W. EbensteinDOE annual review Duke UniversitySeptember, 1998 TRT Barrel Cooling: Electronics  Motivation: u Overheating of electronics causes premature.

Slides:



Advertisements
Similar presentations
Michael Hoch / EP-AIT1 TPC Resistor Rod. Michael Hoch / EP-AIT2 Resistor Chain: Design Constrains  current per resistor chain: 241  A = 25W (total =
Advertisements

So Far: Conservation of Mass and Energy Pressure Drop in Pipes Flow Measurement Instruments Flow Control (Valves) Types of Pumps and Pump Sizing This Week:
MECHANISM OF HEAT TRANSFER Mode of Heat transfer Conduction Convection
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 !!!
PRR TRD COOLING A. Marín (GSI) 7/01/2004 ALICE PRR TRD COOLING P.Glässel, A.Marín, V.Petracek, J.Stachel, M.R.Stockmeier, J.P.Wessels ALICE PRR TRD COOLING.
CHE/ME 109 Heat Transfer in Electronics LECTURE 7 – EXAMPLES OF CONDUCTION MODELS.
HEAT TRANSFER IN LIGHTSABERS An ME 340 Project by Clayton Grames.
Heat Transfer Rates Conduction: Fourier’s Law
HEAT EXCHANGER.
FAZIA DAYS, Bologna 10-12/feb/2010, WG8, Emanuele Vanzanella (mechanics & cooling), Alfonso Boiano (electronics) ELECTRONICS HOLDER & COOLING SYSTEM Side.
ISAT Module III: Building Energy Efficiency
W. EbensteinDOE Review Duke UniversitySeptember 1999 TRT Barrel Cooling: Electronics  Motivation: u Overheating of electronics causes premature failure.
Thomas Jefferson National Accelerator Facility Page 1 IPR October Independent Project Review of 12 GeV Upgrade Jefferson Lab October 18-20,
November 16, 2001 C. Newsom BTeV Pixel Modeling, Prototyping and Testing C. Newsom University of Iowa.
, T. Tischler, CBM Collaboration Meeting, GSI Status MVD demonstrator: mechanics & integration T.Tischler, S. Amar-Youcef, M. Deveaux, D. Doering,
W. Ebenstein Duke University Barrel Cooling  Thermally Conductive Epoxies: (samples sent to Anatoli) Vendor : Epoxies, etc. (Cranston, RI)  :
Tbilisi, 10/07/2014V. Carassiti, P. Lenisa 1. Tbilisi, 10/07/2014V. Carassiti, P. Lenisa2.
ATLAS TRT Barrel Design Review, 1998 Barrel TRT Electronics Cooling Chiho Wang Duke University.
VG1 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Upgrade Stave Study Topics Current Analysis Tasks –Stave Stiffness, ability to resist.
BTeV Pixel Substrate C. M. Lei November Design Spec. Exposed to >10 Mrad Radiation Exposed to Operational Temp about –15C Under Ultra-high Vacuum,
JCOV, 25 OCT 2001Thermal screens in ATLAS Inner Detector J.Godlewski EP/ATI  ATLAS Inner Detector layout  Specifications for thermal screens  ANSYS.
Consideration of Baffle cooling scheme
November 12, 2001 C. Newsom BTeV Pixel Modeling, Prototyping and Testing C. Newsom University of Iowa.
Convection: Internal Flow ( )
Chiho Wang Duke University 1 TRT Barrel integration Status / Schedule Chiho Wang.
1 VI Single-wall Beam Pipe Option: status and plans M.Olcese TMB June 6th 2002.
13.2 Transferring Thermal Energy I.Transfer of Energy A.Conduction-transfer of energy by direct contact. 1.Faster moving particles of one substance come.
Thermal Model of Pixel Blade Conceptual Design C. M. Lei 11/20/08.
13.2 Transferring Thermal Energy. I. Transfer of Energy A.Conduction-transfer of energy by direct contact.
Chiho Wang ATLAS TRT Krakow Workshop Duke University May, HV Plate Design & Assembly Chiho Wang Duke University.
Spacing of Cu clamp = 10” Clamp plate width = 2.5”, thickness = 0.375” Thickness of conductor insulation = 0.03” Thickness of coil ground wrap = 0.03”
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.
Chiho Wang ATLAS TRT Duke University IU, Oct Fuse Box Design & Mounting Chiho Wang Duke University.
How much makes it through the atmosphere. Why a seasonal variation? First, why do we have seasons? Earth’s axis is tilted 23.5° to the plane of its orbit.
Pixel upgrade test structure: CO 2 cooling test results and simulations Nick Lumb IPN-Lyon MEC Meeting, 10/02/2010.
Chiho Wang ATLAS TRT Barrel Duke University U. Penn. Workshop, 2000 Module Thermal Analysis Chiho Wang Duke University.
Chiho Wang ATLAS TRT Duke University CERN, Sep Barrel integration status.
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.
EMC BWE Proto18 - Orsay Meeting 1 PANDA EMC BWE Proto18 Mikel Catania Goikoetxea, Javier Navarro Medrano, David Rodríguez Piñeiro, Yue Ma, Frank.
Thermal Energy Chapter 6. Describe things you do to make yourself feel warmer or cooler.
INDEX Sr noTopic 1.Introduction 2.Advantages 3.Product Types 4.Thermal Insulating Materials 5.Applicatiion.
Heat Transfer by Convection
Professor Eduardo Cabrera
7 February 2012 Annekathrin Frankenberger (HEPHY Vienna) Open CO 2 Cooling System at the beam test Belle II SVD-PXD Meeting.
ATLAS TRT Duke University CERN, Feb Fuse Box Status Duke University.
Chapter 5 – Thermal Energy
Heat Transfer.
Che 451 chemical engineering design i HEAT EXCHANGER DESIGN
Status of GASPARD mechanics
The EMC cooling F. Raffaelli INFN - Pisa 06/09/2017.
HEAT EXCHANGER DESIGNPROJECT ME 414 Thermal Fluid System Design
Prof. Marlon Flores Sacedon
Barrel TRT Module Cooling
Heat and Mass Transfer Heat is ……… Heat Transfer ……
ECE Engineering Design Thermal Considerations
FP420 Detector Cooling Thermal Considerations
Heating and Cooling, the art of Thermal Energy
Thermal energy Chapter 4.
Condensers.
Chapter 16 Temperature and Heat.
Tests on a dummy facet of PIX upgrade using CO2 cooling
Heat transfer Chapter 7.
Hot to Cold Song.
Chapter 7 Chapter 4 in Old Textbook – pg. 115
Hot to Cold Song.
**Plate Tectonics: How did it happen?**
THERMODYNAMIC IN ELECTRONICS
13.2 Transferring Thermal Energy Transfer of Energy
Chapter 6 Thermal energy.
Presentation transcript:

W. EbensteinDOE annual review Duke UniversitySeptember, 1998 TRT Barrel Cooling: Electronics  Motivation: u Overheating of electronics causes premature failure  Requirements: u 60 mW per channel u Total for type 1(inner) module ~ 20 W u Want operating T < 50 ºC  Cooling Plan: u Heat generated by IC u through stamp board/banding u through legs/sockets u into cooling plate u to mounting channel/tubing u to cooling fluid

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Current Duke Prototype: u Aluminum cooling plate/tubing u tension plate u insulated box u additional sensors/readout

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  From Lund: u ASDBLR & DTMROC dummy boards (pictured here) u Roof boards u Readout and display software

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Results of tests: (coolant at 14 ºC) u 1.3 mm cooling plate + all sockets:  ASDBLR: 46 ºC  DTMROC: 48 ºC  roof boards: 38 ºC  cooling, tension plates: ~ 27 ºC u (Typical range: ± 2 ºC)

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Remaining issues/improvements: u Mass production of tubing u Attachment of tubing/channel u Heat transfer banding/legs/sockets u Replacement of aluminum cooling plate by pyrolytic graphite (PG):  Motivation: Need to reduce material to get acceptable radiation length

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Properties of PG material: u Made by pyrolysis of hydrocarbon gases in a vacuum furnace u Thermal conductivity(in-plane):  PG ~ 400 W/m-K  compare: Cu ~ 400, Al ~ 200 u Expensive  ~ $150k for barrel (PG)  ~ $ 50k with aluminum u Machinability / gluing?  We are exploring

W. EbensteinDOE annual review Duke UniversitySeptember, 1998 TRT Barrel Cooling: Module  Motivation: u Uniform temperature needed inside module for optimum TR function  Requirements: u Type 1 module heating is ~ 7.5 Watts u Want T gradient < 7 ºC  Cooling Plan: u Cooling fluid (same as electronics cooling) flows in tubing running full length of module u Tubing makes good contact inside shell at two opposite corners u Shell has good thermal conductivity ( W/m-K)

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Calculation by BNL: u  T = 8.6 ºC

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Duke experimental studies: u Put real module in insulated box u Heat module with current through straws u Flow cooling water at 24 ºC u Measure T with small thermistors inside module and attached to outside of shell

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Module cooling test chamber:

W. EbensteinDOE annual review Duke UniversitySeptember, 1998  Results of experiments: u  T ~ 10 ºC