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National Institute for Subatomic Physics Science Park 105, 1098XG Amsterdam The Netherlands
SciFi Forum on Tracking Detector
Mechanics 2015
R. Walet on behalf of the SciFi Tracker Group
2015-05 Rev_06
OVERVIEW
15-6-2015 R.Walet 2
5 [m]
SciFi Performance Summary
15-6-2015 R.Walet 3
Current tracking • 2 sub-systems: Inner Track, Outer
Tracker • Outer Tracker
– 24 layers of 5 mm gas drift tubes (2.5m long straws) in 3 stations of X-U-V-X
– Resolution ~200 micron • Inner Tracker
– silicon strip sensors with 0.18—0.20 mm pitch
– 12x X-U-V-X stereo layers – Resolution ~ 50 micron
Upgrade tracking • One single tracking Technology • “NEW” SciFi Tracking Detector
– 12 fiber mat layers composed of scintillating fibers (2.5m, d=0,25mm) in 3 stations of X-U-V-X
– Resolution 80 µm – Single hit efficiency: 96-97% – Run trigger less (remove L0) at 40
MHz read-out (only software trigger)
GOAL: “Be able to run at higher luminosity”
Scintillating Fiber Tracker
15-6-2015 R.Walet 4
2.5 m × 250µm
Readout box w/ cooling (-40oC) and FE boards
Fibre mats 2.5m ×13cm Fibres Silicon PM (SiPM) array: 128 × 250µm
Modules = Supporting panels + mats
5m mirrors
3 * X-U-V-X
6 m
5m
fiber
s
R.Walet 5
SUB-SYSTEMS;
5 [m]
• Infrastructure
• C-frames (12x)
• Modules (144x)
• Read-Out Box (288x)
Challenges Replace Inner and Outer tracker with a single technology • Higher granularity to reduce occupancy • Reduced material, Light weight • High rate capability • Large scale detector with fine measurement, handle
deformations of the fibers (modules) and read-out • To mitigate radiation damage until collecting at least
50 fb-1, SiPMs need to be cooled down to -40°C • Relative alignment SiPMs and fibers • Modular design with easy maintenance or
replacement procedures • High Resolution
15-6-2015 R.Walet 6
5 meter
C-Frame with module
R.Walet 7
Modules (144x)
Description Material kg/module TOTAL Scintillating fibers 94% polystyrene + 6% PMMA 4 576 Honeycomb cores Nomex 3 432 Casting and winding epoxy Epotek 301-2 1 144 Panel assembly glue Araldite 1 144 Carbon fibre skin Phenolic Resin 1,5 216 Endplugs* Aluminum 9,5 1368
TOTAL 20 2880
Very schematically a Module is: 1. A core of scintillating fibers, combined in a mat
(8 mats and a mirror makes one core) 2. Sandwich construction
1,5 mm
Materials
0.52 meter
CHALLENGES Winding of the fibermats
Polishing of the optical surfaces Flat/straightness assembled modules
Module Endpiece
R.Walet 8
Modules – Fibermats
2.5 meter
Alignment holes for module assembly
Fibermat winding machine
Fibermat casting JIG Casted Fibermat
13cm
Casting glue ; - protection layer 150μm - 1 day gluing - 3 days curing
Cutting slit Winding wheel
R.Walet 9
Modules – Sandwich
R.Walet 10
SiPMs(4608x)
Silicon Photomultipliers (SiPM)
0.250 mm
60μm pixel 32.59 mm
128 channel array
Kapton flex-pcb
1.62 mm
Connectors
6 layers of fibre per plane (Fiber D=0.250mm)
“Particle track”
R.Walet 11
Read-out Box (288x)
CHALLENGES thermal expansion and contraction
(different CTE’s with ∆T of 80-90°C) high position accuracy’s
condensation and frost prevention
Very schematically a ROB is: 1. SiPMs, SiPM cables, SiPM cooling, etc. “COLDBOX” 2. FE electronics boards, cables, etc. “FE ELECTRONICS”
Cabling, piping
R.Walet 12
Read-out Box Thermal Design Material CTE
[ppm/°C ] ∆T
[-50°Cv 40°C] ∆L [µm/SiPM* ] (*=32,59 mm)]
Silicium 2,6
90
7,6 Ti6Al4V 9 26,3 Copper 16,6 48,6 SS316 16,2 47,4 Epoxy 45-65 131,6-190,1 Polycarbonate 70 204,8
ISSUE 1. Different CTE’s
ISSUE 2. Behavior of the Endpieces by cooling down (every photon counts!!!!) Top: -40°C Outer: 5[W/mk], 16°C
Overall deformation
0.2 mm
0mm
∆Y=0.1mm; Airgap SiPM-Fibers
∆X±0.2mm; mis Alignement SiPM-Fibers
13cm
R.Walet 13
Read-out Box – Cooling bar
R.Walet 14
Read-out Box – Cooling bar Concept 1.
R.Walet 15
Read-out Box – Cooling bar Concept 2.
4-SiPMs heat spreader with SiPM cooling block (copper) 3 positioning pins in end piece
3D printed bellows
Z fixed
Z fixed
X fixed
Y fixed Spring force; optimal optical contacts
4-SiPMs heat spreader with SiPM cooling block (Ti6Al4V)
R.Walet 16
Read-out Box – Cooling bar
Y fixed X fixed
Z fixed Y fixed
Z fixed
EACH INDIVIDUAL COOLING SUBSTRATES POSITIONED AND ALIGNED WITH RESPECT TO SINGLE FIBER MAT
Concept 3. (new input; parallel cooling with d=2mm possible)
R.Walet 17
Read-out Box – Cooling bar Concept 4.
