Cooling pipes, heat management, temperature, humidity control of - - PowerPoint PPT Presentation
Cooling pipes, heat management, temperature, humidity control of - - PowerPoint PPT Presentation
Cooling pipes, heat management, temperature, humidity control of VXD Overview SVD PXD 2 carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013 VXD Heat Sources SVD Origami 1748 APV25 chips ~ 0.4W / chip ~ 700W in total Hybrid
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Overview
2
SVD PXD
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
VXD Heat Sources
3
;
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1748 APV25 chips ~ 0.4W / chip ~ 700W in total 18W per ladder ~ 360 W in total Switcher (1W total) DCD (1.5W/chip) DHP (0.5W/chip) Sensor (1W total) Origami Hybrid Hybrid
SVD PXD
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
VXD Heat Dissipation and CO2 Cooling Circuits
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CO2 Circuit Detector Half Layer Type Side Power [W] 1 up 1&2 endring bwd 90 2 PXD up 1&2 endring fwd 90 3 PXD down 1&2 endring bwd 90 4 down 1&2 endring fwd 90 sum sum PXD 360 5 left 3-6 endring bwd 93 6 right 3-6 endring bwd 93 7 left 3-6 endring fwd 93 8 SVD right 3-6 endring fwd 93 9 SVD left 4&5
- rigami
bwd 68 10 right 4&5
- rigami
bwd 68 11 left 6
- rigami
bwd 96 12 right 6
- rigami
bwd 96 sum sum SVD 700 sum sum VXD 1060
plus parasitic heat load from environment
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
VXD Cooling System Requirements
5
Minimize material in acceptance region SVD requirements:
- APV25 surface temperature @ ~ 0°C for SNR improvement
- dissipated power ~ 700 W
PXD requirements:
- sensor temperature < 25°C (noise)
- temperature of ASICs < 50°C (avoid electro-migration)
- dissipated power ~ 360 W
- goal: cooling block @ < -20°C
Total power generated in VXD ~ 1kW plus:
- additional heat loss through 15 m of transfer lines
- parasitic heat load inside VXD volume from environment
- => required cooling capacity of CO2 system 2-3 kW (IBBelle design 3.3 kW)
Dry Air Volume
- dew point < -30oC
Outside of VXD: room temperature ( ~ 23°C) at the inner surface of CDC
- needs to be kept stable for calibration
- => need a thermal enclosure, well isolated
carsten.niebuhr@desy.de BPAC VXD Cooling 11.09.2013
Compensation for Thermal Expansion/Contraction
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carsten.niebuhr@desy.de BPAC VXD Cooling 11.09.2013
Compensation for Thermal Expansion/Contraction
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Sliding Mechanism SLM in forward direction (M.Friedl)
carsten.niebuhr@desy.de BPAC VXD Cooling 11.09.2013
Compensation for Thermal Expansion/Contraction
6
Sliding Mechanism SLM in forward direction (M.Friedl) After installation forward end-flange is
- nly attached to PXD
support using gliding pin in plastic bushing
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Cooling Environment
7
!"##$%&'()'*"+&),&(%&&-)./0)"-1)/2/3 +$41 56)77
Dry Volumes Docks
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
<=(> >5?#@=(AB& C=5 DEF GH#897I!J GAK -= &)>#C(4)*& =C DEFJ L==B -&BK&54-A5& >5?#@=(AB&' F5?)&'' 5&MA%5&B&)-N >&O K=%)- P#8Q7I!# GAK -= &)>#O4((# =C !F!J RF=<ST# 45&4
@=(AB& C=5
@=(AB& C=5
Dryness requirement: dew point < -30°C
