end-cap mechanics fdr cooling structures
DESCRIPTION
End-cap Mechanics FDR Cooling Structures. Steve Temple, RAL. 1 November 2001. End-Cap Disc Services Cooling Structures. Full details - See ATL-IS-ER-0021 Cooling Circuit Layout 3 circuits per quadrant - corresponding to inner, middle and outer module rings - PowerPoint PPT PresentationTRANSCRIPT
CLRC 1S Temple
End-cap Mechanics FDRCooling Structures
Steve Temple, RAL
1 November 2001
CLRC 2S Temple
End-Cap Disc ServicesCooling Structures
Full details - See ATL-IS-ER-0021 Cooling Circuit Layout
» 3 circuits per quadrant - corresponding to inner, middle and outer module rings
» 3 separate Inlets, 3 outlets are manifolded at patch panel
» Outer and middle module Circuits - Two point cooling
» Inner module circuit - Single point cooling
» Bend radii (inner) kept to 5 times OD i.e. 18.7 mm
Cooling Component Materials/Joining Techniques» C-C cooling blocks
» CuNi pipe - 3.6mm ID, 70 µm Wall
» Cu plating (sputter coat + electroplate) of cooling blocks enables soft soldering to cooling pipe
CLRC 3S Temple
Mechanical Requirements» Position modules to a positional tolerance of 134 microns
(diameter) in the R-phi direction, for one module relative to its neighbour
» Provide co-planar mounting surfaces for modules» Minimise forces transferred to the support structure i.e. carbon
fibre disc» Operational for 10 years» Lowest possible mass
Thermal Requirements» To ensure the highest temperature of any part of the silicon on
a module doesn’t exceed -7 °C
End-Cap Disc ServicesCooling Structures
CLRC 4S Temple
Cooling Pipe Circuit Design» CuNi material chosen for its excellent resistance to corrosion, and its excellent
solderability
» ‘Wiggly’ pipe Layout reduces forces on disc from thermal contractions and pipe manufacturing tolerance
– Thermal Contraction Forces
Forces calculated using an FE model, using following material properties and boundary conditions :
E=152 GPa, = 12e-6/K, T=50K
– Pipe Manufacturing Tolerances
Deviation of pipe bend centres from nominal positions kept to a minimum, through tooling design
In addition stress relieving of manufactured circuits is proposed - testing is planned in next round of prototyping
End-Cap Disc ServicesCooling Structures
CLRC 5S Temple
ANSYS 5.5.3SEP 23 200114:37:31PLOT NO. 1DISPLACEMENTSTEP=1SUB =1TIME=1PowerGraphicsEFACET=1AVRES=MatDMX =.101142
1
NFOR
DSCA=105.01ZV =1DIST=114.691XF =-157.26YF =294.168ZF =-7.5Z-BUFFER
pipes_inner.asm
1.10 N
0.42 N
0.34 N
0.03 N
0.11 N
0.06 N
0.16N0.08 N
1.42 N
0.38 N
33.3 Nmm
8.7 Nmm
19.3 Nmm
18.4 Nmm21.2 Nmm
Inner Circuit
End-Cap Disc ServicesCooling Structures
CLRC 6S Temple
ANSYS 5.5.3SEP 23 200115:21:39PLOT NO. 1DISPLACEMENTSTEP=1SUB =1TIME=1PowerGraphicsEFACET=1AVRES=MatDMX =.077029
1
NFOR
*DSCA=100ZV =1*DIST=128.989*XF =103.967*YF =-471.282*ZF =.127957Z-BUFFER
td-1002-337.igs
15.8 Nmm
1.98 N
0.06 N
0.07 N
0.05 N
0.02 N
0.08 N
0.40 N
0.03 Nmm
2.60 N1.43 N
11.71 N
0.8 N
0.03 N
12.04 N
17.5 Nmm
17.5 Nmm
9.4 Nmm
74.3 Nmm 6.4 Nmm
22.4 Nmm
Outer Circuit
End-Cap Disc ServicesCooling Structures
CLRC 7S Temple
ANSYS 5.5.3SEP 23 200116:03:33PLOT NO. 1DISPLACEMENTSTEP=1SUB =1TIME=1PowerGraphicsEFACET=1AVRES=MatDMX =.100441
1
NFOR
*DSCA=100ZV =1*DIST=164.153*XF =-375.285*YF =162.547*ZF =5.479Z-BUFFER
pipes_middle_asm.igs
0.16 N
10.8 Nmm
2.53 N8.1 Nmm
0.08 N
0.17 N
0.12 N
0.07 N
0.39 N
0.03 N
4.35 N
1.84 N
27.16 N
0.16 N
27.08 N
23.8 Nmm
22.6 Nmm
108 Nmm
13.5 Nmm
43.6 Nmm
0.01 N
Middle Circuit
End-Cap Disc ServicesCooling Structures
CLRC 8S Temple
Cooling Pipe Prototyping» First prototype - Inner cooling
circuit for system test» Old circuit design - Internal
bend radii of 14mm» Ice used as filler material» Custom made pipe bender
designed and manufactured» Manufactured at RAL
End-Cap Disc ServicesCooling Structures
CLRC 9S Temple
Cooling Pipe Prototyping (Cont’d)» Second prototype - Single U
shaped bend» Internal bend radii of 20mm - 5
x OD» Cerobend used as filler material» Swaged ends - enables low
mass joining of pipes» Manufactured by established
pipe bending company
End-Cap Disc ServicesCooling Structures
CLRC 10S Temple
Cooling Block Design» Primary Cooling Block
Thermal Design– C-C material chosen for good thermal conductivity - 300 W/m2K
