IPC-7095C-2013.pdf - 第50页

be characterized by using the Shadow Moiré technique and should meet the warpage reflow specification. The final package coplanarity is a very complex combina- tion of the factors stated at the beginning of this section. A …

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found in solder balls at incoming inspection indicate
reduced solder volumes in the solder balls. This will trans-
late to smaller collapsed solder ball stand-off heights and
thus may reduce reliability.
For voids found during post-assembly inspection, reliabil-
ity of the solder joint may be compromised if a void is
excessive due to the reduction of solder cross-section
and/or surface bonding area both at the interposer and the
product board. It will be necessary to establish an accept-
able level of voiding so that the product can meet customer
expectations, has a useful working life and meets product
reliability requirements.
4.8.3 Solder Ball Attach Integrity One of the factors the
success of the BGA package depends upon is reliable sol-
der ball attachment. The solder balls need to be attached
within acceptable dimensional tolerances. Their height and
width after attach need to be within specified and/or
acceptable limits. Most important of all, they need to form
a proper metallurgical bond with the lands on the substrate.
All the solder balls need to see a temperature profile which
ensures wetting necessary for optimum connection. If the
joint does not wet, then the solder ball is not properly
attached for necessary mechanical and electrical intercon-
nect. Such balls may fall off during shipping, transportation
and handling, or may fail or act intermittently during elec-
trical testing. Figure 4-29 shows the surfaces of the solder
ball and the land. The left picture shows the flattened bot-
tom of a solder ball and the right picture shows the pad on
an FBGA where a ball was supposed to be attached.
If the attach process temperature is inadequate to form a
proper metallurgical bond, only a small amount of force is
needed to dislodge the solder ball from the pad since it was
held in place only by mechanical adhesion.
Solder ball attach integrity can be evaluated through solder
ball shear. Manual and automated shearing and shear force
recording instruments are available for that purpose. For
shear test it is not only the magnitude of the shear force
that is important, but also the failure mode. Failures at the
solder interface, indicated by ripping soldering pads out of
the resin matrix of the BGA or the lands of the PCB, are
positive indications of good wetting. For good attachment,
there should not be any unwetted areas.
4.8.4 Package and Ball Coplanarity Package coplanar-
ity is the result of all of the following factors:
1. Package thickness, pitch, and thermal requirements
2. Substrate design, material, and manufacturing processes
3. Number of devices (silicon) - size and thickness
4. Number of passives - size and thickness
5. Assembly materials and manufacturing processes
Coplanarity that is currently specified at room temperature
does not always ensure that the component will have a
proper joint formation at SMT. The package behavior dur-
ing reflow (dynamic warpage) could result in good or bad
contact with the solder during reflow regardless of room
temperature coplanarity. The dynamic warpage of the pack-
age depends on the package CTE (package size, die size,
package material). The dynamic warpage signature could
Figure 4-27 Example of Missing Balls on a BGA
Component
Figure 4-28 Example of Voids in Eutectic Solder Balls at
Incoming Inspection
Figure 4-29 Examples of Solder Ball/Land Surface
Conditions
Flattened bottom of
a solder ball
Pad on an FBGA where it was
supposed to be attached
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be characterized by using the Shadow Moiré technique and
should meet the warpage reflow specification.
The final package coplanarity is a very complex combina-
tion of the factors stated at the beginning of this section. A
large percentage (~70%) of the package coplanarity is con-
trolled by factors 1 and 2. The type of solder ball used will
determine how much overall package coplanarity can be
tolerated during the final package to board assembly. The
reason why collapsing eutectic solder and tin-alloy based
balls are the most popular is because they can compensate
for larger package coplanarity values.
The JEDEC design guidelines currently define the ball con-
tact diameter (b) at its maximum diameter, as measured in
a plane parallel to the seating plane, Datum C. The detail
illustrated in Figure 4-30 defines the profile tolerance zone
controlling coplanarity (ccc) and the limits for parallelism
between the package top surface (bbb) and the seating
plane (Datum C).
