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Accident? Consider the scenario where a designer wishes to
incorporate a newly developed device into a system and soon learns that a
heat sink is needed to cool the device. The designer finds a rather large
heat sink in a catalog which marginally satisfies the required thermal
criteria. Due to other considerations, such as fan noise and cost
constraints, an attempt to use a smaller heat sink proved futile, and so
the larger heat sink was accepted into the design. A prototype was made
which, unfortunately, burned-out during the initial validation test, the
product missed the narrow introduction time, and the project was canceled.
What went wrong?
The reasons could have been multi-fold. But, under this scenario, the
main culprit could have been the spreading resistance that was overlooked
during the design process. It is very important for heat sink users to
realize that, unless the heat sink is custom developed for a specific
application, thermal performance values provided in vendor's catalogs
rarely account for the additional resistances coming from the size and
location considerations of a heat source. It is understandable that the
vendors themselves could not possibly know what kind of devices the users
will be cooling with their products.
Introduction Spreading or constriction resistances exist
whenever heat flows from one region to another in different cross
sectional area. In the case of heat sink applications, the spreading
resistance occurs in the base-plate when a heat source of a smaller
footprin footprint area is mounted on a heat sink with a larger base-plate
area. This results in a higher local temperature at the location where the
heat source is placed. Figure 1 illustrates how the surface temperature of
a heat sink base-plate would respond as the size of the heat source is
progressively reduced from left to right with all other conditions
unchanged: the smaller the heat source, the more spreading has to take
place, resulting in a greater temperature rise at the center. In this
example, the effect of the edge surfaces of the heat sink is ignored and
the heat source is assumed to be generating uniform heat flux.
In cases where the footprint of a heat sink need not be much larger than
the size of the heat source, the contribution of the spreading resistance
to the overall device temperature rise may be insignificant and usually
falls within the design margin. However, in an attempt to remove more heat
from today's high performance devices, a larger heat sink is often used
and, consequently, the impact of spreading resistance on the performance
of a heat sink is becoming an important factor that must not be ignored in
the design process. It is not uncommon to find in many high performance,
high power applications that more than half the total temperature rise of
a heat sink is attributed to the spreading resistance in the base-plate.
The objectives of this article are:
1) to understand the physics and parameters associated with spreading
resistance
2) to provide a simple design correlation for accurate prediction of the
resistance
3) to discuss and clarify the concept of spreading resistance with an
emphasis on the practical use of the correlation in heat sink applications
The correlation provided herein was originally developed in references 1
and 2. This article is an extension of the earlier presentation.
Spreading Resistance Before we proceed with the analysis,
let us attend to what the temperature distributions shown in Fig. 1 are
telling us. The first obvious one, as noted earlier, is that the maximum
temperature at the center increases as the heat source becomes smaller.
Another important observation is that, as the temperature rises in the
center, the temperatures along the edges of the heat sink decrease
simultaneously. It can be shown that this happens in such a way that the
area-averaged surface temperature of the heat sink base-plate has remained
the same. In other words, the average heat sink thermal performance is
independent of the size of a heat source. In fact, as will be seen later,
it is also independent of the location of the heat source.
The spreading resistance can be determined from the following set of
parameters:
- footprint or contact area of the heat source, As
- footprint area of the heat sink base-plate, Ap
- thickness of the heat sink base-plate, t
- thermal conductivity of the heat sink base-plate, k
- average heat sink thermal resistance, R0
We will assume, for the time being, that the heat source is centrally
mounted on the base-plate, and the heat sink is cooled uniformly over the
exposed finned surface. These two assumptions will be examined in further
detail. Figure 2 shows a two-dimensional side view of the heat sink with
heat-flow lines schematically drawn in the base-plate whose thickness is
greatly exaggerated. At the top, the corresponding surface temperature
variation across the center line of the base-plate is shown by the solid
line. The dotted line represents the average temperature of the surface
which is, again, independent of the heat source size and can be easily
determined by multiplying R0
with the total amount of heat dissipation, denoted as Q.