X fixed Z fixed
Y fixed Y fixed Y fixed
Z fixed • 3D printed Ti-alloy Grade 5 (min. Wall thickness 0,25mm) • Bellows (SS) from Witzenmann Challenge to braze SS (bellows) on Ti (bar) • Alternative: investigate 3D-printing of full cooling bar (incl. flexible joints)
EACH INDIVIDUAL COOLING SUBSTRATES POSITIONED AND ALIGNED WITH RESPECT TO SINGLE FIBER MAT Section; cooling bar
R.Walet 18
Read-out Box – Cooling bar Concept 5. Alternatives; 1. Copper pipe d=2mm
2. Pre-formed corrugated SS pipe D=3.5 d=3.3 mm
R.Walet 19
Read-out Box – Enclosure
Module with interfaces
Optical surface fiber ends
In-/outlet pipe cooling
Top cover with SiPMs, SiPM cables, SiPM cooling
Thermal enclousure (insulation box)
FE electronics
R.Walet 20
Read-out Box – Enclosure Requirements Coldbox to Module connection: o Flat sealing surface around module o Air tightness of all components within this surface o Mounting holes 2x7 m3
Contacted companies, 3D printing; o Shapeways o 3D systems o Heijcon
Coolingbar -40[degC]
SiPM package
R.Walet 21
Read-out Box – Enclosure
Soft Glue silicon
G10 stiffner
Mounting holes
Bends to increase flexibility to compensate
for thermal shrink and release forces on the
connectors
R.Walet 22
Read-out Box – Enclosure Outer shells are 3D printed in PA2200(Wall thickness 0,7mm) Parts will be filled with insulation foam
Cold box PU foam
R.Walet 23
Read-out Box – Enclosure First cold-boxes filled (without using molds) Good experience; but some air gaps in cold box. In parallel, order more boxes with:
• Different materials (e.g. ABS) • Different printing orientation (improve flatness)
R.Walet 24
Vacuum feedthrough
Vacuum insulation
1/8”VCR inside, ½” VCR outside Open vacuum pipe to Manifold
Standard bellows
Feedthrough topcover
End vacuum insulation
R.Walet 25
Vacuum feedthrough Vacuum insulated pipe
Feedthrough reducer
1/8”VCR inside ½” VCR outside Open vacuum pipe to Manifold
Oversized bellow to be able to open 1/8”VCR
Vacuum pipe crosses SiPM cables
End vacuum insulation
R.Walet 26
Vacuum feedthrough
1/8”VCR inside ½” VCR outside Open vacuum pipe to Manifold
Oversized bellow to be able to open 1/8”VCR
Mounting position Opening position
Press to access 1/8”connector
R.Walet 27
Conclusion & Outlook • the SciFi tracker is an essential component of the upgraded LHCb detector • it will allow running at (5×) higher luminosity • an extensive irradiation program demonstrated radiation tolerance of main components
– we can handle damage to fibres (6 layer mats) and SiPMs (cooling down to 40°C)
• lots of progress in new technologies – fiber winding and fiber-mats production on massive scale – custom design of SiPM arrays matching fiber geometry – direct fiber-to-SiPM interface – SiPM cooling down to -40°C in small volumes, modular approach (Read-out Boxes) – High functionality level per volume
• extensive use of exotic technologies like 3D printing
• large collaboration between 17 institutes* from 8 countries • series production to start in 2016 • installation in 2019 during LHC shutdown
*17 institutions: Kurchatov , ITEP, INR (RUS), Aachen, Dortmund, Heidelberg, Rostock (GER), EPFL (SUI), ClermontFerrand, LAL, LPNHE (FRA), Nikhef (NL), Barcelona, Valencia (SPA), CBPF (BRA), Tsinghua (CN), CERN
Back-up slides
15-6-2015 R.Walet 28
15-6-2015 R.Walet 29
Thermal Gap Fillers Take e.g. Laird 6200 T-flex
For ASiPM ~ 2 cm2 , 100 kPa ⇒ 20 N/SiPM force!
For ASiPM ~ 2 cm2 and PSiPM ~ 2 W, ∆T(100 kPa) = 13°C and ∆T(500 kPa) = 4.5°C
R.Walet 30
Radiation Damage - Fibers Light transmission of scintillating fibre decreases under irradiation • up to 35 kGy expected near the beam pipe over the upgrade lifetime
Expected ionizing dose for LHCb Upgrade
As measured by PIN diode
A mix of low dose, low rate xray, gamma, and high rate, high dose proton irradiations
Expect a 40% loss of transmitted light created near the beam pipe after 10 years
R.Walet 31
Radiation Damage - SiPM
SiPM arrays
Plot from N. Lopez March and M.Karacson
DCR reduction: factor 2 every ∆t=-10oC
Image from D. Gerick, presented at DPG Wuppertal, 11.03.2015
SiPM arrays
We expect 1.3 x 1012 neq/cm2 for 50 fb-1
• Requires cooling to -40°C • 150m of silicon arrays, without vacuum • DCR of a few MHz per channel at -40°C
after 50fb-1
• ~1 per 5-10 bunch crossings