|
Metallurgical
Cross Sectioning of Microelectronic Packages for Optical Inspection
and Electron Beam Analysis(2)
Robert James
Burgoyne
Analog Devices, Inc.
SEM/EDS Analysis:
Reflected light microscopes are the analytical tool most frequently used for the
qualitative, and, at times, quantitative, examination of metallurgical cross
sections. These instruments do, however, have limitations. The wavelength of the
light source defines a useful magnification of about 1,000X, and a single focal
plane makes imaging samples with significant topographical details nearly
impossible. Superior depth of focus, considerably higher spatial resolution, and
elemental identification and mapping capabilities make the scanning electron
microscope the ideal complement to the reflected light microscope. This section
of the paper will focus on the practical application of the scanning electron
microscope to the examination of microelectronic package cross sections.
Specimens subjected
to electron beam irradiation undergo several complex interactions with the
electrons from the primary beam. This interaction volume yields a variety of
emission signals that may be collected and processed by one of several chamber
mounted detectors. Figure 9 offers a pictorial representation of a typical
interaction volume and emission products that are created when a sample is
subjected to primary beam excitation. A brief description of the signals that
originate from within the interaction volume follows:
Figure 9
Secondary electrons
(SE): Low energy
electrons emitted from a given atom due to the ionization event that occurs when
the primary beam electron collides with that atom. Created throughout the
interaction volume as a result of inelastic (electron-electron) collisions, SE's
typically have electron energy levels less than 50eV. As such, only those SE's
created near the surface escape the sample; the remainder are absorbed by
adjacent atoms.
Backscattered
electrons (BSE):
Electrons that pass close to, or encounter, the nucleus of a specimen atom and
are subsequently deflected through large angular trajectories with a minimal
loss of electron energy. Created throughout the interaction volume as a result
of elastic (electron-nucleus) collisions, BSE's have an energy level that is, on
average, about 20% lower than their initial accelerating potential. Because of
this negligible loss of energy, BSE's are able to escape to the surface from
deep within the interaction volume.
Characteristic
x-rays: As the incident
beam electron strikes an atom, a weak inner-shell electron is ejected. To
maintain atomic stability, a higher energy, outer-shell electron fills the
vacancy and simultaneously emits radiation whose value is equal to the
difference between the energy levels of the two shells. The portion of energy
lost by the decay of electrons as they move from outer to inner shells reflects
the unique electron transitions of a given element and, as such, are referred to
as a characteristic x-ray.
Continuum x-rays:
When an incident beam electron interacts with the nucleus of an atom, it is
decelerated and inelastically scattered. The resulting loss of energy can range
from 0eV up to the initial accelerating potential of the electron at the
emission source. This continuum, or white radiation, constitutes the major part
of the x-ray spectrum onto which the characteristic x-rays are superimposed.
The scanning electron microscope is an effective analytical tool that can
provide a wealth of useful information. A strong understanding of how a sample
will react to electron beam irradiation is the only surefire way to achieve
optimal results. Examination of the completed sections is fairly
straightforward; however, scanning electron microscopy is subjective in that
each analyst has their own way of conducting analyses to achieve the desired
results. Nonetheless, the following guidelines and helpful hints should be
considered when examining the sections.
Sample preparation:
Ensure that the sample is clean and dry prior to insertion in the SEM vacuum
chamber. If a conductive coating is not tolerable, apply conductive carbon or
silver paint to the bulk of the epoxy and down the side to the metal sample
holder. This practice will significantly reduce excess charging of the bulk
mounting material. Further, understand that prolonged exposure to high vacuum
(typically 10-7 Torr) will result in outgassing and shrinking of the epoxy, thus
creating small gaps along the periphery of the package. This could be of concern
if the sample is to be re-worked after examination of that specific plane of
interest.
Coating:
There are four interconnected reasons for coating a sample. In short, these are
to: 1) improve the signal, 2) increase the spatial resolution, 3) provide
conductivity so that excess surface charging can be shunted to ground potential
and 4) minimize thermal damage. Coatings fall into two categories: carbon (C)
and precious metals (Au, Au/Pd, Pt, etc.). The decision to apply a coating
largely depends on the type of analysis being performed. (Remember that the
features within microelectronic packages are huge when compared to the submicron
features on the integrated circuit. Imaging is often performed at magnifications
less than 20,000X; consequently, a 50Å - 100Å thick layer of conductive coating
is imperceptible and recommended when X-ray analysis is not being performed.
SE Imaging:
The majority of sample "viewing" will be accomplished using secondary electron
imaging. This mode of operation is invaluable when the identification of surface
structure is the principal objective for the analysis. When performing SE
imaging, it is often best to use lower beam accelerating potentials (<7.5kV) to
maximize surface topology resolution. This will not only reduce the amount of
local charging on the surface of uncoated samples, but will provide better
contrast in the image and photomicrograph due to the decrease in penetration of
the incident beam. The application of a precious metal film to semiconductor and
insulator materials will further enhance the quality of the image and
photomicrograph.
Figures 10A and 10B illustrate the effect that accelerating potential has
on image resolution and contrast. Shown is silver filled epoxy die attach that
has been etched in oxygen plasma for five minutes. Figure 10A was imaged at
3.0kV accelerating potential, and Figure 10B was imaged at 25.0kV accelerating
potential. Note the increase in surface resolution, decrease in edge charging
effects and inherently better image detail at 3.0kV. Both images were taken at a
magnification of 5,000X and at a 40° tilt angle to improve depth of field.
Figure 10A

