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Transient Plane Source Techniques for measuring Thermal Conductivity of Various Materials Evitherm September 15, 2003 Dr. Lars Hälldahl Hot Disk AB

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  • Transient Plane Source Techniques for measuring Thermal Conductivity of Various MaterialsEvitherm

    September 15, 2003

    Dr. Lars HlldahlHot Disk AB

  • Hot Disk

    or

    Transient Plane Source, TPS

    or

    Gustafsson Probe

    or

    G-Probe

  • The technique is based around:-A unique sensorA new mathematical model for thermal conductivityA Transient Plane Source in infinite material- Special electronics to collect dataDesigned for accuracy and precision

  • The SensorA double spiral made of Nickel metal foil, cladded by Kapton or Mica to provide electrical insulation from the sample. The diameter varies from 1 mm up to 60 mm. It connects to the electronics, which sends out a current during a selected time, while the voltage drop is recordedSee in the following four slides the historical development of Hot Diskfrom Hot Wire Hot Strip !

  • Hot Wire

    About 1960-tiesMetal wire in contact with the sampleOK for liquids, but not for solids contact resistance problems

  • Hot Strip

    Development of Hot Wire the wire.flattened outbetter contact on sample

  • From a Strip..to a spiralcovers larger area on smaller sample

  • So.the story is

    from

    Hot Wire

    to

    Hot strip

    and next stepTransient Plane SourceThis is Hot Disk

  • Sensor embedded in the sample. Heat can spread in all directions

  • A transient recordingPowerTimeTimeVoltage=resistance=temperatureSend in power...and measure at the same timeFor good conductors:high power, short timeFor good insulators: low power, long time

  • Ideally, the sensor is surrounded by infinite sample in all direction. Cant see the edge, the temperature increase doesnt reach the edges.Both Conductivity and Diffusivity are measured, and from them Heat Capacity is calculatedHeat dissipation in infinite sample

  • Sample

    Parameters of importance: POWER, TIME SENSOR SIZE The relation between Diffusivity, Time for measurement and radius of sensor is called Total to Characteristic Timex tr x r

    SampleSensor=1This value between 0.3 1.0 satisfies the basic assumption done for the Heat Conductivity equation: A Plane Source in Infinite Material

  • Variants of the TPS methodBy varying sensor size, power and time in the basic method, thermal conductivity over morethan 4 orders of magnitude can be covered.To cover more applications, some variants have been developed

  • Thin Film MethodSamples like paper, textile, cloth, polymer films, etc.Background material

    Sample Sensor Sample

    Background materialThickness from ~ 10m ~ 500m Conductivity from ~ 0.01W/mK ~ 10W/mKBackground material is good conductor, experiment parameters as if this is the sample: high power, short time

  • Thin Film often uses a square, naked Ni-sensorwhich is most sensitive, but also cladded sensors can be used

  • Slab MethodInsulator

    SampleSensorSample

    InsulatorFor good conductors, >10 W/mK- Ceramic, metals, Si-wafer, SiC. Etc.Relation between Sample Thickness/Sensor radius 0.03 < t/R < 0.75 - Different radii to match different samples

  • Developing Slab Method-Air is very insulating

  • Anisotropic samplesRadial directionConductvityDiffusivity

    Axial directionConductivityDiffusivityTo solve the heat conductivity equation in this case: Heat Capacity Cp must be known!

  • Anisotropic sampelsTensile testing bars, polymer matrix with fiber reinforcement in the plan. Thickness2 mm.

  • radial W/mK axial W/mK radial mm2/s axial mm2/s mm2/s W/mK

    Diagr1

    0.1060505330.08107838910.23005423070.1758824394

    0.09393397590.06523192770.3021892040.2098536139

    0.10433047190.07235122880.35020875380.2428632134

    laxial [W/mK]

    kaxial [mm2/s]

    lradial [W/mK]

    kradial [mm2/s]

    % Fiber

    l [W/mK] k [mm2/s]

    Results

    Results :Dragprov5%Number of Rows:9

    File:(Points)TemperatureAx.Th.ConductivityAx.Th.DiffusivityRad.Th.ConductivityRad.Th.DiffusivityAx.Pr.DepthRad.Pr.DepthTemp.Incr.Temp.DriftTotal/Char.TimeTime Corr.Mean Dev.Disk Res.