As indicated in Fig. 2, the maximum constriction resistance Rc,
which accounts for the local temperature rise over the average surface
temperature, is the only additional quantity that is needed for
determining the maximum heat sink temperature. It can be accurately
determined from the following correlation.
 Figure
2 - Two dimensional schematic view of local resistance or temperature
variation of a heat sink shown with heat flow Lines
Note that the correlation addresses neither the shape of the heat source
nor that of the heat sink base-plate. It was found in the earlier study
that this correlation typically results in an accuracy of approximately 5%
over a wide range of applications with many combinations of different
source/sink shapes, provided that the aspect ratio of the shapes involved
does not exceed 2.5. See references 1 and 2 for further discussions.
Example Problem Consider an aluminum heat sink (k
= 200W/mK) with base-plate dimensions of 100 x 100 x 1.3 mm thick.
According to the catalog, the thermal resistance of this heat sink under a
given set of conditions is 1.0 °C/W. Find the maximum resistance of
the heat sink if used to cool a 25 x 25 mm device.
Solutions With no other specific descriptions, it is assumed
that the heat source is centrally mounted, and the given thermal
resistance of 1.0 °C/W represents the average heat sink performance.
From the problem statement, we summarize:
- As = 0.025 x 0.025 =
0.000625 m2
- Ap = 0.1 x 0.1 = 0.01 m2
- t = 0.0013 m
- k = 200 W/mK
- R0 = 1.0 °C/W
Therefore,

Hence, the maximum resistance, Rtotal
, is:
Rtotal = Ro
+ Rc = 1.0 + 0.66 = 1.66 °C/W
Readers should note the far right temperature distribution in Fig. 1
which is the result of a numerical simulation for the present problem in
rectangular coordinates.
Effect of Source Location In the following two sections, we
will limit our examination to the current example problem. As we shall
see, the result of this limited case study will allow us to draw some
general yet useful conclusions. Suppose the same heat source in the above
example was not centrally located, but mounted a distance away from the
center. Obviously, the maximum temperature would further rise as compared
to that found in the above example. Figure 3 shows the local resistances
corresponding to two such cases:

Figure
3 - Heat-sink local resistance showing the effect of source location: from
L to R, heat source at (37.5,0) and (37.5,37.5)
the first one is for the case where the heat source is mounted midway
along the edge, and the other, where it is mounted on one corner of the
heat sink. For these two special cases, the maximum spreading resistance
can be calculated by using Eq. (1) for Rc
with input parameters t and R0
modified as shown below:
| Rc
= C x Rc (Ap,As,k,t/C,R0/C) |
|
(3) |
with for the first
case, and C = 2 for the second case. It is to be noted that this
expression is independent of the source size. Numerically, for the current
problem with a 25 x 25 mm heat source, it results in the maximum spreading
resistances of 1.29 and 2.38 °C/W, or the total resistances of 2.29
and 3.38 °C/W for the first and second cases, respectively. For both
cases, it can be shown that the average surface resistance has not changed
from unity.
For other intermediate source locations, numerical simulations were
carried out and a plot is provided in Fig. 4 for the correction factor Cf
which can be used to compute the total resistance as
where Rc is determined from
Eq. (1), given for the case with the heat source placed at the center.
 Figure
4 - Correction factor as a function of source location
The coordinates in Fig. 4 indicate the location of the center of the
heat source measured from the center of the base-plate in mm: the case
with a centrally located heat source corresponds to (0,0), and the cases
shown in Fig. 3 correspond to (37.5,0) and (37.5,37.5) for the first and
second cases, respectively. Only one quadrant is shown in Fig. 4 as they
would be, owing to the assumption of uniform cooling, symmetrical about
(0,0). As can be seen from the figure, the correction factor increases
from 1 as the heat source is placed away from the center. It is worthwhile
noting that the increase is, however, very minimal over a wide region near
the center, and most increases occur closer to the edges.
