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BWEC Cooling shell design
PANDA 17/2 Collaboration Meeting BWEC Cooling shell design S. Ahmed, L. Capozza, A. Dbeyssi, P. Grasemann, J. Jorge Rico, F. Maas, O. Noll, D. Rodríguez Piñeiro, S. Wolf BWEC Cooling shell design
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Contents Overview Calculations (thermal and fluid mechanics) 3D design
Simulations (thermal and fluid mechanics) Summary and future tasks BWEC Cooling shell design 2
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Overview 1 What is our aim? BWEC Cooling shell design 3
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Vacuum insulation panel (VIP)
Overview Overview Cooling requirements Work at -25°C Maximum 500 mbar pressure drop (leakless-mode) Limited space Low temperature gradient Inserts Outer shell Mounting plate Cover Front cooling Boards Vacuum insulation panel (VIP) Crystals Coolant Inner shell Methanol 60% Water 40% Property Value Units Density 930 kg/m3 Dynamic viscosity 0.0077 kg/s/m Cp 3151 J/kg/K BWEC Cooling shell design 4
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THE PROCESS IS THIS Calculate & Design Simulate Test
BWEC Cooling shell design 5
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Thermal and fluid mechanics calculations of the cooling shells
2 Thermal and fluid mechanics calculations of the cooling shells BWEC Cooling shell design 6
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Thermal calculations Electronics Heat flow through the walls
Heat sources Electronics Heat flow through the walls Power to cool down P +70C APFEL 1.5 BWEC Cooling shell design 7
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Thermal calculations 150 mW/crystal * 524 crystals =78.60 W
Electronics 150 mW/crystal * 524 crystals =78.60 W Applied in back side of crystals Cables out of the detector are not taken into account BWEC Cooling shell design 8
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Thermal calculations Worst case at 70°C surrounding temperature
Outer face Heat flow through walls Front face Back face Worst case at 70°C surrounding temperature Inner face Source Value [W] Outer face 40.23 Inner face 17.25 Front face 16.63 Back face 18.59 Radiation 27.92 BWEC Cooling shell design 9
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Thermal calculations Constant cooling flow Initial temperature 30°C
Power to cool down Constant cooling flow Initial temperature 30°C Final temperature -25°C Time 24 h 𝑷= 𝑚∙ 𝐶 𝑝 ∙∆𝑇 𝑡 = 0,06 𝑚 3 ∙ 8280 𝑘𝑔 𝑚 3 ∙ 262 𝐽 𝑘𝑔 ∙(55°𝐶) 24 ℎ∙3600 𝑠 =𝟖𝟑.𝟎𝟎 𝑾 BWEC Cooling shell design 10
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Summary of heat sources
Stationary Transient Source Value [W] Outer face 40.23 Inner face 17.25 Front face 16.63 Back face 18.59 Radiation 27.92 Electronics 78.60 Cooling down 83.00 Total 199.30 203.70 Total*1.5 298.95 305.98 Safety factor 1.5 BWEC Cooling shell design 11
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Thermal calculations Mass flow calculation Distance between pipes
0.3 °C between inlet and outlet (homogeneity) 𝑚 = 𝑃 𝐶 𝑝 ∙∆𝑇 = 𝑘𝑔 𝑠 → 20.88𝑙 𝑚𝑖𝑛 2 outer shells and 2 inner shells Outer shell 7.34 l/min Inner shell 3.10 l/min Distance between pipes 0.25 °C max temperature difference (homogeneity) 15 mm thickness L= 150 mm 𝑃 𝐿 2 8∙𝑘∙𝑡 =∆𝑇→𝐿= 8∆𝑇𝑘𝑡 𝑃 L BWEC Cooling shell design 12
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Fluid mechanics calculations (Half outer shell)
Outer shell parts 6 pipes d = 13 mm 4 pipes d = 10 mm 5 front square connectors 4 back elbow connectors BWEC Cooling shell design 13
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Fluid mechanics calculations
Pipe with d = 10 mm ∆𝑝= 8 𝑄 2 𝜋 2 𝑓 𝐿 𝐷 5 𝜌=11.37𝑚𝑏𝑎𝑟 Elbow of d = 10 mm ∆𝑝= 8 𝑄 2 𝜋 2 𝑓 𝐿+ 𝐿 𝑒𝑞 𝐷 5 𝜌=21.05 𝑚𝑏𝑎𝑟 Pipe with d = 13 mm ∆𝑝= 8 𝑄 2 𝜋 2 𝑓 𝐿 𝐷 5 𝜌=3.99 𝑚𝑏𝑎𝑟 Square connector (estimation) ∆𝑝= 8 𝑄 2 𝜋 2 𝑓 𝐿+ 𝐿 𝑒𝑞 𝐷 5 𝜌=27.60 𝑚𝑏𝑎𝑟 BWEC Cooling shell design 14
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Fluid mechanics calculations summary
Part Pressure drop (mbar) Amount Total Pd (mbar) Straight d =13 mm 3.99 6 23.94 Straight d = 10 mm 11.37 4 45.48 Elbow d = 10 mm 21.05 84.20 Square connectors 27.60 5 138.00 Total mbar 𝟐𝟗𝟏.𝟔𝟐𝒎𝒃𝒂𝒓<𝟓𝟎𝟎𝒎𝒃𝒂𝒓 BWEC Cooling shell design 15
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An overview of the outer shell 3D design
🎨 3D design 3 An overview of the outer shell 3D design BWEC Cooling shell design 16
