3 NEW THEORETICAL MODEL AND VALIDATION BY LOCK-IN MICRO-THERMOGRAPHIC TEMPERATURE MAPPING
Transcription
3 NEW THEORETICAL MODEL AND VALIDATION BY LOCK-IN MICRO-THERMOGRAPHIC TEMPERATURE MAPPING
5th European Thermal-Sciences Conference, The Netherlands, 2008 3ω SCANNING THERMAL MICROSCOPY: NEW THEORETICAL MODEL AND VALIDATION BY LOCK-IN MICRO-THERMOGRAPHIC TEMPERATURE MAPPING M. Chirtoc, J.F. Henry Thermophysics Lab., UTAP, Univ. Reims, BP 1039, 51687 Reims Cedex 2, France Abstract We developed a general theory of ac hot wire method formulated in terms of dimensionless parameters. Simple analytical solutions are found for special cases of experimental relevance in scanning thermal microscopy (SThM) with Wollaston resistive thermal probe (ThP). Contrary to the ac or dc SThM electrical signal which is related to the spatial average temperature of the probe wire, the use of infrared micro-thermography permits to address directly the local parameters involved in the model and to confront the experimental results with the theoretical predictions. In particular, we investigated by dc and lock-in thermography the temperature distribution in the ThP as a function of modulation frequency, and the temperature profile along the heated wire on upscaled, self-made thermal probes, with the probe in air and in contact with solid and liquid samples. At last, we exploit the amplitude and phase thermograms of a thin composite sample out-of-contact and in-contact with the Wollaston ThP in order to evaluate the heat flux transferred to the sample through the air and by the physical contact. The latter amounts to 8% from the total electrical power and is frequency-independent. The separation of the two contributions is achieved by vector subtraction. 1 Introduction Resistive thermal probes (ThP) with Wollaston wire have been employed in conjunction with atomic force microscopes (AFM) for micro-thermal analysis [Pollock and Hammiche (2001)] and for scanning thermal microscopy (SThM) [Gmelin et al. (1998)]. The ThP consists of a thin PtRh wire bent at sharp angle. With modulated excitation current, its temperature-dependent resistance oscillates at the second harmonic while the voltage across the wire has a component at the third harmonic, proportional to the temperature amplitude averaged along the wire (3ω method) [Altes et al. (2004), Lefèvre and Volz (2005)]. In SThM, one of the problems in validating theoretical models by the experiment resides in the fact that the primary parameters which intervene in the models, such as the temperature profile along the wire, the local temperature at the ThP apex, the sample thermal conductance due to solid-solid contact only, the fraction of heat loss to ambient air, etc. are not directly accessible by the dc or ac electrical response of the ThP. This is because this signal is generated by the average wire temperature, in the sense of a spatial integral over length l, leading to spatial and temporal (i.e., high frequency) resolution loss. The motivation for the use of IR micro-thermography method in this study was to address directly the mentioned parameters and to confront the experimental results with the predictions of our model. 2 Theoretical background 5th European Thermal-Sciences Conference, The Netherlands, 2008 We developed a general theory of ac hot wire method accounting for distributed as well as for localized heat exchange mechanisms [Chirtoc and Henry (2007)]. The former depends on the exchange coefficient h with the ambient while the latter is relevant for SThM operation. The salient features of this model are: - dimensionless formulation in terms of normalized thermal admittances; - modular structure i.e., the heat balance in the wire is separated from the modeling of heat transfer parameters; - simple analytical solutions for local and average temperature field in the wire; - it accounts for possible non-linear effects. For thermal conductivity k mapping, the apex of the ThP is brought in contact with a solid sample. The resulting heat transfer through the contact surface is quantified by a dimensionless sample thermal admittance y. The solution of the differential fin equation is expressed as a form factor F(x,f)=θ(x,f)/θ0 representing the dimensionless temperature profile along the wire half-length l (with f the thermal modulation frequency corresponding to 2ω): F ( x) = [ 1 (ml ) 2 )] ( [ ( )] ⎧ ml + y 1 − e −ml e mx + ml − y 1 − e ml e −mx ⎫ ⎬ ⎨1 − ml(1 + yM ) e ml + e −ml ⎭ ⎩ ( ) (1) In particular, at the two ends F(l)=0 since the thick silver prongs supporting the wire act as heat sinks, while at the apex: F (0) = MM 1 / 2 2(1 + yM ) (2) with