Thank you, Lee. I got it and I will let you know what we find out.
Dewey
-----Original Message-----
From: Leadfree [mailto:[log in to unmask]] On Behalf Of Lee Parker
Sent: Friday, August 25, 2006 7:08 AM
To: [log in to unmask]
Subject: Re: [LF] Copper Pad Peel Strength
Dewey
http://pcdandm.com/cms/cms/content/view/2802/95/
Best regards
Lee
J. L. Parker Ph.D.
JLP Consultants LLC
(804) 779 3389
-----Original Message-----
From: Leadfree [mailto:[log in to unmask]] On Behalf Of Whittaker, Dewey
(EHCOE)
Sent: Friday, August 25, 2006 9:58 AM
To: [log in to unmask]
Subject: Re: [LF] Copper Pad Peel Strength
Lee,
Good work. Could I get a copy of that or a link. We are starting to see
some of this and I have few theories on some new variables that been
thrown into the fray and would like to establish a good baseline test.
Dewey
-----Original Message-----
From: Leadfree [mailto:[log in to unmask]] On Behalf Of Lee parker
Sent: Friday, August 25, 2006 6:24 AM
To: [log in to unmask]
Subject: Re: [LF] Copper Pad Peel Strength
Amol
I published a paper on this issue in this months PC Design and
Fabrication.
In the paper, I go through a rigorous mathematical analysis of the peel
strength measurement. Essentially, I found it does not measure the bond
strength of the cooper, but rather a vector combination of shear and
tensile
stresses. For thermal failures the desired measurement is the shear
strength
of the bond. The plane and magnitude of the vector is highly dependent
upon
the radius of curvature and thickness of the copper being peeled from
the
substrate as well as the peel angle. In fact the dependence of the peel
strength is exponential dependent upon all three variables. So by very
minor
adjustments you can rotate the stress vector direction and magnitude and
get
a significant modification in the result (peel strength). We have all
known
this to be the case for years, I have only quantified the analysis. Keep
in
mind the ultimate tensile strength and the ultimate shear strength vary
by
an order of magnitude. So minor changes in the variables mentioned above
produce significant changes in the peel strength.
What I proposed in the article is the use of a double lap joint that is
pulled to failure. The test vehicle I proposed creates only a shear
stress.
This should be a huge improvement over the peel strength measurement.
----- Original Message -----
From: "Kane, Amol (349)" <[log in to unmask]>
To: <[log in to unmask]>
Sent: Friday, August 25, 2006 7:29 AM
Subject: [LF] Copper Pad Peel Strength
Dear Technetters,
We are having instances where copper pads (Under BGAs) are being lifted
off
ENIG Boards almost too easily during rework. We use the same thermal
profile
on each board (for the same component removal) and only some show this
phenomenon. Is there a test or standard to test the copper adhesion @
incoming to see whether it's the fab (i.e. are the boards coming to us
with
poor copper adhesion strength to being with) or the process that's doing
this. The board is heated upto 120 C when the component is reflowed for
removal. Also, is there data to show the decrease in Cu adhesion
strength
with temp?
Thanks,
Amol Kane
M.S (Industrial Eng.)
Process Engineer
Harvard Custom Manufacturing, Inc.
941 Route 38 Owego, NY 13827
Phone: (607) 687-7669 x349
[log in to unmask]
www.harvardgrp.com
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