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3D design BWEC Cooling shell design 17
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3D design Front square connectors Back elbows
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4 Simulations Thermal and fluid mechanics simulations
Autodesk Simulation Mechanical & Autodesk CFD 2016 BWEC Cooling shell design 19
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Thermal simulations 1 quarter dummy for simulations
Outer shell (Aluminum) Front shell (HDPE) Inserts (Aluminum) Gap (air 4mm) Crystals (PbWO4) Inner shell (Aluminum) 1 quarter dummy for simulations BWEC Cooling shell design 20
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Only outer and inner shells
Thermal simulations Only outer and inner shells Not front shielding 2°C gradient °C °C BWEC Cooling shell design 21
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Back pipe with both inner and outer shells
Thermal simulations Back pipe with both inner and outer shells Back homogeneity °C Not front shielding 2°C gradient °C BWEC Cooling shell design 22
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Front shell, back pipe and both inner and outer shells
Thermal simulations Front shell, back pipe and both inner and outer shells Out of scale -5°C Front shielding Less than 0.5°C gradient °C °C Solid angle loss (further for the IP) BWEC Cooling shell design 23
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Possible 140W (STT worst elect. case) front without front cooling
Thermal simulations Possible 140W (STT worst elect. case) front without front cooling -25,06 °C Huge temperature gradient (7.13°C) -17.87°C BWEC Cooling shell design 24
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Possible 140W (STT worst elect. case) front with front cooling
Thermal simulations Possible 140W (STT worst elect. case) front with front cooling Out of scale 57°C Good front protection Less than 0.5°C gradient °C -24.00°C Solid angle loss (further from the IP) BWEC Cooling shell design 25
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Straight pipes and elbow
Fluid mechanics simulations Straight pipes and elbow 4.00 mbar 23.82 mbar 11.63 mbar BWEC Cooling shell design 26
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Front square connectors
Fluid mechanics simulations Front square connectors BWEC Cooling shell design 27
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Front square connectors
Fluid mechanics simulations Front square connectors BWEC Cooling shell design 28
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Front square connectors
Fluid mechanics simulations Front square connectors BWEC Cooling shell design 29
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Front square connectors
Fluid mechanics simulations Front square connectors 35.44 mbar 31.21 mbar 30.28 mbar BWEC Cooling shell design 30
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Fluid mechanics simulations
Summary Part Pressure drop/part(mbar) Amount Total Pd (mbar) Straight d = 10 mm 11.63 4 46.52 Straight d = 13 mm 4.00 6 24.00 Elbow d = 10 mm 23.82 95.28 Square conn 1 35.44 2 70.88 Square conn 2 31.21 62.42 Square conn 3 30.28 1 Total mbar BWEC Cooling shell design 31
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Fluid mechanics calculations vs. simulations
Part Pressure drop (mbar) Amount Total Pd (mbar) Straight d =10 mm 11.37 4 45.48 d = 13 mm 3.99 6 23.94 Elbow d = 10 mm 21.05 84.20 Square conn 1 27.60 2 55.20 Square conn 2 Square conn 3 1 Total mbar Part Pressure drop (mbar) Amount Total Pd (mbar) Straight d = 10 mm 11.63 4 46.52 d = 13 mm 4.0 6 24.00 Elbow 23.82 95.28 Square conn 1 35.44 2 70.88 Square conn 2 31.21 62.42 Square conn 3 30.28 1 Total mbar BWEC Cooling shell design 32
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Summary and future works
5 What is next? BWEC Cooling shell design 33
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Summary Less than 0.3oC of gradient in the coolant temperature
Good homogeneity with front cooling Low pressure drop: Different pressure drop values because of the square parts (simplifications in calculations for complex geometry) Calculations Simulation mbar mbar BWEC Cooling shell design 34
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Future works Building an outer shell prototype (on process)
Make measurements for validating calculations and simulations Tests for front cooling with existing prototype (on process) Design inner shell with the same procedure BWEC Cooling shell design 35