M(ml) = [tanh(ml)]/(ml) and M1/2 = M(ml/2). The argument ml is the fin parameter depending on geometrical and thermal properties of the wire, on h coefficient and on modulation frequency f. The 3ω voltage signal is proportional to F(x,f) averaged over the length l: V3ω ∝< F(x, f ) >= F( f )= 1 ⎛ 1+ yM1/ 2 ⎞ ⎜1− M ⎟ 2⎜ 1+ yM ⎟⎠ (ml) ⎝ (3) The equation (3) can be approached by a low pass transfer function [Chirtoc et al. (2004), (2006)]: F( f ) = F ( f << f c ) 1 + j f / fc (4) with fc=3α/2πl2 the cross over frequency and α the thermal diffusivity of wire material. In general, fc(y)>fc0(y=0). Equation (4) has two limiting cases (operation modes) in the frequency domain: isothermal (I) for f<fc and adiabatic (A) for f>fc. Measurements of thermophysical properties are possible in (I) mode in which F is independent of frequency. Then F(y) varies between 1/3 and 1/12 when 0<y<∞, yielding a theoretical dynamic range DR=4 in signal amplitude. A maximum phase variation of 35o is found around fc. The parameter y is related to the constriction thermal conductance [Carslaw and Jaeger (1959)], proportional to rck (rc is the radius of tip-sample contact area). Moreover, y is subjected also to large variability due to contact characteristics (area, force, humidity, surface roughness, hardness) and to ThP characteristics. We showed that most of these unwanted influences can be efficiently cancelled 5th European Thermal-Sciences Conference, The Netherlands, 2008 by normalization techniques [Chirtoc et al. (2006)]. Two limiting situations can be used for reference measurements at low frequency (I mode). With the tip in air (y→0), F(y)=1/3 and neglecting the heat loss to ambient, the temperature profile of equation (1) reduces to equation (5a). With the tip in perfect contact with an ideal heat sink (y→∞), F(y)=1/12 and instead of equation (5a) one obtains equation (5b). Both represent a parabolic temperature profile along the wire: 2 1⎡ ⎛x⎞ ⎤ F ( x) = ⎢1 − ⎜ ⎟ ⎥ 2⎣ ⎝ l ⎠ ⎦ (5a) 2 1 ⎡x ⎛ x⎞ ⎤ F ( x) = ⎢ − ⎜ ⎟ ⎥ 2⎣l ⎝ l ⎠ ⎦ (5b) When a thin sample suspended in air is in contact with the ThP, it is equivalent to an insulated and thermally thin (d<<μ) radial fin with axial symmetry. The radial temperature field θ(r,f) can be approximated by [Carslaw and Jaeger (1959)]: θ (r , f ) = − P/d 2π k π⎞ ⎛ 1.26 r + i ⎟⎟ ⎜⎜ ln μ 4⎠ ⎝ (6) with μ=(α/πf)1/2 the thermal diffusion length and P the heat flux amplitude leaving the ThP apex. From the real part of equation (6) one obtains: P − Re[θ (r , f )] = 2π kd ln(1.26 r / μ ) (7) Based on the model presented above, a number of figures of merit for the 3ω SThM can be defined [Chirtoc et al. (2004), Chirtoc and Henry (2007)]: - the mixing efficiency; - the temperature calibration factor; - the crossover frequency between isothermal and adiabatic mode of operation; - the dynamic range of amplitude and phase signals. 3 Materials and methods The Wollaston ThP produced by Veeco Co. (figure 1a), comprises a sensing element made of Pt0.9Rh0.1 wire (on the left in the figure) and is 2l=200 μm long and 5 μm in diameter. The thick prongs with coaxial structure (Wollaston wire) are 75 μm in diameter Ag sheaths. The epoxy glue ball is for mechanical rigidity. Behind it one can note the small mirror plate which reflects a diode laser beam in order to achieve the z-feedback control in the SThM. We used an IR camera type CEDIP JADE IRC 320-4 Long-Wave (LW) with 3:1 or 1:1 imaging objectives, which acquires 320x240 pixels/frame with 10x10 μm2 pixel size. Amplitude and phase thermograms in the range 0.4-90 Hz were obtained by lock-in processing and accumulation of video frames using the software developed in our laboratory [Pron et al. (2000), Pron and Bissieux (2004)]. The W (2l=3 mm and 100 μm in diameter) and Ni wires used for the home-made ThP were covered by lampblack to increase their IR emissivity and were imaged by at least two pixels across the diameter. The composite specimen studied in section 4.3 was a 2x2 cm2 typewriter carbon paper consisting of 20 μm thick paper substrate facing the ThP and 10 μm thick carbon-powder based black layer facing the IR camera. 5th European Thermal-Sciences Conference, The Netherlands, 2008 a) c) b) d) Figure 1: Wollaston thermal probe for SThM. a) Optical microscopy photograph, b) dc IR thermogram (red corresponds to strong IR radiation), c) amplitude and d) phase lock-in thermograms at 24 Hz frequency of excitation current. 4 Results and discussion There are three types of heat exchanges in a thermal microscopy experiment: the thermal balance within the thermal probe, the heat exchanged between the ThP tip and the sample following several heat flow channels, and the heat diffusion within the sample in relation with its structure and geometry. 