    Dragprov_1procent. 1.ani( 13- 200,tc)Rumstemp 23 deg. C0.10671190880.08158402820.2277899990.17415137541.8029458632.63416859942.00744473260 (No corr.)0.32396674790.06818926980.00100373132.4391883427

    Dragprov_1procent. 2.ani( 11- 200,tc)Rumstemp 23 deg. C0.10605698050.08108331840.23029433350.17606600421.79740469322.64860910782.09159920410 (No corr.)0.32752845430.06493702220.00097298832.4395240383

    Dragprov_1procent. 3.ani( 12- 200,tc)Rumstemp 23 deg. C0.10538270970.08056782080.23207835960.17742993851.79168196752.6588483352.05306347030 (No corr.)0.33006572620.05998533730.00091250942.4396604686

    Average0.10610.08110.2300.176

    Stdev0.00070.00050.0020.002

    Stdev %0.60.60.90.9

    Dragprov_2p5procent. 3. 1.ani( 17- 200,tc)Rumstemp 23 deg. C0.09324416070.06475288940.30342819120.21071402171.60623723812.89752260081.80809214650 (No corr.)0.39198275750.05979339940.00101941492.438608362

    Dragprov_2p5procent. 3. 2.ani( 12- 200,tc)Rumstemp 23 deg. C0.09404777620.06531095570.30220465070.20986434081.61314398682.89167473071.98973895020 (No corr.)0.39040213060.06888370750.00101089392.4393531958

    Dragprov_2p5procent. 3. 3.ani( 13- 200,tc)Rumstemp 23 deg. C0.09450999090.06563193810.30093476990.20898247911.6171031712.88559284541.94656121280 (No corr.)0.38876163910.07376207880.00079178132.4392357993

    Average0.09390.06520.3020.2099

    Stdev0.00060.00040.0010.0009

    Stdev %0.70.70.40.4

    Dragprov_5procent. 1.ani( 10- 200,tc)Rumstemp 23 deg. C0.1045385730.0724955430.34973895670.2425374181.69955712943.10863325781.86091427340 (No corr.)0.45118253230.0498447190.00100174862.4372097143

    Dragprov_5procent. 2.ani( 10- 200,tc)Rumstemp 23 deg. C0.10415165130.072227220.3506127290.24314336271.69640898463.11251407131.8625816620 (No corr.)0.45230974680.05003665690.00086337312.4375126291

    Dragprov_5procent. 3.ani( 12- 200,tc)Rumstemp 23 deg. C0.10430119130.07233092330.35027457560.24290885961.69762639233.1110127551.78420769760 (No corr.)0.45187351020.0498447190.00085680182.4377487672

    Average0.10430.07240.35020.2429

    Stdev0.00020.00010.00040.0003

    Stdev %0.20.20.10.1

    Outp.power.Meas.timeSp.heat SampleRadius

    Dragprov_1procent. 1.ani0.02101.3082.001

    Dragprov_1procent. 2.ani0.02101.3082.001

    Dragprov_1procent. 3.ani0.02101.3082.001

    Dragprov_2p5procent. 3. 1.ani0.02101.442.001

    Dragprov_2p5procent. 3. 2.ani0.02101.442.001

    Dragprov_2p5procent. 3. 3.ani0.02101.442.001

    Dragprov_5procent. 1.ani0.02101.4422.001

    Dragprov_5procent. 2.ani0.02101.4422.001

    Dragprov_5procent. 3.ani0.02101.4422.001

    laxial [W/mK]kaxial [mm2/s]lradial [W/mK]kradial [mm2/s]Cp [MJ/m3K]

    1Sample 1%Average0.10610.08110.2300.1761.308

    2.5Sample 2.5%Average0.09390.06520.3020.20991.44

    5Sample 5%Average0.10430.07240.35020.24291.442

    &A

    Page &P

    Results

    0000

    0000

    0000

    laxial [W/mK]

    kaxial [mm2/s]

    lradial [W/mK]

    kradial [mm2/s]

    % Fiber

    l [W/mK] k[mm2/s]

    Parameters

    Parameters :Dragprov5%Number of Rows:9

    File:TemperatureOutp.power.Meas.timeSp.heat SampleRadiusTCRDisk TypeTemp.drift rec.