Unlike C in the earlier expression, Cf
is case dependent (i.e. it depends on the heat-source size). However, it
was found that the plots of Cf
obtained for many other cases exhibit essentially the same profile as that
shown in Fig. 4, with magnitudes at the corners determined from Eq. (3),
and the domain of the plot defined by the maximum displacement of the heat
source. Based on this observation, a general conclusion can be made: for
all practical purposes, as long as the heat source is placed closer to the
center than to the edges of the heat sink, the correctional increase in
the spreading resistance may be ignored, and Cf
=1 may be used. As noted above, this would introduce a
small error of no greater than 5-10% in the spreading resistance which, in
turn, is a fraction of the total resistance.
So far, we have assumed a uniform cooling over the entire finned-surface
area of the base-plate. Although this is a useful assumption, it is seldom
realized in actual situations. It is well known that, due to the thinner
boundary layer and the less down-stream heating effect, a device would be
cooled more effectively if it is mounted toward the air inlet side. Again,
a numerical simulation is carried out using our example problem with the
boundary layer effect included.
Figure 5 shows the resulting modified correction factor as a function of
the distance from the center of the heat sink to the heat source placed
along the center line at y=0: x = -37.5 mm corresponds to the front most
leading edge location of the heat source and x = 37.5 mm the rear most
trailing edge placement.
 Figure
5 - Correction factor modified for boundary layer effect at y=0
As can be seen from the figure, it is possible to realize a small
improvement by placing the heat source forward of the center location
where Cf < 1. However, it
was experienced in practice that accommodating a heat source away from the
center and ensuring its mounting orientation often cause additional
problems during manufacturing and assembly processes.
Summary and Discussion A simple correlation equation is
presented for determining spreading resistances in heat sink applications.
A sample calculation is carried out for a case with a heat source placed
at the center of the heat sink base-plate and a means to estimate the
correction factor to account for the effect of changing the heat-source
location is provided. It is to be noted that the correlation provided
herein is a general solution which reduces to the well known Kennedy's
solution3 when R0
approaches 0: the mathematical equivalent of isothermal boundary
condition. Kennedy's solution is valid only when R0
is sufficiently small such that the fin-side of the heat sink base-plate
is close to isothermal. Otherwise, Kennedy's solution, representing the
lower boundary of the spreading resistance, may result in gross
underestimation of the resistance.
The earlier study revealed that, depending on the relative magnitude of
the average heat sink resistance, the spreading resistance may either
increase or decrease with the base-plate thickness. If the heat sink
resistance is sufficiently small, as in liquid cooled heat sink
applications, the spreading resistance always increases with the
thickness, and an optimum thickness does not exist. On the other hand, if
the heat sink resistance is large, as experienced in most air-cooled
applications, the spreading resistance decreases with the thickness and a
finite optimum thickness exists.
It is to be noted that the present correlation calculates the spreading
resistance only in the base-plate and does not account for the effect of
additional spreading that may exist in other places, such as the fins in a
planar heat sink. This additional spreading in the fins usually affects
the spreading resistance in a similar way to a thicker base-plate. The
current author found that an increase of 20% in the base-plate thickness
during the calculation roughly accounts for the effect of this additional
spreading in the fins of the same material for most planar heat sinks
under air cooling. No modification is required for pin-fin heat sinks.
Seri Lee Amkor Electronics, Inc. 1900 South Price Road Chandler,
AZ 85248, USA Tel: +1 (602) 821-2408 x 5459 Fax: +1 (602) 821-6730 Email:
lees@amkor.com
References
| 1. |
S. Lee, S. Song, V. Au, and K.P.
Moran, Constriction/Spreading Resistance Model for Electronic Packaging,
Proceedings of the 4th ASME/JSME Thermal Engineering Joint Conference,
Vol. 4, 1995, pp. 199-206. |
| 2. |
S. Song, S. Lee, and V. Au, Closed
Form Equation for Thermal Constriction/Spreading Resistances with
Variable Resistance Boundary Condition, Proceedings of the 1994 IEPS
Conference, 1994, pp. 111-121. |
| 3. |
D. P. Kennedy, Spreading
Resistance in Cylindrical Semiconductor Devices, Journal of Applied
Physics, Vol. 31, 1960, pp. 1490-1497. |
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