Figure 10B

BSE Imaging:
BSE imaging provides both atomic number contrast and topographical information
about the sample being examined. Because BSE yield is significantly lower than
SE yield, higher beam accelerating potentials (>15kV) are often needed to
increase signal levels. Although charging is not an issue in BSE imaging, a
conductive coating is recommended for the reasons described earlier. Any
concerns that the image will be of a single contrast (i.e. that of the coating)
are unfounded; the vast majority of BSE's are generated well below the thin
conductive coating layer.
The number of BSE's generated in a given area of a sample is directly
proportional to the average atomic number of the material in that area. BSE
images of non-homogeneous samples will therefore inherently show dramatic
contrast variations. For example, in BSE images of gold-silicon (Au-Si)
eutectic, the Au phases (Z=79) will appear much brighter than the Si phases
(Z=14). This atomic number contrast information can prove invaluable when
"mapping" different materials in a sample or conducting EDS analysis.
Figures 11A and 11B illustrate the difference between BSE atomic number
contrast (11A) and BSE topography (11B) modes of operation. Shown is the plastic
multi-chip module sectioned for this paper. Note the more uniform grey shade and
"textured" appearance of Figure 11B, whereas Figure 11A has significant contrast
variations but lacks depth. Both images were taken at a magnification of 300X.
Figure 11A

Figure
11B
Figure 12 shows the
various layers found within a ceramic sidebraze package. Shown, from top to
bottom, is the silicon chip, gold/silicon die attach, nickel and cobalt plating
layers, sintered tungsten refractory and the ceramic package. The sample was
imaged in a SEM, in BSE mode, at a magnification of 1,250X.
Figure 12

Figure 13 shows a
plastic leadless chip carrier (PLCC) soldered onto a multi-layer printed circuit
board (PCB). This assembly was sectioned in an area that did not include the
silicon chip, thus making it an "all soft materials" sample. Shown clearly is
the bottom of the plastic package; the solder dipped, copper core package lead;
the multi-layer PCB; and the solder joint. (Note that the epoxide fully
encapsulated the assembly with no air bubble formation in the restricted area
between the lead and package body. This further illustrates the benefits of
using both a vacuum impregnation chamber and a pressurization vessel during
encapsulation.) The sample was imaged in a SEM, in BSE mode, at a magnification
of 250X.
Figure 13