    Dragprov_1procent. 1.aniRumstemp 23 deg. C0.02101.3082.0010.004693KaptonYes

    Dragprov_1procent. 2.aniRumstemp 23 deg. C0.02101.3082.0010.004693KaptonYes

    Dragprov_1procent. 3.aniRumstemp 23 deg. C0.02101.3082.0010.004693KaptonYes

    Dragprov_2p5procent. 3. 1.aniRumstemp 23 deg. C0.02101.442.0010.004693KaptonYes

    Dragprov_2p5procent. 3. 2.aniRumstemp 23 deg. C0.02101.442.0010.004693KaptonYes

    Dragprov_2p5procent. 3. 3.aniRumstemp 23 deg. C0.02101.442.0010.004693KaptonYes

    Dragprov_5procent. 1.aniRumstemp 23 deg. C0.02101.4422.0010.004693KaptonYes

    Dragprov_5procent. 2.aniRumstemp 23 deg. C0.02101.4422.0010.004693KaptonYes

    Dragprov_5procent. 3.aniRumstemp 23 deg. C0.02101.4422.0010.004693KaptonYes

    &A

    Page &P

    T-t

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    T(drift)

    Temperature drift graph :Number of Columns:0

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    &A

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    Temperature-f(Tau) graph :Number of Columns:0

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    Diff

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  • Single sided methodIf you do not want to cut your precious sampleput the sensor on the surface..and back it up with a known sample. Tell the software the properties of the known, and run the analysis as before.In principal, the more similar, the better

  • In Transient Methods, like Hot Disk, the contact resistance does not cause any problem.

    This is not the case with Steady State Methods, wherethis is a limitation for the use.

    The following slides explains how Contact resistanceis dealt with, and gives an illustrative example.

  • Ideally, the sensor is surrounded by infinite sample in all direction. Contact areaTemp CTime sCut off here!

  • Ideally, the sensor is surrounded by infinite sample in all direction.

    If this should occur, the later part of the raw data are removedCut off here!Temp CTime s

  • Measuring coated and uncoated ceramicsVaristors made of ZnO ceramicsuncoated surfacesurface coated by Al-metal, 60m thickMeasuring with same conditions sensor, time, power,temperature

  • It seems like the Al-metal coating was insulating?A metal like Al ?In this case the sprayed metal was very porous. The conductivity was about 0.5 W/mK60m of porous metal added to the kapton coating increases the temperture about 4 times!

  • Some resultsGreen Metal Coated W/mK std % W/mk std% 23 C 24.70 (0.2) 24.69 (0.8) 300 C 12.67 (2.2) 13.36 (0.8) Sensor radius 6.675 mmSensor radius 14.65 mm23 C 24.71 (0.8) 24.88 (1.0) 300 C 12.19 (1.3) 13.08 (0.4) Mica sensorKapton sensorMica sensorMica sensor

  • Constant T after initial period

    Thin film making use of contact resistance

    Temp. vs time without sample

    Temp. vs time with sample

    Temp

    Time

  • Measuring liquids-vertical sensor-low power-short timeto avoid convectionPut it in a heating/cooling bath, and run at different temperatures- liquids with a viscosity as low as water and methanol can be measured

  • Sheet1

    -350.3007

    -200.33110.2515

    00.37230.5379

    00.5271

    250.6191

    250.6366

    400.44310.711

    800.51880.90440.3127

    1000.3605

    Sheet1

    Mix Gly/Water

    Water

    Pure Glycol

    Temp C

    W/mK

    Conductivity

    Sheet2

    -350.11442.6208

    -200.10982.2910.12322.6894

    00.13092.8490.15123.5572

    00.14553.64

    250.16743.7058

    250.17953.5487

    400.13763.2220.20653.445

    800.08933.5040.14993.46940.27983.2392

    1000.11243.207

    Sheet2

    000

    000

    000

    000

    000

    000

    000

    000

    000

    Glycol

    Mixture

    Water

    Temp C

    mm2/s

    Diffusivity

    Sheet3

    Sheet3

    -352.6208-35

    2.2912.6894-20

    02.8493.5572

    003.64

    25253.7058

    25253.5487

    403.2223.445

    3.5043.46943.2392

    3.207100100

    Cp Glycol

    Cp Mixture

    Cp Water

    Temp C

    MJ/m3K

    Heat Capacity

  • Pure water:

    Temperature Time Conductivity std Diffusivity std Heat Capacity std C s W/mK % mm2/s % MJ/m3K % 0 5 0.538 0.4 0.151 1.7 3.56 1.3 0 2.5 0.530 0.8 0.146 1.9 3.64 1 25 see A 2.5 0.619 2.4 0.167 6.5 3.71 3.9 25 see B 2.5 0.637 1.5 0.180 3. 7 3.55 2.3 40 2.5 0.711 0.7 0.207 1.6 3.45 0.9 80 1 0.904 2.9 0.280 6.8 3.24 4.1

