been made and tested.  Baseline design of sectors is under configuration control.  Final design of support rings is almost complete, but not yet under configuration control. Need to verify mount concept to frame - see next pages.  Requirements and interface documents for sectors exist and Final Design Review completed.  Production Readiness Review for sectors(and corresponding barrel element - staves) scheduled for June 19.  On track to make a preproduction disk(8 sectors + 1 ring) starting in July.  On or ahead of schedule, costs OK so far but still very early - production ahead.

DOE/NSF Review of U.S. ATLAS /March Support Frame Barrel Section Disk Sections Barrel Support Cone

DOE/NSF Review of U.S. ATLAS /March Support Frame Status  Full-size disk portion of frame made and tested. Looks good.  Prototype endcone under construction. Tests complete by July.  Prototype disk ring mounts made, preliminary tests complete.  Final location of disks made by drilling in frame. Fixture to do this under fabrication, prototype ring modified to accept prototype mounts, procedure, including insertion, will be tested by Sept.  Interfaces(to barrel region, services and support tube) now design drivers.

DOE/NSF Review of U.S. ATLAS /March Support Tube SCT TRT 3450mm 3400mm (end-plug face) PP0 Overlap region Z=[750,1070] PP1 In End-Plug Z=3400 Length of service panel Pixel + Pigtails 795mm (Barrel Tube half length) Pixel system and services roll in on support tube Ends of tube are plugged to complete thermal environment

DOE/NSF Review of U.S. ATLAS /March Support Tube Status  Conceptual design phase  Full-scale mockup under construction at LBL  Test insertion and services support schemes  Will fabricate prototype of center section by next year. Extruded Service Rails detector Rails

DOE/NSF Review of U.S. ATLAS /March Services - Inner Detector Region Pigtail PP1 “Type II” 3.2m to PPB2 PPB1 Pixel Volume All Low mass Cables run along the Support Tube and then to PPB2 with breaks as indicated Patch PPF1 Inner Tracker Section To PP3 PP0 Location PPB2 No Longer Used  Power, signal, monitoring signals  Coolant piping  Connections at patch panels(PP#)  Strong coupling to support frame and support tube designs.  At conceptual, early prototype stage. Support tube

DOE/NSF Review of U.S. ATLAS /March C 8C 7C 6C 5C 4C 3C 2C 1CBL 4CBL 3CBL 2CBL PP3 USA 15 Services - Outside Inner Detector  PP2  PP2 -> PP3  PP3 -> underground caverns  Also conceptual, early prototype phase. PP2 region

DOE/NSF Review of U.S. ATLAS /March Services I Z_400.7 Z_ R_190 R_90 100mm 205mm 260mm 50mm 120mm 130mm 50mm 30mm 160mm Bi-Stave Assy 6X7X 370mm End of Pixels+Pigtails Z_1070 Electrical-to-optical transition made here Patch panel 0(pp0) 2c m Optic fibers OSU Optical Hybrid Prototype Support frame Integration of services -cooling, power, signal- is now major design driver for support frame and other mechanical structures

DOE/NSF Review of U.S. ATLAS /March Services - II Hanger Structure Barrel Patch Panel 0 Disk Patch Panel 0 Structure necessary to support services during installation. These slide along rails in support tube Service panels hold cables, pipes and fibers

DOE/NSF Review of U.S. ATLAS /March Services - III Float -Z- Beam pipe Support Arm Service Panels Bulkhead Connectors Bulkhead moves With services Cover plate made in Quarters to pass beam Pipe support wires Double wall beam pipe Beam pipe support collar End sheet fixes rigidly to beam pipe support collar floats in cover plate Floating seal— attached last Auxiliary EMI foil on beam pipe Need to affect both Gas and EMI seal 240 Tube Flange Beampipe support arm Interfaces with flange Not with end cover PP1 region

DOE/NSF Review of U.S. ATLAS /March Cooling  Evaporative C 3 F 8 is baseline.  Sectors tested - test setup below. Substantial headroom to maintain temperature of silicon at or below 0 o C. Capillary(0.030” ID 1.2 m long) Exhaust lines

DOE/NSF Review of U.S. ATLAS /March Cooling Connections  Advanced prototype stage.  Joint US/Europe program with multiple options for joining tubes and connectors.  Brazing, gluing and e-beam welding under study.  Connector types under study and test.  Corrosion of aluminum under radiation in C 3 F 8 studied - not a problem.  Baseline choice for connection to sector(or stave) in time for June PRR.

DOE/NSF Review of U.S. ATLAS /March Cables and Connections  Conceptual framework documented(eg. for ATLAS- wide power supply review this month).  Prototypes built for  module -> PP0 ->PP1  evaluating prototype power supplies(simulate full length)

DOE/NSF Review of U.S. ATLAS /March Final Assembly/Installation  Full “trial assembly” of structures in schedule.  Disk regions assembled at LBNL.  Shipped(as units or pieces) to CERN for integration with barrel. Barrel assembly will be done at CERN.  Conceptual installation sequence in support tube exists.  Still in conceptual design phase but mockup will allow test of some concepts(not all).  Close integration with ongoing overall re- baselining of ATLAS installation plan and access scenarios.

DOE/NSF Review of U.S. ATLAS /March US Mechanics/Services Team  Almost all at LBL or under contract to LBL(Hytec, Inc).  Engineers[Anderssen, Goozen, Hartman, Hoeferkamp(EE - UNM), Miller(Hytec), Miller(Hytec)]  Designers(Taylor, Uken, Hytec team)  Techs(Johnson, McCormack, Weber, Wirth, Witharm)  Shops, special services + students.  Physicists[Gilchriese + Einsweiler/Garcia- Sciveres on services]

DOE/NSF Review of U.S. ATLAS /March Funding Profile - Base Cost

DOE/NSF Review of U.S. ATLAS /March Mechanics -Schedule Flow