4.1 Investigation of the Wollaston thermal probe The dc thermogram of figure 1b shows that with dc current excitation the whole body of the Wollaston ThP is heated above ambient by the heat developed mainly in the thin PtRh wire at the left end of the probe. The latter does not appear to be very bright due to its low emissivity typical for metals, but in fact it has the highest temperature in the image. On the lock-in thermograms of figures 1c and 1d one can see that with ac excitation the ac temperature field is well localized at the tip already at a frequency of 24 Hz. It follows that with the 3ω technique we may restrict the analysis of heat exchanges to the thin PtRh wire. As shown in section 2, the value of fc parameter scales with l-2. In order to verify this statement, we studied by thermography the temperature distribution along a tungsten (W) wire welded at each end to brass blocks [Chirtoc et al. (2004), (2005)]. The calculated temperature oscillation was 5 K for 1.4 A excitation current amplitude. Lock-in amplitude and phase profiles are shown in figure 2. Numerical values extracted from amplitude thermograms are shown in figure 3. The representation in figure 3a is based on dimensionless parameters f/fc and x/2l. The lines were computed for the Wollaston ThP with a finite element model assuming only conductive heat loss along the wire to the end-supports, and are identical to equation (1). The good agreement demonstrates the validity of the scaling law and the assumption of the predominance of heat loss by conduction through the wire to the supports. The saturation for f/fc<<1 (I mode) is clearly visible. By contrast, at high frequency f/fc>10 (A mode), the profile tends to be flat along the wire. 5th European Thermal-Sciences Conference, The Netherlands, 2008 0,4 Hz 200 μm 4 Hz 30 Hz Figure 2: Amplitude (left) and phase (right) temperature profiles along a linear, ac heated W wire, obtained by lock- in thermography. The wire is 3 mm long and 100 μm in diameter. The average temperature data of figure 3b are proportional to F(f) factor of equation 4. For this upscaled system, the cross over frequency between (I) mode and (A) mode is situated at fc=5.19 Hz corresponding to an effective length of 2l=5 mm (αW=67.4x10-6 m2s-1). This is longer than the free length of the wire and can be explained by residual thermal resistance at the welding sites. 4.2 Effect of the tip-sample contact We investigated the thermal balance of a self-made ThP with Ni wire as a function of various contact situations [Henry and Chirtoc (2005)]. We used a well-conducting liquid (Hg) in order to determine the DR of the ThP for large y in absence of thermal contact resistance, figure 4. At 0.5 Hz (I mode), the ratio between the integral over the half-length l of the experimental profile with the tip in air (red triangles) and the one with the tip in contact with the Hg droplet (red circles), yields DR=2.9. The maximum theoretical value saturates at DR=4 for y→∞, in agreement with equations (3) and (4). The same result is obtained by using the respective curves in figure 4c, calculated with finite element software or with equations (5a) and (5b). By contrast, at the same frequency, the DR of the local temperature at the contact is DR=9, and in theory it tends to infinity for a perfect contact with an ideal heat sink (from equation (2)). These findings show that the measurement of local contact temperature rather than the average one over the wire length (such as with electrical signals) might increase the performance of SThM. NORMALISED AMPL. 1 0,1 (b) fT 0,01 0,1 1 10 100 f (Hz) Figure 3: Temperature profiles of half-length wire (a) and integrated temperature along the wire (b), for the ac heated W wire of Figure 2. Points are data obtained from the thermograms. Lines are finite element computations. 5th European Thermal-Sciences Conference, The Netherlands, 2008 1,0 In air 0,5 Hz In air 40 Hz Perfect contact 0,5 Hz Perfect contact 40 Hz In air 0,5 Hz Contact Hg 0,5 Hz Contact Hg 40 Hz (a) (b) Normalized temperature amplitude 0,9 0,8 0,7 0,6 (c) 0,5 0,4 0,3 0,2 0,1 0,0 -1,0 -0,9 -0,8 -0,7 -0,6 -0,5 -0,4 -0,3 -0,2 -0,1 0,0 Normalized distance x / L Figure 4: dc thermograms of a thermal probe made of Ni wire (2l=3 mm and 40 μm in diameter) in the proximity (a) and in contact (b) with a Hg droplet, at 0.5 Hz. c) Temperature amplitude profiles of half-length wire in two extreme situations: lock-in thermograms (points) and finite element computations or with equations (5a,b) (lines). We measured also