  • Measuring at high temperaturesSampleMuffle furnace from RTto 700 CMica cladded sensor

  • How accurate is Hot Disk ?An article by professor Torbjorn Log*compares results from 5 different materials, measured with different techniques, with Hot Disk measurements.*T.Log, S.E.Gustafsson, Transient Plane Source (TPS) Technique for Measuring Thermal Transport Properties of Building Materials, Fire and Materials 19, 43-49 (1995)

  • Layer Thickness : The thickness of the copper layers and intermediate insulating glass epoxy layers is specified in Table 1 using millimeters (mm).

    Table 1 Cross sectional details of the Test PCB #4's construction.

    PCB #

    Thickness of each Copper

    Layer (micrometers)

    Representation of Construction

    (Red=Copper and Black = FR-4)

    Thickness of each FR-4

    Layer (millimeters)

    PCB #4

    4-Layer

    Outer Signal Layer - 70 (m

    Top Plane Layer - 35 (m

    Bottom Plane Lyr - 35 (m

    Outer Signal Layer - 70 (m

    0,30 mm (2 Prepreg Layers)

    0,22 mm (core)

    0,30 mm (2 Prepreg Layers)

    0,40 mm (core)

    0,30 mm (2 Prepreg Layers)

    Notes: the Core and Prepreg layers are both considerd to have the same thermal conductivity values as FR-4.

  • ITHERM 2000: Seventh Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems,

    May 23-26, 2000, Las Vegas, NE, USA.

    Using Experimental Analysis to Evaluate the Influence of Printed Circuit Board

    Construction on the Thermal Performance of Four Package Types

    in both Natural and Forced Convection

    John Lohan1, Pekka Tiilikka2, Peter Rodgers3, Carl-Magnus Fager2, Jukka Rantala2

    1 Mechanical & Industrial Engineering Department, Galway-Mayo Institute of Technology, Galway, Ireland

    2 Nokia Research Center, P.O. Box 407, FIN-00045 NOKIA GROUP, Finland

    3 Mechanical & Aeronautical Engineering Department, University of Limerick, Limerick, Ireland

    [email protected]

  • ITHERM 2000: Seventh Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems,

    May 23-26, 2000, Las Vegas, NE, USA.

    Using Experimental Analysis to Evaluate the Influence of Printed Circuit Board Construction on the Thermal Performance of Four Package Typesin both Natural and Forced Convection

    John Lohan1, Pekka Tiilikka2, Peter Rodgers3, Carl-Magnus Fager2, Jukka Rantala2

    1 Mechanical & Industrial Engineering Department, Galway-Mayo Institute of Technology, Galway, Ireland

    2 Nokia Research Center, P.O. Box 407, FIN-00045 NOKIA GROUP, Finland

    3 Mechanical & Aeronautical Engineering Department, University of Limerick, Limerick, Ireland

    [email protected]

  • These are the samples..with properties found with different techniques.Almost 4 orders of magnitude

  • Results for diffusivity. Small deviations but who is right?

  • Results on Conductivity almost perfect agreement

  • Measuring on a NIST StandardExtruded Polystyrene, cert. No 1453Values given for a range of density and temperatures for a thickness of 13.4mmDensity from 38 kg/m3 to 46 kg/m3at 295 K, the given Thermal Resistance (m2K/W),converted to Thermal Conductivity by using the thicknessgives a range 0.0328-0.0338 W/mK

  • 13.4 mm100 mmDensity 43.8 kg/m3

    40.4 kg/m34 possible combinations to place the sensorSide combinations Results (W/mK) Std % 1-2 0.03394 0.12 2-1 0.03379 0.042-2 0.03451 0.081-1 0.03346 0.23

  • So.what Hot Disk can do in Evitherm..

    measure most materials from 0.005 to 500 W/mK..

    develop new applications

    provide consultancy, measurements and equipment,

    as well as training, courses, seminarsIn Uppsala development electronics, manufacturing, applications, testingservice

    In Gteborg development sensors/software applications, testing

  • Thats all folks !

    Thank you for your attention.

  • Metal insertVacuum feed throughSample holder and sensor

  • Outer lid with vacuum connection, gas valves, pressure valveand cables