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Low mass carbon based support structures for the HL-LHC ATLAS pixel forward disks R. Bates* a , C. Buttar a , I. Bonad a , F. McEwan a , L. Cunningham a , S. Canfer b , C. Lockett b , J. Pater c , R. Thompson c , T. Jones d a: SUPA school of Physics and Astronomy, University of Glasgow, Glasgow, UK b: Advanced Materials Group, RAL, STFC, UK c: School of Physics and Astronomy, The University of Manchester, UK d: Department of Physics, The University of Liverpool, UK * Contact e-mail: [email protected] Introduction Pixel mechanical test structure Pixel 2012: International Workshop on Semiconductor Pixel Detectors for Particles and Imaging , September 2012, Japan 0 5 10 15 20 25 30 35 -34 -33 -32 -31 -30 -29 -28 Position (mm) Temperature (deg C) Thermal testing and Simulations Proposed design Test object simulated and measured in dry air Thermal run-away on the test structure Thermal measurement test apparatus Thermal conductivity results Foam & CFRP Conductivity of BN filled Hysol 9396 epoxy Phi overlap on modules all disks on in ring to be placed on the same side gives simpler tape design - Lower contact area to high modules => Detailed FEA to take place Disks with have an inner radius of 130 mm and outer radius of 315 mm 3 rings of quad(hex) modules required. Services for middle ring will be a challenge Zoom showing space around modules Disk 4 Mixed module sizes (Hex, quad, quad) l measurements are steady state stems are verified against copper and silicon mperatures measured with 4 wire PT100s at from 4 wire electrical heaters Through-thickness measurements for glues and thin films Sample between Cu rods Pressure and DC340 at interfaces Measured at RT In-plane measurements for thin sheets Sample surrounded by radiation shield Under vacuum (10 -5 mbar) Measurements from -30C to +20C Plastic insulation supports Sample Aluminium thermal shield 1 Shiel d heate r 2 3 4 Pt100_5 H 2 O Wate r cool ed Heate r wires Pt100_ 6 Sampl e heate r Ancho r Heat sink Pt10 0 wire s Sample • ASIC power set to 1.56 W/chip (0.41 Wcm -2 ) • Nominal detector power ~ 3 mWmm -2 at 0C • Exact power depends on sensor thickness and desired collected charge • Factor of 4 in safety Cross-section of loaded cooling structure Silicon readout IC (150 μm thick) Solder bumps (20 μm thick) Silicon detector (300 μm thick) DC SE4445 gel (200 μm thick) CFRP K13C2U 50 gsm (200 μm thick) Allcomp Foam (2.3 mm thick) • Solder bumps at 5.3% fill factor • DC SE4445 100% coverage • No glue between foam and pipe • Input data from measurements • No glue between foam and pipe • HTC CO2 = 10k Wm -2 K -1 • HTC still air = 5 Wm -2 K -1 • Good agreement with data 0 2 4 6 8 10 12 14 16 18 -30 -28 -26 -24 -22 -20 -18 -16 -14 -12 -10 Qref T=0C (mW/mm2) Temperature (C) Pixel dummy heaters • 500um thick Silicon • 1um Tungsten with Cu solderable strip - Thermal simulation verification - Disk loading Allcomp foam 0 100 200 300 400 500 600 0 1 2 3 4 5 Glue thickness (um) Resistance (K/W) nterface resistance foam to metal ~ 0 K/W 0 50 100 150 200 250 0 5 10 15 20 25 30 35 Distanc e Temperature (C) Heat sink Q 500µm of hysol + 35% BN Senso rs Coppe r Coppe r Allcomp foam Glue penetrated into the foam Glue 1 Glue 2 • 35% BN by weight: k=1.4 W/mK • Degassing under vacuum makes little difference • Little change after irradiation IR camera plot of temp through sample k = t i k i t i = 2 k f FAW ρt for 90 direction K13D2U kf = 800 W/mK: K13C2U kf = 620 W/mK. Density = 2.19 gcm -3 CFRP K13D2U 0-90-0 100 gsm K13C2U 0-90-0 100 gsm Thickness (um) 230 254 0 - Predicted 318 229 ± 7 0 - measured 294 ± 20 285 ± 12 90 - predicted 159 114 ± 6 90 - measured 144 ± 20 Through thickness 1.20 & 0.96 1.3 & 1.1 • Large Hadron Collider (LHC) at CERN luminosity will increase by an order of magnitude around 2020 to the high luminosity HL-LHC • The ATLAS experiment will require a new tracker radiation damage and event density & rate • This tracker will consist of pixel and strip devices both as barrel and endcap disks. The new pixel detector Smaller pixels -> to minimize occupancy & increase spatial resolution Extremely radiation hard silicon detectors. New front-end electronics to cope with the higher data rates. These devices will be supported by low mass thermal-mechanical structures. • Enclosure at 20C flushed with N2 • CO2 from gas bottle - via chiller - & needle valve • Evaporation T = -33C • Measure with IR camera Test box / Cooling system