Package height is measured from top surface of the pack-
age to the seating plane (where the ball meets the mount-
ing surface of the host printed circuit board). It is impor-
tant that the top surface of the package remains parallel to
the seating plane, accommodating component handling in
test, inspection and assembly. The bilateral tolerance zone
(bbb) for parallelism references the top surface of the pack-
age with respect to Datum C, the seating plane.
4.8.4.1 Example for FBGA Coplanarity Tolerance limits
for coplanarity varies slightly with the increase in ball
diameter. The following shows the Controlled Coplanarity
(ccc) per ball size:
0.30 mm ball = 0.08 mm (ccc)
0.40 mm ball = 0.10 mm (ccc)
0.50 mm ball = 0.12 mm (ccc)
The unilateral profile tolerance zone (ccc) extends upward
from the seating plane. The lowest point of the ball contact
must be within the tolerance zone. Each ball has a toler-
ance zone associated with diameter ‘b’ that is located on
true position with respect to Datums A and B and is per-
pendicular to Datum C. The center of each ball must lie
within the tolerance zone. The positional tolerance for the
ball contact is defined with relationship to package outline
Datums A, B and C, as illustrated in Figure 4-31.
The array of tolerance zones associated with the ball diam-
eter (b), spaced on a basic pitch (e), controls the location
of the balls. The design guideline allows the array to float
with respect to the tolerance zone ‘ddd’’; however, the
centers of the balls must simultaneously lie within both
tolerance zones. For more detail in measuring the BGA
package, see JEDEC JEP95, Section 4.17 (BGA Package
Measuring and Methodology).
4.8.5 Moisture Sensitivity (Baking, Storage, Handling,
Rebaking)
Moisture sensitivity requirements are defined
by J-STD-020 and J-STD-033. The J-STD-033 provides
information on handling moisture sensitive components.
Components are segregated into eight levels as shown in
Table 4-10. These classes define how long a component
can be left out on the production floor once removed from
its sealed shipping bag. Parts exposed to ambient air for
longer than the specified time must be rebaked prior to use,
to drive out excess absorbed moisture.
Many BGA components are moisture sensitive; particular
attention should be paid to tape ball grid array (TBGA) and
flip chip FBGA components. Ceramic BGA/CGA compo-
nents are generally not moisture sensitive. J-STD-020 lim-
its the amount of time in which the package is permitted to
absorb moisture, but it is recommended that BGAs meet at
least a Level 3 specification. Level 5 and Level 6 parts are
particularly undesirable from a manufacturing handling
perspective because they drive additional shop floor and
component handling controls. In the case of Level 6 parts,
nX
ccc
C
bbb
C
C
A1
IPC-7095c-4-30
Figure 4-30 Establishing BGA Coplanarity Requirement
A
B
C
C
ddd
eee
M
M
b nX
IPC-7095c-4-31
Figure 4-31 Ball Contact Positional Tolerance
Table 4-10 Moisture Classification Level and Floor Life
Level
Floor life (out of bag) at factory
ambient 30°C/60% RH or as stated
1 Unlimited at 30°C/85% RH
2 1 year
2a 4 weeks
3 168 hours
4 72 hours
5 48 hours
5a 24 hours
6
Mandatory bake before use. After bake, must be
reflowed within the time limit specified on the label
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bake-out ovens will be required. Bake-out may take
between four hours and 48 hours at 125°C or five days to
68 days at 40°C depending on package thickness and size.
In order to remove moisture from BGA components, a rec-
ommended bake cycle should be established. It should be
noted that the higher reflow temperatures required for lead-
free solders may require a more rigorous moisture removal
bake cycle.
4.8.6 Shipping Medium (Tape and Reel, Trays, Tubes)
As with all SMT components, BGA parts should be pack-
aged in Electrostatic Discharge (ESD) packaging which
meets the requirements of the appropriate standards or
specifications. BGA components should be available in
JEDEC approved matrix trays able to withstand multiple
bake cycles, as many BGAs are moisture sensitive. See
4.8.5 for required bake temperatures and times for the dif-
ferent classes of moisture sensitive components.