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Any questions? You can write me jjorgeri@uni-mainz.de
THANKS! Any questions? You can write me BWEC Cooling shell design 36
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Back Up slides BWEC Cooling shell design
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Front cooling Connectors MP Hole Preparation in Outer shell and MP
BWEC Cooling shell design B1
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Front cooling Parallel circuits (low pressure drop)
Preliminary design Parallel circuits (low pressure drop) Different diameter each branch (homogeneity) 3D printed (HDPE) BWEC Cooling shell design B2
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Simulations Velocity examples BWEC Cooling shell design B3
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Thermal calculations General inputs BWEC Cooling shell design
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Thermal calculations Example BWEC Cooling shell design B5
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Thermal calculations Output summary BWEC Cooling shell design
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Fluid mechanic calculations
Serial Pressure drop calculator Inputs: Coolant Section´s geometry Length Local elements Flow Valve Height BWEC Cooling shell design B7
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Fluid mechanic calculations
Serial Pressure drop calculator Outputs: Reynolds Laminar/ Turbulent Friction factor Pressure drop Pressure difference BWEC Cooling shell design B8
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Fluid mechanic calculations
Parallel calculator Flow Aim: Constant flow through all branches. Procedure: Change diameter of branches. Flow/4 Flow/4 Flow/4 Flow/4 Flow BWEC Cooling shell design B9
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Fluid mechanic calculations
Parallel calculator Inputs: Coolant Different geometry for sections Lengths Local elements Number of branches Height . BWEC Cooling shell design B10
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Fluid mechanic calculations
Parallel calculator Outputs: Total pressure drop Pressure drop in manifold Different diameters . BWEC Cooling shell design B11
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Front cooling test Aim: See the effect of different materials
in the front cooling Effect of different VIP´s configuration 20mm 2x10mm Validate thermal and fluid mechanic calculation system. . BWEC Cooling shell design B12
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Front cooling test Layout . Different materials
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Cold nitrogen test Layout . Cool down the nitrogen
BWEC Cooling shell design B14
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Dew point at 20°C Calculations BWEC Cooling shell design 08.06.2017
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Dew point at 20°C Psychrometric chart BWEC Cooling shell design
B14
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Dew point at 20°C Kapton heating BWEC Cooling shell design 08.06.2017
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Distance between pipes
All the heat received for the plate is transported by conduction 𝑃 𝑞𝑐 +∆𝑥 = 𝑞𝑐+ 𝜕𝑞 𝜕𝑥 𝑑𝑥+… Q w 𝑞𝑐 +∆𝑥 − 𝑞𝑐= 𝜕𝑞 𝜕𝑥 𝑑𝑥+… 𝑞𝑐 𝑞𝑐 +∆𝑥 t 𝑞𝑐 +∆𝑥 − 𝑞𝑐= 𝜕 𝜕𝑥 −𝑘 𝜕𝑇 𝜕𝑥 𝑑𝑥+… dx x 𝑑 𝑑𝑥 𝑄 𝐶 =𝑃∙𝑤∙𝑑𝑥 (𝑞𝑐 +∆𝑥 −𝑞𝑐)∙𝑡∙𝑤=𝑃∙𝑤∙𝑑𝑥 −𝑘∙𝑡∙𝑤∙ 𝑑 2 𝑇 𝑑 𝑥 2 𝑑𝑥=𝑃∙𝑤∙𝑑𝑥 𝑑 2 𝑇 𝑑 𝑥 2 =− 𝑃 𝑘∙𝑡 BWEC Cooling shell design B14
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Distance between pipes
Boundary conditions Symmetry: Q(L/2)=0 T(0)=Te 𝑇 𝑥 =− 𝑃 2∙𝑘∙𝑡 ∙ 𝑥 2 +𝐴∙𝑥+𝐵 𝑇 0 =− 𝑃 2∙𝑘∙𝑡 ∙ 0 2 +𝐴∙0+𝐵→𝐵=𝑇𝑒 𝜕𝑇 𝜕𝑥 𝐿/2 =− 2𝑃 2∙𝑘∙𝑡 ∙ 𝐿 2 +𝐴=0→𝐴= 𝑃𝐿 2𝑘𝑡 𝑑 2 𝑇 𝑑 𝑥 2 =− 𝑃 𝑘∙𝑡 Te x L/2 BWEC Cooling shell design B14
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Distance between pipes
Te 𝑇 𝑥 =− 𝑃 2∙𝑘∙𝑡 ∙ 𝑥 2 + 𝑃𝐿 2∙𝑘∙𝑡 ∙𝑥+𝑇𝑒 x L/2 We want T(L/2) ≤ Te+0,5 𝑇 𝐿/2 =− 𝑃 𝐿 2 8∙𝑘∙𝑡 + 𝑃 𝐿 2 4∙𝑘∙𝑡 +𝑇𝑒=𝑇𝑒+0,5 𝑃 𝐿 2 8∙𝑘∙𝑡 +𝑇𝑒= 𝑇𝑒+0,5 𝑃 𝐿 2 8∙𝑘∙𝑡 =∆𝑇→𝐿= 8𝑘𝑡∆𝑇 𝑃 BWEC Cooling shell design B14
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Thermal simulations Out of scale
BWEC Cooling shell design B14
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Thermal simulations Out of scale
BWEC Cooling shell design B14
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Leakless mode Calorimeter Pressure Height Total static energy Losses
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