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Technical Forum Alice week Clemens Adler

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Gain dependence of backpanel deformation by overpressure: ... and two-stage outlet regulation for ensuring uniform flow and overpressure (2,3) ... – PowerPoint PPT presentation

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Title: Technical Forum Alice week Clemens Adler


1
Transition Radiation Detector Status
  • Participating Institutions
  • Athens University, NIPNE Bukarest, JINR Dubna,
    IKF Frankfurt, GSI, PI Heidelberg, KIP
    Heidelberg, Uni Kaiserslautern, FH Köln, IKP
    Münster

2
Overview
  • Chamber design Body, Radiator,Padplane-/panel,
  • Reviews EDR, PRR
  • Performance EDR/PRR measurements, test beam
    results
  • Infrastructure Detector Control/Gas system
  • Production Sites, QA, Timescale

3
TRD Chamber Design
  • 540 (324) individual drift chambers (lt1450x1220
    mm²)
  • Main components
  • Radiator
  • Driftchamber
  • Padplane Backpanel
  • Challenge for mechanical design
  • Large Area, little Material
  • high rigidity _at_ low weight
  • (total 15 X0)

XeCO2(85/15)
4
Radiator
  • Produced at IKP Münster
  • Transition radiation produced by PP-fibres
    (different foams and fibres tested)
  • Rohacell core between Carbon fibre sheets (2 x
    100 µm)
  • Carbon laminate 2 manufactures in the game (FACC
    Fischer, AIK Stesalit)
  • Production started mid Feb.
  • 10 milestone reached end of July

5
Driftchamber/Wiring
  • 3 cm Driftregion
  • 2 wire planes
  • Cathode 75µm Cu-Be
  • Anode 25µm Au-W wire
  • Moderate gas gain 5000
  • Winding frame??

? Glueing
? Winding
6
Padplane
  • 1.2 million pads
  • Very large Area PCB
  • good precision challenge
  • Signalwires to be soldered to padplane
  • Soldering will be done at IKF Frankfurt with
    dedicated soldering machine

7
Padplane test system
  • Checking for shorts/bad (solder-) connections
    after soldering (at IKF)
  • Principle Capacitance measurement between pads
    and ground plate
  • Labview based system electronics developed at
    PI Heidelberg

8
Back Panel
  • Sandwich design build by FACC (Fischer)
  • Honeycomb between Carbon fibre (100µm)
  • Additional 2 mm Honeycomb on padplane side to
    reduce parasitic capacitance
  • Gluing of padplane to 2mm honeycomb very sucessful

9
TRD in Space Frame
  • 6 Layers, 5 colums per Supermodule
  • Small-scale prototype supermodule at Hd
  • Open issues
  • Connection of services
  • Final Engineering
  • Plan concentrated effort by JINR DubnaPI Hd to
    settle design by end 2003

10
Milestones EDR/PRR
  • EDR (Engineering Design Review) Sep. 2002
  • Questions adressed
  • Mechanical stability
  • Gain uniformity, etc.
  • Open questions
  • Gain uniformity
  • Leak rate (3 mbarl/h)
  • PRR (Production Readiness Review) April 2003
  • Question addressed
  • Final mechanical design
  • Prototype performance
  • Production steps
  • QA procedures
  • Leak rate

11
Prototype measurements
  • Gain non-uniformity lt 15
  • tight requirement on backpanel flatness lt200µm
  • Gain dependence of backpanel deformation by
    overpressure
  • Gas tightness (driven by cost of Xenon)
  • Goal lt3 mbarl/h
  • Prototype lt0,1 mbarl/h (optimistic conditions)
  • Gas interconnections need test in realistic
    conditions (several chamb.)
  • Agrees well with Garfield calculations
    mechanical measurements

12
Test beam results
Signal vs. Drift time
  • Testbeams at CERN and GSI
  • ? TR-Spectrum
  • Pion reject. factor gt100 ?

13
Test beam cont.
  • Position resolution vs. Gain
  • 300-400 µm (??)
  • High precision dE/dx measurement ? NIM paper in
    prep.
  • Space charge effects in drift chambers operated
    with Xe/CO2
  • ? NIM paper in prep.

14
Detector Controls (DCS)
  • HVLV
  • Power supplies decided
  • Minor Problems concerning communication (between
    electronics)

15
Cooling
  • Tests at CERN last year
  • cooling pipe design fixed
  • cooling seems to be no problem
  • Final tests to be done at Heidelberg (all
    hardware is available)

16
Services
  • Little space within Supermodule, but all services
    fit
  • Services towards TOF stay within envelope

17
Gas system
  • Problems
  • High cost gas (5 /l of Xe)
  • High hydrostatic pressure over 7 m height
  • Light and large detectors, no big under- or
    over-pressures affordable
  • Highly segmented detector (540 chambers)
  • Solutions
  • Gas recirculation, minimal fresh gas injection
    (1)
  • Pressure regulation subdivided into (groups of)
    sectors (2,3)
  • Capillary gas inlet and two-stage outlet
    regulation for ensuring uniform flow and
    overpressure (2,3)
  • Gas regeneration for Xe recuperation (1,4)

18
Gas system schedule
  • Design practically ready
  • Need to decide on final regulation segmentation
  • PRR in October (following other gas system PRRs)

19
Chamber Production Sites
  • Production sites
  • Heidelberg
  • Dubna
  • GSI
  • Bukarest
  • (Münster)
  • (Frankfurt)
  • Philosophy Each site does everything
  • to be seen...

20
Production QA
  • During production
  • Tolerances
  • Panel flatness
  • Wiring
  • Field cage
  • Padplane
  • After Production
  • Electrostatic tests
  • Leak rate
  • Gain (-uniformity)
  • Gas system ready in Hd (Ar/CO2)
  • X-Ray test stand (Dubna/Hd)
  • Okt./Nov. 2003
  • Results stored in DCDB (work ongoing)
  • Labview interface to DB
  • Interface to HV, O2 meter etc.

21
Schedule
  • 3 Supermodules 90 chambers have to be ready by
    1/2005
  • production rate per site 2 chambers/week

Material delivery times
  • Production start
  • Heidelberg now
  • Dubna Dec.
  • Bukarest 1/2004
  • GSI 4/2004

22
Summary
  • Chamber design is finalized
  • Prototype performance to spec.
  • TRD Chamber production is starting NOW (material
    is slowly arriving) at Hd
  • Other institutions getting ready for production
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