„cold“ VXD dry volume up to VXD end flange
Dry Volumes Inside CDC
8
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Connection of CO2 Lines to Vacuum Isolation
9
&)<#=> ?@45AB#<5C#D=(EA& '-4)<45< F!G H=))&H-=5' ?'I4H& %)'%<& <=HJ#45&4B# „normal“ atmosphere
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
CO2 Lines inside VXD Volume
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;<=>#!?9#(%)&' -@ &)A#5%)*' /B= C+#DB= 9 0E=># !?9#(%)&' -@ F@G)- H(@IJ /B= 9+#DB= 9 5&A># I@))&I-%@)' K@5 &)L%5@)F&)-4(# F@)%-@5%)* MD?;N#
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
CO2 Lines inside VXD Volume
Need CO2 connectors close to the endflange
- CO2 pipes must be assembled prior to VXD installation
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;<=>#!?9#(%)&' -@ &)A#5%)*' /B= C+#DB= 9 0E=># !?9#(%)&' -@ F@G)- H(@IJ /B= 9+#DB= 9 5&A># I@))&I-%@)' K@5 &)L%5@)F&)-4(# F@)%-@5%)* MD?;N#
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
CO2 Lines inside VXD Volume
Need CO2 connectors close to the endflange
- CO2 pipes must be assembled prior to VXD installation
10
;<=>#!?9#(%)&' -@ &)A#5%)*' /B= C+#DB= 9 0E=># !?9#(%)&' -@ F@G)- H(@IJ /B= 9+#DB= 9 5&A># I@))&I-%@)' K@5 &)L%5@)F&)-4(# F@)%-@5%)* MD?;N#
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Miniature Tube Fittings
11
Design based on development for CMS pixel upgrade
- modification for Belle II: add copper gasket
Tests performed
- 2 (150 bar) √
- tightness test with CO2 (110 bar, 48 h) √
- helium leak test at room temperature and in liquid nitrogen √
- repeatability (open/close cycles with same gasket) √
copper gasket
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Transfer Line Routing to VXD
12
<=4((# >?5@4-?5& 54A%?' B&C(4>& >D55?*4-&A C%C& EF <<#@4>??= C%C& G69#==H
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Transfer Lines
13
! !
*(`b
- *+
- *P
- A9W;8
@;4W; F64A;8 F56;8 =>F5J47=9> *)J4Y;8 *
- *`+
- ,
- 1
- V4<55ED#**)`*b(#EEc
%>657D#)`/Pb#EEc O57657D#bC)bP#EEc
Baseline for CO2 transfer line diameter increased from 12mm to 18mm
- CERN uses 18 mm lines for ATLAS-IBL
- want to maintain maximum compatibility
between ATLAS-IBL and Belle II VXD
Disadvantages
- bending radius might be problematic
- service space allocation is no longer sufficient
if 18 mm lines are used everywhere
Mechanical bending tests performed at MPI
- bending by 40° (elastically) needs about 3 kg
- quoted bending radius is 45 mm
- tested down to 20 mm
- Xray shows no problems even for 20 mm bend
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Transfer Lines
13
! !
*(`b
- *+
- *P
- A9W;8
@;4W; F64A;8 F56;8 =>F5J47=9> *)J4Y;8 *
- *`+
- ,
- 1
- V4<55ED#**)`*b(#EEc
%>657D#)`/Pb#EEc O57657D#bC)bP#EEc
Baseline for CO2 transfer line diameter increased from 12mm to 18mm
- CERN uses 18 mm lines for ATLAS-IBL
- want to maintain maximum compatibility
between ATLAS-IBL and Belle II VXD
Disadvantages
- bending radius might be problematic
- service space allocation is no longer sufficient
if 18 mm lines are used everywhere
Mechanical bending tests performed at MPI
- bending by 40° (elastically) needs about 3 kg
- quoted bending radius is 45 mm
- tested down to 20 mm
- Xray shows no problems even for 20 mm bend
CO2 inlet CO2 return MLI
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Transfer Lines
13
! !