It may be preferable to procure high volume parts, e.g.,
SRAM or DRAM devices, in tape-and-reel for faster
assembly cycle times. Component size and moisture sensi-
tivity may dictate that tape and reel is not applicable for
some BGAs. Tape widths up to 56 mm are available, and a
tape ‘leader of at least 200 mm should be provided. Cau-
tion must be used when baking parts in tape-and-reel, as
this type of packaging is usually restricted to lower bake
temperatures than matrix trays.
4.8.7 Solder Ball Alloy Component manufacturers
should establish a method to clearly identify the metallurgy
of the solder alloy used for the BGA balls, accompanied by
a part number change. J-STD-609 provides a convenient
method to identify the BGA ball alloy. Users may want to
verify the BGA alloy using screening methods such as
X-Ray Flourescence (XRF).
5 PRINTED BOARDS AND OTHER MOUNTING
STRUCTURES
Printed Boards (PBs) and other similar types of intercon-
nection platforms serve as mounting structures for BGAs
and other components. There is a wide variety of mounting
structures available to fulfill various interconnection sub-
strate requirements. These structures employ a wide range
of materials, both organic and inorganic and have a wide
range of physical properties. Materials are normally chosen
based on cost/performance needs of the finished product.
5.1 Types of Mounting Structures Following is an
examination of some of the more commonly used mount-
ing structure substrates.
5.1.1 Organic Resin Systems Organic substrates are
those that are most commonly used in the construction of
electronic interconnection structures. There is a well-
established worldwide manufacturing base for the organic
type of product. As a result of the large manufacturing
base, the organic materials used to create the structures
have the lowest cost among the competing technologies.
Organic materials have intrinsic beneficial electrical prop-
erties. Most notable is a relatively low dielectric constant
which can be made lower by the choice of resin and rein-
forcement. Rigid organic substrates are commonly rein-
forced with woven glass cloth. Flexible substrates are typi-
cally not reinforced.
5.1.2 Inorganic Structures Inorganic substrates are an
alternative to the organic substrates. They are commonly
refractory materials comprised of sintered metal oxides.
While they are typically brittle, they have some significant
benefits not easily obtained with organic substrates.
Chief among the advantages are excellent thermal proper-
ties. Like organic structures there are a number of possible
choices available: ceramic, silicon, and enameled metals.
The dielectric properties of these materials tend to be
higher than organic based materials and, because they are
brittle, they are generally more prone to breakage. Because
of the more limited vendor base for inorganic substrates,
these structures are normally more expensive.
5.1.3 Layering (Multilayer, Sequential or Build-Up)
While single and two metal layer circuits are still common,
multilayer interconnection structures are commonly
required to support the interconnection of BGAs in today’s
high performance electronics. There are several approaches
to creating multilayer circuit product. The traditional mul-
tilayer is created by printing and etching thin layers of
copper clad substrates and laminating them into a mono-
lithic structure which can be drilled and plated so as to
make connection between the layers where required.
More recently, however, alternative structures have been
developed to address the higher density and routing diffi-
culties associated with BGAs. These newer structures
employ a variety of different approaches to create suitable
multilayer structures. The new structures are variously
referred to as build-up multilayers, sequential multilayers
and co-laminated multilayers. A key feature of these struc-
tures is their use of very small vias. The term microvias has
been applied to describe these miniscule interconnections.
A typical microvia is less than 150 µm in diameter and has
a capture land (where the via starts) and a smaller target
land (where the via ends). The following examples in Fig-
ure 5-1 show different high density interconnect (HDI)
printed boards (see IPC-2226).
5.2 Properties of Mounting Structures
5.2.1 Resin Systems
There are a number of different
resin systems suitable for use in organic laminate construc-
tion. There is a long and well understood history and years
January 2013 IPC-7095C
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Provided by IHS under license with IPC
Not for Resale
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