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1 VI Single-wall Beam Pipe tests M.OlceseJ.Thadome (with the help of beam pipe group and Michel Bosteels’ cooling group) TMB July 18th 2002
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TMB: CERN June 2002 M.Olcese – J.Thadome2 Double Vs. Single Wall Design Same heater Same outer envelope Same reflective layer (moved outside)
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TMB: CERN June 2002 M.Olcese – J.Thadome3 Proposed thermal insulation Nano-porous Silica Aerogel in flexible quartz fiber carrier Very low thermal conductivity: 10-12 mW/mK @ Tamb Very low density: 0.09-0.12 g/cm3 Radiation length: 250 cm (worst density) Resistant up to 600 °C Contains: mostly inert materials Si oxides, quartz fibers, not sensitive to irradiation Two available types from Aspen Aerogels: White grade (Pyrogel UQS) Black grade (Pyrogel CQS): carbon opacified to minimize the radiation at high temperature
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TMB: CERN June 2002 M.Olcese – J.Thadome4 Thermal conductivity vs. T The thermal conductivity of the Carbon opacified type does not change in the temperature range we are interested in Carbon opacified type is apparently also more stable in terms of aerogel powder release However it contains small quantities of carbon which in case of failure of the encapsulation might have a bad impact on the pixel detector
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TMB: CERN June 2002 M.Olcese – J.Thadome5 Local effects and beam pipe offset Conduction and radiation are uniform in , while the convective heat flux varies significantly with his is due to the non symmetric flow pattern in the gap I have found an article on an experimental study in equivalent conditions (in terms of characteristic dimensionless Ra number). The proposed correlations lead in our case to a max local heat flux 2.6 times higher than the average (on the top). Other experimental studies show that the influence of the beam pipe offset up to 5 mm produce a change of both the average and local heat flux of less than 10% The worst case heat flux, which the top B-layer stave will have to dissipate during the bake out is 10 W (9% of nominal cooling capacity) conclusion
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TMB: CERN June 2002 M.Olcese – J.Thadome6 Thermal tests on real scale mockup 1 m long tube with deposited heater Two layer of Aerogel UQS (total Aerogel thickness of 5-6 mm) with aluminized kapton encapsulation (total thickness of insulation package 9 mm) External cylindrical heat exchanger to simulate the B-layer structure (black internal surface to maximize radiation) Tube cooled and maintained at a uniform temperature Insulating plug Beam pipe with heater and insulation Tube was heated up to 250 ° C and as function of the outer tube temperature we measured: the required heating power (heat dissipated by the B-layer + losses) The temperature distribution on the outer surface of the insulation 1000 mm
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TMB: CERN June 2002 M.Olcese – J.Thadome7 Experimental setup Heat exchanger Monophase C6F14 cooling unit Beam pipe mockup Detail of aluminized kapton encapsulation fridge readout
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TMB: CERN June 2002 M.Olcese – J.Thadome8 Test results Equivalent thermal conductivity of insulation package is 75% above the Aerogel expected value (from vendor data sheet): air gaps, radiation? Measured heating power is about 35% more than what was expected but this includes the heat losses difficult to estimate correctly The heating power increases only by 10 % for a B-layer temperature change of 10 ° C
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TMB: CERN June 2002 M.Olcese – J.Thadome9 Temperature distribution vs. offset Positive vertical offset does not show significant changes in temperature distribution In case of negative vertical offset the mid and bottom temperatures are lower This is confirmed by the measurements of the total heating power which in case of negative vertical offset is about 4% higher and it is also in agreement with literature Beam pipe Temperature sensor insulation top mid bottom 5 mm vertical positive offset
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TMB: CERN June 2002 M.Olcese – J.Thadome10 Extrapolation to proposed design Extrapolation from measurements leads to a max power of about 200 W/m Worst stave position (top) would require a coolant T of – 8 ° C to keep the whole module below 0 ° C ° -8 ° C ° - 4 ° C ° 0 ° C 1.5 W/module (top stave) (15% nominal cooling capacity) Flex hybrid sensor FE stave Cooling tube
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TMB: CERN June 2002 M.Olcese – J.Thadome11 New irradiation studies A sample of Aerogel UQS has been bent at the beam pipe radius and irradiated up to a dose of 5x10 15 pt/cm 2 It has a negligible contact activation dose The irradiated area of the sample does not show any visible mechanical degradation (cannot be distinguished from the non irradiated one)
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TMB: CERN June 2002 M.Olcese – J.Thadome12 Remarks The installation of the Aerogel around the beam pipe is not easy The aerogel material is wavy and shows significant non-uniformities The Aerogel cannot be glued : has to be hold in place by the kapton encapsulation Need to find a better technical solution and to make more practice
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TMB: CERN June 2002 M.Olcese – J.Thadome13 Next steps check thermal conductivity of last irradiated sample at higher dose (Sept.) Make vibration tests on thermal mockup (with a conservative spectrum) and repeat the thermal tests to check possible loss of thermal performances due to aerogel powder migration (Oct.) Make same vibration tests on the irradiated sample and measure again the thermal conductivity (Oct.) Assess installation methods including encapsulation Study design changes to be incorporated in the current baseline: redesign the support collars, assess the design impact on the wire supports Make a full VI section prototype?? I can manage I can help
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