*(`b
- *+
- *P
- A9W;8
@;4W; F64A;8 F56;8 =>F5J47=9> *)J4Y;8 *
- *`+
- ,
- 1
- V4<55ED#**)`*b(#EEc
%>657D#)`/Pb#EEc O57657D#bC)bP#EEc
Baseline for CO2 transfer line diameter increased from 12mm to 18mm
- CERN uses 18 mm lines for ATLAS-IBL
- want to maintain maximum compatibility
between ATLAS-IBL and Belle II VXD
Disadvantages
- bending radius might be problematic
- service space allocation is no longer sufficient
if 18 mm lines are used everywhere
Mechanical bending tests performed at MPI
- bending by 40° (elastically) needs about 3 kg
- quoted bending radius is 45 mm
- tested down to 20 mm
- Xray shows no problems even for 20 mm bend
CO2 inlet CO2 return MLI
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Test of ATLAS-IBL Prototype Transfer Lines
14
Inlet Outlet Rigid Part Flexible Part
- 0.1
0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 5 5.5 6 6.5 7 7.5 8 8.5 9 9.5 10 dT [K] Mass Flow Rate [g/s]
(Tout-Tin) vs Mass Flow Rate
- 0.5
0.55 0.6 0.65 0.7 0.75 0.8 0.00E+00 5.00E-04 1.00E-03 1.50E-03 2.00E-03 2.50E-03 3.00E-03 3.50E-03 4.00E-03 dT [K] Vacuum Level [mbar]
(Tref-Tcs) vs Vacuum Level
- M. Gutt-Mostowy
CERN Cryo Lab Results according to expectations
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Transfer Line Routing
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5<=-%)* <> ?4@==A8%'<(4-&B
- 54)'>&5 (%)&'
/EF DEF J!K8L J!K8C
=+/*$&.20)$042$0662%/07-2$5+4$!9!$(4+,%$
Detailed solution
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Transfer Line Routing
16
!;9+ 4%5 !;9+#4%5
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Alternative Design for Transfer Lines
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- K. Gadow
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Simulation vs Measurement
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Cobra example: Node network for IBL
23 T
environement
R4 HTCair R2 +R3 TFoM R1 HTCCO2 TCO2 T
environement
TCO2 TCO2 R4 +R3 Insulation+HTCair R5 Heat exchange R1 HTCCO2 R2 Tube wall Q3 Applied power T
environement
TCO2 R4 +R3 HTCair R1 HTCCO2 R2 Tube wall T
environement
TCO2 R1 HTCCO2 R2 Tube wall TCO2 R1b HTCCO2 R1a HTCCO2 R4 +R3 Insulation+HTCair
- 1. Concentric line
- 3. Bare tube
- 2. Bundled lines
- 4. Stave
Detector Mechanics Forum Oxford, 20 June 2013 Bart Verlaat
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Simulation vs Measurement
18
Cobra example: Node network for IBL
23 T
environement
R4 HTCair R2 +R3 TFoM R1 HTCCO2 TCO2 T
environement
TCO2 TCO2 R4 +R3 Insulation+HTCair R5 Heat exchange R1 HTCCO2 R2 Tube wall Q3 Applied power T
environement
TCO2 R4 +R3 HTCair R1 HTCCO2 R2 Tube wall T
environement
TCO2 R1 HTCCO2 R2 Tube wall TCO2 R1b HTCCO2 R1a HTCCO2 R4 +R3 Insulation+HTCair
- 1. Concentric line
- 3. Bare tube
- 2. Bundled lines
- 4. Stave
Cooling development philosophy
Whatever the model give as a result:
models are empirical. Use them as a design guideline.
Always verify in a test!
