Upload
bruce-lee
View
219
Download
0
Tags:
Embed Size (px)
Citation preview
2010-04-08 LEPP meeting Dan Peterson
ILC highlights : Development of a TPC for the ILD detector at the ILC
There are some significant differences between an e+e- experiment (ILC, CESR, LEP) and a pp experiment (LHC).
At the ILC, the reduced noise in the detector opens tracking options that are not possible at the LHC; ILD uses a TPC. (OK, Alice uses a TPC, but that is different.)
The experiments drive the detector requirements; measurement of the recoil mass of l+ l- in (e+ e- HZ, Z l+ l-) drives the resolution; particle Flow Analyses requires a hermitic detector (98%). I will touch on the reasons for what we (LCTPC collaboration) are doing.
Then describe the “highlights” what I have been doing this year.
ILC TPC Large Prototype
Detectors, like the ILD are being planned by international collaborations.
One of the two certified detectors employs a Time Projection Chamber (TPC) for recognizing tracks and measuring the momentum.
(from a poster for “graduate student night” 2006)
30-October-2008, Endplate, fully assembled, with Micromegas module in center location.
30-October-2008 The leak test, on the field cage:
With 42 o-rings, and 8 pipe threads, the leak test passed.
(from a presentation at a Linear Collider workshop, 2008-11-15 )
The Cornell group built the endplatefor the TPC large prototype.Current work is an extension of the previous endplate development.
measure the mass recoiling against l+ l- in (e+ e- HZ, Z l+ l-)
δPt / Pt2 = 2 x 10-5 /GeV
recoil mass resolution is dominated by other effects
δPt / Pt2 = 4 x 10-5 /GeV
recoil mass resolution is starting deteriorate
δPt / Pt2 = 7 x 10-5 /GeV
recoil mass resolution is dominated by momentum resolution
(from a Journal Club, 2006-January )
Meeting the resolution goal δ(1/Pt) < 3 x 10-5 / GeV requires a point resolution of ~100μm, but more importantly, requires a knowledge of the magnetic field ∫ δ(Br) dz ~ 20 μm construction can deliver ~20 mm (not μm), mapping can deliver ~2 mm.
The improvement must come from track-based magnetic field calibration. For magnetic field calibration to converge, we must have a non-track-based calibration of the detector positions ~ 50 μm. We must have the stability of the detector positions ~ 50 μm
(from a Journal Club, 2006-January )
Particle Flow Analysis provides must jet energy resolution of about dE/E = 30% / E1/2
There are processes where WW and ZZ must be separated without beam constraints (example e+e- WW, ZZ ).
The energy resolution goal of the Particle Flow Analysis constrains the material in the endplate of the TPC, which is in front of the forward calorimeters.
This is not the LHC; this is a 98% hermetic detector.
At this time, the leading thought is that the material limit for the TPC endplate including structure, detector modules, electronics, and cooling, is 15% XO .
That is a summary of our development goals: detector placement and stability at the level of 50 μm (achieved by the 2008 endplate) endplate material ~ 15% XO (not achieved by the 2008 endplate).
Progress this year has been in building and comparing CAD models of possible replacements for the current Large Prototype endplate, which will provide input for designing the ILD endplate.
Material: space-frame has slightly more material than the Al-C hybrid.
Deflection: space frame is more rigid than LP1, ~3x more rigid than the lightened (all Aluminum), and > 3x more rigid than the Al-C hybrid.
mass material deflection stress kg %X0 microns Mpa (yield: 241)
LP1 18.87 16.9 33 1.5
Lightened 8.93 8.0 68 3.2(all aluminum)
Lightened Al 7.35 7.2 < 168* < 4.8* (Al-C hybrid) C 1.29 (* values for the aluminum only)
Space-Frame 8.38 7.5 23 4.2
Space-frame model
Lightened outer rim LP1 stiffening ring is removed. Cut-outs in radial machine tool direction leave material for strut mount.
Lightened Uninstrumented Area 5mm thickness as in hybrid
Sheet back-plane simple landing for strut mount removes adjustment of back-plane
Between-Row Struts term change, these are now “struts” not the major load carriers in the ILD endplate and can be low density
In-Row Struts major load carriers in ILD higher density
Outer circumference struts termination as in ILD
Strut properties
All struts are adjustable.
All parts are Aluminum.
Machined mount bolted to the front and back plates
Adjustment screw 10-24 (m4.8-1.06) on one end 10-32 (m4.8-0.91) on the other end sensitivity is 150 micron/turn As modeled, the screw is 4mm, which is approximately the stress diameter.
Spanning Rod As modeled, is 6mm solid, but could be 8mm hollow.
Deflection
Maximum is 23 microns
Back-plane locally warps ±5 micronsThe inside surface is smooth.
Back-plane twists at 3-point intersections. This feature will carry over to the ILD.
Not optimized: back-frame distance back-frame thickness vs strut density (spacing) strut thickness