temperature profiles of the wire in case of contact with solid samples, figure 5. The ThP was attached to a micrometric z-translation stage and the sample was placed on a balance. By lowering the height of the ThP further beyond contact, the balance displayed the contact force in units of mass with a resolution of 0.1 mg. In addition to the sample conductivity, the figure 5c shows that the local temperature is strongly dependent on the contact force which modifies the size of contact surface. As expected, this dependence is less pronounced with hard materials like glass. For Cu, at 20 mgf, the local DR is 3.3, which is again larger than DR=1.5 of the spatial average. The theoretical values of the DR with solids cannot be estimated in absence of contact radii data. In the thermograms of figures 4a,b and 5a,b, the reflection of the bright (hot) wire at the Hg and Cu surface, respectively, allow to control the limit between in-contact and out-of-contact. 1.0 (a) (b) Normalized temperature . 0.9 0.8 0.7 0.6 (c) 0.5 0.4 0.3 0.2 0.1 Glass Steel Th Aluminium Copper f = 1 Hz 0.0 0 5 10 15 20 25 30 35 Force ( mgf) Figure 5: a) and b) same as Figures 4 a) and b), for polished Cu surface, at 1 Hz. c) Temperature amplitude at wire apex during contact, normalized to temperature out of contact, vs. contact force. 5th European Thermal-Sciences Conference, The Netherlands, 2008 4.3 Heat diffusion in a thin sample We measured in back-detection configuration the temperature distribution over a thin composite paper sample in the region of contact with the ThP (figure 6) [Henry et al. (2007)]. Experimental data fit with equations (6) and (7) allowed for determination of sample in-plane thermal diffusivity as α = 2.93x10-6 m2/s ±7% which results in k = 4.32 Wm-1K-1 the equivalent thermal conductivity of the composite sample (ρc = 1.47x106 kg m-3). The direct heat transfer via the contact was determined by vector subtraction of out-of-contact data from in-contact data, for different modulation frequencies. In figure 7a, P decreases with increasing frequency due to thermal wave attenuation by conduction across the air layer. The maximum power is reached at r ≈ 0.2 mm which represents the (surprisingly large) equivalent heat source radius in absence of contact. From the total ac heat flux, 6% to 23% are transferred by air conduction for f = 40 ... 0.2 Hz, respectively. On the other hand, from figure 7b a fraction of only about 8% is transferred directly to the sample via the contact. It is almost frequency- and radius-independent, in agreement with the point-heat source and radial-fin model employed. (a) (b) Figure 6: Radial distribution of temperature amplitudes (a) and phases (b) relative to the center, when theWollaston thermal probe is in contact with the specimen, at 0.2...40 Hz, from top to bottom. Insets show typical amplitude and phase lock-in thermograms. (a) (b) Figure 7: ac power (according to equation (7)) transferred from the thermal probe to the sample, vs. distance from the center; a) out-of-contact; b) difference between in-contact and out-of-contact. 5th European Thermal-Sciences Conference, The Netherlands, 2008 References Altes, A. Heiderhoff, R.and Balk, L.J., 2004, J. Phys. D: Appl. Phys. 37, 952. Carslaw, H.S. and Jaeger, J.C., 1959, Conduction of Heat in Solids, Second ed. (Oxford Univ. Press, London). Chirtoc, M., Filip, X., Henry, J.F., Antoniow, J.S., Chirtoc, I., Dietzel, D., Meckenstock, R. and Pelzl, J., 2004, Superlattices and Microstructures 35, 305 Chirtoc, M., Filip, X., Henry, J.F., Antoniow, J.S. and Pelzl, J., 2005, J. Phys. IV France 125, 83-85 Chirtoc, M., Gibkes, J., Antoniow, J.S., Henry, J.F., Neubauer, E., Bein, B. and Pelzl, J., 2006, J. Phys. IV France 137, 265 Chirtoc, M. and Henry, J.F., 2007, Proc. 14th Int. Conf. on Photoacoustic and Photothermal Phenomena, 14ICPPP, Cairo, Egypt, in The European Physical Journal, Special Topics (in press). Gmelin,E., Fischer, R.and Stitzinger, 1998, R., Thermochim. Acta 310, 1 Henry, J.F. and Chirtoc,M., 2005, Proc. "Congrès Annuel de la Societé Française de Thermique, SFT2005", Reims, France, (Ed SFT, Paris, Vol. 1, ISBN: 2-905267-43-7), 477 Henry, J.F., Pron, H. and Chirtoc, M., 2007, Proc. 14th Int. Conf. on Photoacoustic and Photothermal Phenomena, 14ICPPP, Cairo, Egypt, in The European Physical Journal, Special Topics (in press). Lefèvre, S.and Volz, S., 2005, Rev. Sci. Instrum., 76, 033701 Pollock H.M.and Hammiche, A., 2001, J. Phys. D: Appl. Phys. 34, R23 Pron, H., Henry, J.F., Offermann, S, Bissieux, C. and Beaudoin, J.L., 2000, High Temp. High Pressures 32, 473 Pron, H. and Bissieux, C., 2004, Int. J. Therm. Sci. 43, 1161