Cooling of GEM detector CFD-2012-03_GEM 2012/03/06 E. Da RivaCFD-2012-3_GEM1.

Slides:



Advertisements
Similar presentations
Conduction Conceptests
Advertisements

New Plate Baffle Water Flow. Quick Simulation Use triangular prism as rough estimate of a vane Uniform heat flux on each surface –600 kWm -2 on end face.
RFQ Cooling Studies.
RFQ End Flange Dipole Tuner Finger Cooling. Basis of Study Need multi-purpose end flange –Adjustable dipole mode suppression fingers –Beam current transformer.
As close to chemistry as we can get
Chapter 7 : Convection – External Flow : Cylinder in cross flow
122 Nov GTK Microchannel Cooling Hydraulic simulation with Rectangular Manifold Enrico Da Riva, Vinod Rao CERN (EN/CV/DC) 22 th Nov 2011 E. Da Riva,
UNIT 13 : HEAT 13.1 Thermal Conductivity 13.2 Thermal Expansion.
Extended Surfaces Chapter Three Section 3.6.
Extended Surface Heat Transfer
Chapter 2: Overall Heat Transfer Coefficient
Analysis of Simple Cases in Heat Transfer P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Gaining Experience !!!
M. Yoda, S. I. Abdel-Khalik, D. L. Sadowski and M. D. Hageman Woodruff School of Mechanical Engineering Extrapolating Experimental Results for Model Divertor.
Conduction & Convection.
Convection Prepared by: Nimesh Gajjar. CONVECTIVE HEAT TRANSFER Convection heat transfer involves fluid motion heat conduction The fluid motion enhances.
© 2011 Autodesk Freely licensed for use by educational institutions. Reuse and changes require a note indicating that content has been modified from the.
L 17 - Thermodynamics [2] Today’s topics –Practical thermal effects –Devices for temperature measurement –Mechanisms of heat transfer Science dealing.
RF-Accelerating Structure: Cooling Circuit Modeling Riku Raatikainen
Engineering Department ENEN 16/08/2013 LR - BBC Pre-Study 1 STATUS of BBC DESIGN and ENGINEERING : PRELIMINARY RESULTS G. MAITREJEAN, L. GENTINI.
STEADY HEAT TRANSFER AND THERMAL RESISTANCE NETWORKS
Steam Condenser II Prof. Osama El Masry
ISAT Module III: Building Energy Efficiency
1 Calorimeter Thermal Analysis with Increased Heat Loads September 28, 2009.
1 Denis Grondin / Julien Giraud – 01 December 2008 SLAB COOLING Denis Grondin Julien Giraud
Electric Current Electric current I is the rate of the flow of charge Q through a cross-section A in a unit of time t. One ampere A is charge flowing.
Calorimeter Analysis Tasks, July 2014 Revision B January 22, 2015.
20 th June 20111Enrico Da Riva, V. Rao Project Request and Geometry constraints June 20 th 2011 Bdg 298 Enrico Da Riva,Vinod Singh Rao CFD GTK.
Tbilisi, 10/07/2014V. Carassiti, P. Lenisa 1. Tbilisi, 10/07/2014V. Carassiti, P. Lenisa2.
July 4 th 20061Moritz Kuhn (TS/CV/DC/CFD) CERN July 4 th 2006 Moritz Kuhn Cooling of the P326 Gigatracker silicon pixel detector (SPIBES) CFD – Cooling.
Lesson 13 CONVECTION HEAT TRANSFER Given the formula for heat transfer and the operating conditions of the system, CALCULATE the rate of heat transfer.
One-Dimensional Steady-State Conduction
JCOV, 25 OCT 2001Thermal screens in ATLAS Inner Detector J.Godlewski EP/ATI  ATLAS Inner Detector layout  Specifications for thermal screens  ANSYS.
30 th June 20111Enrico Da Riva, V. Rao Parametric study using Empirical Results June 30 th 2011 Bdg 298 Enrico Da Riva,Vinod Singh Rao CFD GTK.
Consideration of Baffle cooling scheme
CLIC Prototype Test Module 0 Super Accelerating Structure Thermal Simulation Introduction Theoretical background on water and air cooling FEA Model Conclusions.
August 7, 2003K. Chow, LHC Luminosity Detector Thermal Analysis1 Analysis cases Approach: Start simple to get information— with speed with confidence that.
Heat Transfer from Extended Surfaces Heat Transfer Enhancement by Fins
Convection: Internal Flow ( )
Heat Transfer Equations. Fouling Layers of dirt, particles, biological growth, etc. effect resistance to heat transfer We cannot predict fouling factors.
CO 2 Cooling: Overview over CMS activities Jennifer Merz RWTH Aachen University, 1. Physikalisches Institut B May CEC General Meeting, Karlsruhe.
Overview WG4 Meeting - 16th October 20121M. Gomez Marzoa, E. Da Riva Maximum ΔT admissible at cooling system T_1 T_2 T_1+0.5*ΔT Stave  If T_2 – T_1 =
14th August E. Da Riva, A.L. Lamure CFD thermal simulations IBL Enrico Da Riva, Anne-Laure Lamure 14th August 2012.
1 Monophase Measurements on Prototype Pixel Structures D. Bintinger, M. Gilchriese, J. Taylor and J. Wirth and contributions from D. Cragg, E. Perrin and.
Simple CFD Estimate of End Flange Tuner Finger Cooling.
Cooling System Solutions
Chapter 3 Part 2 One-Dimensional, Steady-State Conduction.
M. Yoda, S. I. Abdel-Khalik, D. L. Sadowski, B. H. Mills and M. D. Hageman G. W. Woodruff School of Mechanical Engineering Correlations for Divertor Thermal-Hydraulic.
AAE 450 – Spacecraft Design Sam Rodkey 1 Active Thermal Control Design Sam Rodkey March 1 st, 2005 Project Management Project Manager.
E. Da Riva/M. Gomez Marzoa1 CFD Weekly Meeting - 3rd June 2012 ITS Upgrade: Cooling progress Enrico DA RIVA (EN-CV-PJ) Manuel GOMEZ MARZOA (EN-CV-PJ) 3.
E. Da Riva1 ITS Upgrade - Air cooling Layers Geometry Change!
E. Da Riva/M. Gomez Marzoa1 WG4 Meeting - 27th June 2012 Air Cooling by means of carbon fiber structure Enrico DA RIVA (EN-CV-PJ) Manuel GOMEZ MARZOA (EN-CV-PJ)
Pixel upgrade test structure: CO 2 cooling test results and simulations Nick Lumb IPN-Lyon MEC Meeting, 10/02/2010.
Simulation of heat load at JHF decay pipe and beam dump KEK Yoshinari Hayato.
Exercises for Q1. Insulated copper tube A thin walled 10 mm copper tube is used to transport a low-temperature refrigerant with a temperature that is.
TUTORIAL 1 7/3/2016.
24 September 2012 Immanuel Gfall (HEPHY Vienna) Annekathrin Frankenberger (HEPHY Vienna) SVD Status of Mechanics PXD-SVD Meeting Göttingen.
Lesson 7: Thermal and Mechanical Element Math Models in Control Systems ET 438a Automatic Control Systems Technology 1lesson7et438a.pptx.
Axion Relics Thermal – mechanical simulation for a flange UHV 114/63 1D with copper gasket
Aachen Status Report: CO2 Cooling for the CMS Tracker
CFD-Team Weekly Meeting - 8th March 2012
Ultra-light carbon fiber structures: evaporative tests
Detector Technology Group
Chapter Three Sections 3.1 through 3.4
Volvo V70R Brake Rotor Heat Transfer
Condensers.
Tests on a dummy facet of PIX upgrade using CO2 cooling
Heat Transfer from Extended Surfaces (Fins)
Thermal behavior of the LHCb PS VFE Board
PANDA Collaboration Meeting
Presentation transcript:

Cooling of GEM detector CFD _GEM 2012/03/06 E. Da RivaCFD _GEM1

1. Geometry and material properties E. Da RivaCFD _GEM2

Geometry and material properties Copper, k = 400 W m -1 K -1 PCB, FR-4, k = 0.25 W m -1 K -1 E. Da Riva3CFD _GEM A single chip is considered in the CFD simulations

Geometry and material properties Soldered = perfect thermal contact Gap-pad k = 2 W m -1 K -1 Chip, silicon, q = 1 W Water, T = 18°C All surfaces are adiabatic but the inner surface of the pipe E. Da Riva4CFD _GEM

Geometry and material properties Connector k = 0.27 W m -1 K -1 Volume including the GEM sensors is not taken into account. This surface is assumed as adiabatic. E. Da Riva5CFD _GEM

2. Schematic and estimations E. Da RivaCFD _GEM6

E. Da RivaCFD _GEM7 Schematic of the problem 18°C Water heat transfer coefficient T Cu strip TT Gap-padPCB T chip q = 1W T GEM PCB, connectors, etc. q = 0 W  The temperature of the GEM sensors will be the same as the PCB.  In order to reduce the sensor temperature, the thermal resistances must be reduced: -) higher water flow rate -> higher heat transfer coefficient -) shorter Cu strip or larger “cross section” -) Thinner gap-pad or higher thermal conductivity -) good thermal contact Cu strip/gap-pad and gap-pad/PCB

Water in the pipe E. Da RivaCFD _GEM8 Di [mm] Vel. [ms -1 ] Flow rate [kg s -1 ] Temp. rise [K] Re [-] HTC [Wm -2 K -1 ] Δp (2 m pipe) [bar] * * Heat load per VFAT chip = 1 W # VFAT chips = 30 Total heat load = 1 W * W = 34W * Erosion limit for copper pipe  Low water temperature rise is good to achieve a uniform sensor temperature.  The diameter of the pipe may be reduced if needed because of geometrical constraints.

3. Simulation results E. Da RivaCFD _GEM9

E. Da RivaCFD _GEM10 With water at 18°C, the temperature of the GEM sensor is expected to be around 60°C.

E. Da RivaCFD _GEM11 The dominant thermal resistance is due to the low PCB thermal conductivity and the small interface area between chip and PCB

E. Da RivaCFD _GEM12 The resistance due to water heat transfer coefficient is negligible (wall temperature very close to water temperature)

E. Da RivaCFD _GEM13 Schematic of the problem 2 18°C Water heat transfer coefficient T Cu strip TT Gap-padPCB T chip T GEM PCB, connectors, etc. Negligible~ 10 KDominant thermal resistance Increase heat contact area -) Increase Cu thickness -) Increase Cu width

E. Da RivaCFD _GEM14 Conclusions The dominant thermal resistance is between the chip and the PCB Direct thermal contact between the copper strip and the chip may be needed (putting the chip above the PCB instead of below?) A further step may be increasing the thickness and the width of the copper strip The diameter of the pipe may be slightly reduced if needed.