X-ray Analysis:
When elemental identification (EDS) is required to complete an analysis, several
factors must be taken into consideration. First is the accelerating potential. A
general rule of thumb is to select an accelerating potential that is at least
2.5 times the primary x-ray line (in keV) of the heaviest element being
detected. For the vast majority of packages, including the one that will be used
as an example, that element is lead (Pb), common to most solders and frit seals.
The Pb La line appears at 10.55keV; thus, based on this line, the accelerating
potential should be set at approximately 26.5kV. However, lead has numerous
emission peaks due to its high atomic weight. The Pb Ma line appears at 2.34keV,
thus reducing the recommended accelerating potential substantially. This is
beneficial when analyzing samples that are mainly nonconductive. Severe local
charging can actually deflect the beam away from the primary area of interest,
resulting in erroneous data collection. Lowering the kV setting, without
compromising the detectability of all potential elements, is therefore highly
desirable. If appropriate, a high accelerating potential can initially be used
to identify all potential elements present. The accelerating potential can then
be lowered to not only reduce charging, but to improve the spatial resolution of
x-ray energies at the lower end of the spectrum.
Figures 14A and 14B represent the spectrum obtained when a ceramic
sidebraze package (14A) and plastic multi-chip module (14B) were subjected to a
whole package EDS analysis.
Figure 14A

Figure 14B

Conductive coating
is another factor that needs to be addressed. It is always best to perform an
initial x-ray analysis without a conductive coating. This preliminary analysis
provides a true and accurate qualitative assessment of all elements contained
within the package. When coating is necessary, select carbon, as it is the
preferred conductive coating when performing x-ray analysis. It generates only a
single peak (~0.25keV) at the low end of the spectra.
A third issue is
the scanning mode of the microscope. Most SEM's have three basic modes of
operation. These are: 1) Normal scan: the area being scanned is that which is
displayed on the screen; 2) Window or partial field: the area scanned is a
variable percentage of the total screen area; and 3) Spot: the X & Y deflection
coils are fixed at a controllable DC level, thus creating a moveable, single
point electron microprobe. Normal scan is generally used when analyzing whole
package sections, whereas window or spot mode is used when specific areas, such
as plating layers, intermetallics, etc. need to be analyzed.
X-ray mapping is a
versatile mode of x-ray analysis used to detect and display the spatial
distribution of one or more specific elements in a non-homogeneous sample when
multiple elements are being detected. In this application, a specific element is
initially selected for detection and display. When the given element is
detected, a bright spot is displayed on the SEM screen at the location that
correlates to the detection site. Numerous scans will generate a pattern of
light regions representing the relative distribution of the selected element.
This procedure can be repeated for several different elements, resulting in a
series of x-ray maps showing the distribution of all elements of interest.
Figure 15
illustrates the results of an x-ray map performed on the die attach area of the
plastic multi-chip module sectioned for this paper. Shown are: 1) a SE image of
the site, 2) a silicon (Si) map, 3) a copper (Cu) map and 4) a nickel (Ni) map.
Figure 15