(fibre direction), 50 W/m2K (transverse direction)– Fibre orientation optimised– Straight split corresponding to hybrid and silicon – Further details see thermal performance
Mechanical Design– Machined module location boss– Planar module mounting surface wrt block mounting surface– Accurate cooling block height
End-Cap Disc ServicesCooling Structures
CLRC 11S Temple
Cooling Block Design (Cont’d)» Second Point Cooling Blocks
Thermal Design– C-C material chosen for good thermal conductivity - 300 W/m2K (fibre
direction), 50 W/m2K (transverse direction)– Fibre orientation optimised
Mechanical Design– As primary cooling block
» Second Point Mounting Blocks
Thermal Design– No thermal requirements - Made from low mass PEI polymer
Mechanical Design– As primary cooling block
End-Cap Cooling StructuresCooling Block Design
CLRC 12S Temple
Cooling Block Prototyping» Two prototyping exercises
(old and current design)» Several manufactured,
metrology checked to assess ability to machine key features within appropriate tolerances
– 3mm OD location boss– Parallelness between
bottom and top surfaces– Block height dimension
End-Cap Cooling Structures
Cooling Block Design
CLRC 13S Temple
End-Cap Disc ServicesCooling Structures
Cooling Block Prototyping (Cont’d)» Current cooling block design metrology results
» Improvements to design for machining operations
simplification identified
CLRC 14S Temple
Joining of C-C Blocks to Cooling Pipe» Soldering of cooling blocks to pipe
– Good thermal joint– Good mechanical joint - Soldered joint sample (using swaged end)
undergone helium vacuum leak test – Standard SnPb (60/40) solder with non-corrosive Castolin 197 flux.– Requires Cu plating of C-C block
» Cu Plating of C-C Blocks– Plating trials show good adhesion to C-C base material achieved
by :
Cleaning, Cu Sputtering, Cu Electroplating and Au Flash (to prevent copper oxidisation)
– 15 micron Cu plating followed by 2 micron Au flash
End-Cap Disc ServicesCooling Structures
CLRC 15S Temple
Cooling Structure Precision Assembly» To achieve positional
tolerances required a precision assembly technique is performed during the disc services to disc assembly stage
» This involves a precision rotary stage (r-phi) and an alignment arm (providing radial position)
» Details see ATL-IS-ER-0022
End-Cap Disc ServicesCooling Structures
CLRC 16S Temple
Cooling Structure Precision Assembly (Cont’d)» Blocks are required to be positioned in r-phi with a positional
tolerance of 66 microns - Out of 134 micron error budget» Results show this is readily achievable using this method
End-Cap Disc ServicesCooling Structures
CLRC 17S Temple
Thermal Performance» Extensive prototype testing and thermal simulation carried
out on the Baseline Design (see ATL-IS-ER-0009) – Full cooling quadrant (3 circuits) manufactured and tested
on evaporative cooling rig
– Dummy thermal module mounted on sector and tested
– Successfully demonstrated a coolant temperature of -20 to -22 °C was sufficient to keep the inner module below -7 °C.
– Design consisted of Aluminium Alloy cooling blocks joined to Aluminium cooling pipes.
– Effect of material changes therefore need to be assessed
End-Cap Disc ServicesCooling Structures
CLRC 18S Temple
Thermal Performance (Cont’d)» Assessment of cooling block
material change– C-C block substituted into
the simulation. Again boundary conditions - 4000 W/m2K @ -20C (7.5 W, 1W)
– Minimal change on silicon side. Better performance on hybrid side.
ANSYS 5.5.3SEP 18 200110:28:30PLOT NO. 1NODAL SOLUTIONSTEP=1SUB =1TIME=1TEMP (AVG)RSYS=0PowerGraphicsEFACET=1AVRES=MatSMN =-19.998SMX =-8.456
1
MN
MXX
Y
Z -19.998-18.716-17.433-16.151-14.868-13.586-12.303-11.021-9.738-8.456
CC Cooling Block - Temperature Plot - 4000W/m2K @ -20C
Al Tsil=-11.5°CC-C Tsil=-11.3°C
Al THyb=-6.9°CC-C THyb=-8.4°C
End-Cap Disc ServicesCooling Structures
CLRC 19S Temple
Thermal Performance (Cont’d)» Assessment of cooling pipe material change
– Reduction in thermal conductivity and wall thickness results in reduction of convective heat transfer area.
– However as htc increases with heat flux, this effect will be decreased.
– Small scale prototype testing on an evaporative C3F8 cooling rig is planned
End-Cap Disc ServicesCooling Structures