Not only to quantify heat transfer, but as well to filter out strange behavior
2 4 6 8 10 12 14
- 20
- 18.4
- 16.8
- 15.2
- 13.6
- 12
Length [m] Temperature [°C] Test 1 | m = 2.94g/s | Qtotal = 159.30W | dP = 17.77Bar | dT = 4.20°C dTexp =6.55°C dPexp =20.41bar 2 4 6 8 10 12 14 19 23.4 27.8 32.2 36.6 41 Pressure [Bar]
- Exp. Wall Temperature
Theory Wall Temperature Theory CO2 Temperature
- Exp. CO2 Pressure
Theory CO2 Pressure
Detector Mechanics Forum Oxford, 20 June 2013 Bart Verlaat
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Thermal Mock-up @ DESY
19
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Thermal Mock-up @ DESY
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Hot water chiller Paraffin chiller Beam pipe heating Vacuum isolated transfer lines (8m) CO2 Distributor Beam pipe Vacuum pump PXD dry volume end caps
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Beam Pipe Mock-up
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Aluminium Stainless Steel
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
MARCO connected to Thermal Mock-up
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Delivery of MARCO to DESY delayed (22.7.) because of failures of CO2 pumps. Spare pump heads ordered as back-up. Alternative pumps under long-term study at CERN. Thermal camera Dummy load
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Simulatig PXD Heat Load
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carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Simulatig PXD Heat Load
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carsten.niebuhr@desy.de BPAC VXD Cooling 11.09.2013
Dummy Sensors
23
Heater will be replaced by dummy sensors with integrated resistors to be provided by HLL
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Set-up for Telescope Test @ DESY
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- 4 SVD layers
2 PXD layers Detectors will be cooled with CO2 Chance to gain experience with full chain under more realistic conditions Extended thermal mock-up (incl. SVD) will allow more detailed studies after beam test
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Dry Air Supply @ Tsukuba Hall
25
Existing Dryer filter on top of Belle E-hut Dew point of -50°C reached ~ 6 hours after switching on Capacity 30 l/min should be sufficient Tsuboyama-san
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Dry Air Supply
26
In total foresee 12 cooling pipes on both side of VXD
- CO2 lines: 8 bwd and 4 fwd
- (cold) dry air: 4 bwd and 8 fwd
Only sketch of a solution
- exact path and connection details will depend on experience
to be gained with thermal mock-up
<=4((# >?5@4-?5& 54A%?' B&C(4>& >D55?*4-&A C%C& EF <<#@4>??= C%C& G69#==H
bwd fwd 12
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Dry Air Supply
26
In total foresee 12 cooling pipes on both side of VXD
- CO2 lines: 8 bwd and 4 fwd
- (cold) dry air: 4 bwd and 8 fwd
Only sketch of a solution
- exact path and connection details will depend on experience
to be gained with thermal mock-up
<=4((# >?5@4-?5& 54A%?' B&C(4>& >D55?*4-&A C%C& EF <<#@4>??= C%C& G69#==H
bwd fwd 12 x2 x2 x2 x2 12
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Temperature & Humidity Control
Several redundant temperature measurements will be in place
- fibre optical sensors (FOS)
- temperature sensors integrated in chip (slow r/o)
- PT100 => fast trigger for power off
Ensure VXD volume tightness
- the enclosure needs to be sufficiently tight so that in case of a dry gas failure it takes minutes/hours for
the humidity to rise and to reach the dew point
Need a humidity monitoring system
- monitoring system based on humidity sensors
- preventive system that monitors humidity inside VXD volume
- radiation hardness is an issue (– system under development at IFIC-CSIC, Valencia)
In addition need independent safety interlock system (based on PLCs) to monitor dry gas flow into detector volume with flowmeter (also at outlets if the volume tightness is good enough).
- measurement requires minimum flow
- safety interlock system powers down the main power system of the detector (see talk on SC by
M.Ritzert)
27
Fiber Bragg Grating Optic Sensor
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
4%/1* +,-%#.#$'/%0"123&' !""#$%&&
Temperature Rise in Case of CO2 Failure
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Failure of cooling system caused temperature rise above 100°C within a few minutes Fast reaction is required to avoid damage of detector FOS measurement
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Humidity Sensors
Fibres for temperature and %RH monitoring on the PXD frame (IFCA) A standalone temperature and %RH system is being developed at IFIC for BEAST-II:
- RH% Sensors = UPS-500 or UPS-600
from Ohmic instruments
- PT100 temp sensors
- Readout = Mother-board based on
ARDUINO
Next steps:
- Finalize characterization of prototype
- Irradiation with protons in the next
months
- Try and test 2 other capacitive sensors.
The same readout can be used. Better
- perational range (0-100 %RH)
29
Arduino: 6,5 X 5,5 cm Sensor Sensor with integrated readout, but RO not radiation tolerant Developed Mother-board P-14 (Innovative Sensor Technology) HCH-1000 (Honeywell)
carsten.niebuhr@desy.de SVD Review VXD Cooling 11.09.2013
Summary
Requirements for VXD cooling system well defined Overall concept of heat management available Many detailed individual studies indicate that VXD cooling concept is viable
- see specific talks on PXD and SVD
Several aspects require further studies with a realistic thermal mock-up
- goal is to complete mock-up after telescope test at DESY
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