Artifacts:
Microelectronic packages are no different than any other complex sample prepared
using metallographic techniques in that improper preparation can lead to induced
artifacts. Table 5 details the artifacts that microelectronic packages are more
likely to incur and suggestions on how to correct them. The recommended
corrective actions listed below are by no means exhaustive and the analyst may
have to resort to a "trial and error" method to determine the appropriate course
of action.
Table 5
|
Preparation Artifact |
Recommended Corrective Action(s) |
|
Relief |
Minimize
polishing times, use napless cloths, use diamond abrasives |
|
Edge
Rounding |
Minimize
polishing times, use napless cloths, use epoxide, reduce applied
pressure |
|
Smearing |
Reduce
applied pressure, use colloidal silica, increase lubrication, reduce
wheel speed |
|
Cracking &
Gaps |
Clean
sample before mounting; minimize abrasive size, reduce applied pressure, |
|
Embedded
Abrasives |
Reduce
applied pressure, use high viscosity lubricant, use medium nap cloth for
polishing |
|
Scratches |
Clean work
area, clean sample thoroughly after each step, finish each preparation
step |
Conclusions:
Proper implementation and utilization of metallographic sample preparation
techniques will provide valuable information about the overall quality of
microelectronic package components and the assembly process. The data obtained
by metallographic sectioning, and subsequent reflected light and electron beam
analysis, can be a critical part of failure analysis activities, process and
package qualifications and overall quality control. By always considering the
properties of all materials in a microelectronic package throughout the sample
preparation sequence, the analyst is able to produce deformation free cross
sections that can provide a wealth of information not easily obtained from any
other analytical technique.
Acknowledgements
The author would
like to take this opportunity to thank James Griffin, Hardie Macauley and Andrew
Olney at Analog Devices, Inc. and James Nelson at Buehler, LTD., for their
editing services, and Bruce Fried at Analog Devices, Inc., for his ultrasonic
imaging and radiography support.
References
1) B. Bousfield,
"Surface Preparation and Microscopy of Materials", John Wiley & Sons, LTD., West
Sussex, England, (1992).
2) "Metallography Principles and Procedures", Leco, Corp. (1992).
3) "Buehler Dialog, Microstructural Analysis Reference Manual", Buehler, LTD.
4) "Metalog Guide, Your Guide to the Perfect Materialographic Structure",
Struers Corp. (1992).
5) S.N. Chanat, A.M.H. Trujillo, D.C. Zipperian, Buehler Digest, Vol. 27, No. 1,
"Advanced Techniques for High Speed Precision Sectioning", Buehler, LTD, (1993).
6) B.L. Gabriel, "SEM, A User's Manual for Materials Science", American Society
for Metals, (1985).
7) A.M. Glauert, A.W. Agar, R.H. Anderson, D. Chescoe, "Principles and Practices
of Electron Microscope Operation", North-Holland Publishing Company, Amsterdam,
(1974).
Appendix
Table 3 (Process
Description for Ceramic and Metal Alloy Packages)
|
|
SURFACE |
LUBRICANT |
ABRASIVE |
TIME |
FORCE |
SPEED |
ROTATION |
|
PLANAR
GRINDING |
hard
lapping wheel |
water |
15µ M poly
diamond (water base) |
until plane |
7 psi/sample |
120 rpm |
contra-directional |
|
1ST
SAMPLE INTEGRITY |
napless
chemo-textile cloth |
colliodal
silica |
6 µ poly
diamond (water base) |
5 minutes |
6 psi/sample |
120 rpm |
complementary |
|
2ND
SAMPLE INTEGRITY |
napless
chemo-textile cloth |
colloidal
silica |
1 µ poly
diamond (water base) |
4 minutes |
5 psi/sample |
120 rpm |
complementary |
|
1ST
FINAL POLISH |
napless
chemo-textile cloth |
colloidal
silica |
colloidal
silica |
8 minutes |
7 psi/sample |
120 rpm |
complementary |
|
2ND
FINAL POLISH |
low-medium
nap cloth |
water |
50%
colloidal
silica/50% alumina |
2 minutes |
5 psi/sample |
90 rpm |
complementary |
Table 4 (Process
Description for Plastic Packages)
|
|
SURFACE |
LUBRICANT |
ABRASIVE |
TIME |
FORCE |
SPEED |
ROTATION |
|
PLANAR
GRINDING |
medium-hard
lapping wheel |
lapping oil |
9µM poly
diamond (oil base) |
until plane |
5 psi/sample |
90 rpm |
contra-directional |
|
1ST
SAMPLE INTEGRITY |
napless
chemo-textile cloth |
lapping oil |
3µM poly
diamond (oil base) |
5 minutes |
5 psi/sample |
90 rpm |
contra-directional |
|
2ND
SAMPLE INTEGRITY |
napless
chemo-textile cloth |
lapping oil |
1µM poly
diamond (oil base) |
4 minutes |
5 psi/sample |
90 rpm |
complementary |
|
1ST
FINAL POLISH |
napless
chemo-textile cloth |
colloidal
silica |
colloidal
silica |
5 minutes |
5 psi/sample |
90 rpm |
complementary |
|
2ND
FINAL POLISH |
low-medium
nap cloth |
di water |
50%
colloidal
silica/50% alumina |
2 minutes |
5 psi/sample |
90 rpm |
complementary |
(1) (2) |