Low mass carbon based support structures for the HL-LHC ATLAS pixel forward disks R. Bates* a, C. Buttar a, I. Bonad a, F. McEwan a, L. Cunningham a, S

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Low mass carbon based support structuresfor the HL-LHC ATLAS pixel forward disks

R. Bates*a, C. Buttara, I. Bonada, F. McEwana, L. Cunninghama, S. Canferb, C. Lockettb, J. Paterc, R. Thompsonc, T. Jonesd

a: SUPA school of Physics and Astronomy, University of Glasgow, Glasgow, UKb: Advanced Materials Group, RAL, STFC, UKc: School of Physics and Astronomy, The University of Manchester, UKd: Department of Physics, The University of Liverpool, UK* Contact e-mail: [email protected] mechanical test structurePixel 2012: International Workshop on Semiconductor Pixel Detectors for Particles and Imaging , September 2012, JapanThermal testing and SimulationsProposed designTest object simulated and measured in dry airThermal run-away on the test structureThermal measurement test apparatusThermal conductivity results Foam & CFRPConductivity of BN filled Hysol 9396 epoxy

Phi overlap on modules all disks on in ring to be placed on the same sidegives simpler tape design- Lower contact area to high modules => Detailed FEA to take placeDisks with have an inner radius of 130 mm and outer radius of 315 mm3 rings of quad(hex) modules required.Services for middle ring will be a challenge

Zoom showing space around modulesDisk 4 Mixed module sizes (Hex, quad, quad) All measurements are steady stateSystems are verified against copper and siliconTemperatures measured with 4 wire PT100sHeat from 4 wire electrical heatersThrough-thickness measurements for glues and thin filmsSample between Cu rodsPressure and DC340 at interfacesMeasured at RTIn-plane measurements for thin sheetsSample surrounded by radiation shieldUnder vacuum (10-5 mbar)Measurements from -30C to +20C

Plastic insulation supportsSampleAluminium thermal shield1Shieldheater234Pt100_5H2OWater cooledHeater wiresPt100_6Sample heaterAnchorHeat sinkPt100wiresSample ASIC power set to 1.56 W/chip (0.41 Wcm-2) Nominal detector power ~ 3 mWmm-2 at 0C Exact power depends on sensor thickness and desired collected charge Factor of 4 in safety

Cross-section of loaded cooling structureSilicon readout IC (150 m thick)Solder bumps (20 m thick)Silicon detector (300 m thick)DC SE4445 gel (200 m thick)CFRP K13C2U 50 gsm (200 m thick) Allcomp Foam (2.3 mm thick) Solder bumps at 5.3% fill factor DC SE4445 100% coverage No glue between foam and pipe

Input data from measurements No glue between foam and pipe HTC CO2 = 10k Wm-2K-1 HTC still air = 5 Wm-2K-1 Good agreement with data

Pixel dummy heaters 500um thick Silicon 1um Tungsten with Cu solderable strip - Thermal simulation verification - Disk loading

Allcomp foam

Interface resistance foam to metal ~ 0 K/WDistanceTemperature (C)Heat sinkQ500m of hysol + 35% BNSensorsCopperCopperAllcomp foam Glue penetrated into the foamGlue 1Glue 2 35% BN by weight: k=1.4 W/mK Degassing under vacuum makes little difference Little change after irradiation IR camera plot of temp through sample

K13D2U kf = 800 W/mK: K13C2U kf = 620 W/mK. Density = 2.19 gcm-3CFRPK13D2U0-90-0100 gsmK13C2U0-90-0100 gsmThickness (um)2302540 - Predicted318 7 0 - measured294 20285 12 90 - predicted159114 690 - measured144 20Through thickness1.20 & 0.961.3 & 1.1 Large Hadron Collider (LHC) at CERN luminosity will increase by an order of magnitude around 2020 to the high luminosity HL-LHC The ATLAS experiment will require a new tracker radiation damage and event density & rate This tracker will consist of pixel and strip devices both as barrel and endcap disks.The new pixel detectorSmaller pixels -> to minimize occupancy & increase spatial resolutionExtremely radiation hard silicon detectors.New front-end electronics to cope with the higher data rates. These devices will be supported by low mass thermal-mechanical structures.

Enclosure at 20C flushed with N2 CO2 from gas bottle - via chiller - & needle valve Evaporation T = -33C Measure with IR cameraTest box / Cooling system